US20040179953A1 - Gear pump - Google Patents
Gear pump Download PDFInfo
- Publication number
- US20040179953A1 US20040179953A1 US10/798,136 US79813604A US2004179953A1 US 20040179953 A1 US20040179953 A1 US 20040179953A1 US 79813604 A US79813604 A US 79813604A US 2004179953 A1 US2004179953 A1 US 2004179953A1
- Authority
- US
- United States
- Prior art keywords
- pressure
- pump
- gear
- fluid
- pump section
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000004891 communication Methods 0.000 claims abstract description 39
- 239000012530 fluid Substances 0.000 claims description 61
- 230000001105 regulatory effect Effects 0.000 claims description 29
- 239000000446 fuel Substances 0.000 claims description 10
- 230000033228 biological regulation Effects 0.000 claims description 8
- LCGLNKUTAGEVQW-UHFFFAOYSA-N Dimethyl ether Chemical compound COC LCGLNKUTAGEVQW-UHFFFAOYSA-N 0.000 description 96
- 230000003247 decreasing effect Effects 0.000 description 12
- 238000011144 upstream manufacturing Methods 0.000 description 10
- 238000002347 injection Methods 0.000 description 5
- 239000007924 injection Substances 0.000 description 5
- 239000007788 liquid Substances 0.000 description 5
- 230000006735 deficit Effects 0.000 description 4
- 238000004804 winding Methods 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000009834 vaporization Methods 0.000 description 3
- 230000008016 vaporization Effects 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical group [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 238000001816 cooling Methods 0.000 description 1
- 238000012937 correction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005674 electromagnetic induction Effects 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2/00—Rotary-piston machines or pumps
- F04C2/08—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C2/12—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type
- F04C2/14—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons
- F04C2/18—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing of other than internal-axis type with toothed rotary pistons with similar tooth forms
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C11/00—Combinations of two or more machines or pumps, each being of rotary-piston or oscillating-piston type; Pumping installations
- F04C11/001—Combinations of two or more machines or pumps, each being of rotary-piston or oscillating-piston type; Pumping installations of similar working principle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C15/00—Component parts, details or accessories of machines, pumps or pumping installations, not provided for in groups F04C2/00 - F04C14/00
- F04C15/0003—Sealing arrangements in rotary-piston machines or pumps
- F04C15/0034—Sealing arrangements in rotary-piston machines or pumps for other than the working fluid, i.e. the sealing arrangements are not between working chambers of the machine
- F04C15/0038—Shaft sealings specially adapted for rotary-piston machines or pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2/00—Rotary-piston machines or pumps
- F04C2/08—Rotary-piston machines or pumps of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
- F04C2/082—Details specially related to intermeshing engagement type machines or pumps
- F04C2/086—Carter
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2210/00—Fluid
- F04C2210/20—Fluid liquid, i.e. incompressible
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C2210/00—Fluid
- F04C2210/20—Fluid liquid, i.e. incompressible
- F04C2210/201—DME
Definitions
- the present invention relates to a gear pump used to send fluid under pressure.
- a gear pump as disclosed, for example, in Japanese Laid-Open Patent Publication No. 2001-140770 has been known.
- This gear pump has a pump section 101 as shown in FIG. 9.
- the pump section 101 has two stages of gear trains 111 , and each of the gear trains 111 has two pairs of drive gears 111 a and driven gears 111 b meshing with each other.
- a plurality of pump chambers 111 c for conveying fluid are defined by the gears 111 a and 111 b .
- Both drive gears 111 a are connected to a drive shaft 102 so as to be rotatable integrally with the drive shaft 102
- both driven gears 111 b are supported by a driven shaft 103 .
- each end portion of the drive shaft 102 and driven shaft 103 is supported via a bearing 104 .
- a gap i.e., an internal space 105 exists around the cylindrical surface of each of the shafts 102 and 103 at a position adjacent to the gears 111 a and 111 b in the pump section 101 . Therefore, there arises a problem in that the fluid leaks from the pump chambers 111 c into the internal space 105 , so that the efficiency of gear pump decreases.
- DME has a low viscosity and hence is liable to leak. Therefore, leakage of fluid, i.e., leakage of DME from the above-described pump chambers 111 c into the internal space 105 poses a serious problem.
- the gear pump mounted on a vehicle is especially required to have a small size. Therefore, it is difficult to arrange a sealing member in a leakage path between the pump chambers 111 c and the internal space 105 .
- An object of the present invention is to provide a gear pump in which fluid leakage from pump chambers to an internal space is reduced.
- the present invention provides a gear pump for sending fluid under pressure.
- the gear pump includes a pump section that draws fluid and discharges pressurized fluid.
- the pump section includes a gear train, a drive shaft and a driven shaft.
- the gear train has a pair of meshed gears. Each gear defines a plurality of pump chambers for conveying fluid in the pump section.
- the drive shaft has a cylindrical surface.
- One of the gears is coupled to the drive shaft such that the gear rotates integrally with the drive shaft.
- the driven shaft has a cylindrical surface. The driven shaft supports the other one of the gears.
- the pump section has an internal space that is located at a position adjacent to at least one of the gears and about the cylindrical surface of at least one of the drive shaft and the driven shaft.
- the pressure atmosphere of the internal space is an intermediate pressure atmosphere of the pressure of fluid drawn into the pump section and the pressure of fluid discharged from the pump section.
- FIG. 1 is a cross-sectional view of a pump in accordance with a first embodiment of the present invention
- FIG. 1A is an enlarged view of a portion surrounded by a chain line 1 A in FIG. 1;
- FIG. 2 is a sectional view taken along the line II-II of FIG. 1;
- FIG. 3 is a sectional view taken along the line III-III of FIG. 1;
- FIG. 4 is a schematic view of a fuel supply system provided with the pump shown in FIG. 1;
- FIG. 5 is an enlarged cross-sectional view of an essential portion of a pump in accordance with a second embodiment of the present invention.
- FIG. 6 is a cross-sectional view of a pump in accordance with a third embodiment of the present invention.
- FIG. 7 is a cross-sectional view of a pump in accordance with a fourth embodiment of the present invention.
- FIG. 8 is a cross-sectional view of a pump in accordance with a fifth embodiment of the present invention.
- FIG. 9 is a cross-sectional view of a prior art pump.
- a fuel supply system has a two-stage gear pump 1 .
- the fuel supply system supplies a fuel to an internal combustion engine (an engine), which is a driving source for running a vehicle.
- the suction side of the pump 1 is connected to a tank 2 through a suction pipe 3 .
- the tank 2 stores DME (dimethyl ether) used as fluid, or as a liquefied gas fuel.
- the discharge side of the pump 1 is connected to an injection pump 5 through a discharge pipe 4 .
- An engine 6 is connected to the discharge side of the injection pump 5 .
- the injection pump 5 supplies the DME, which is sent under pressure from the pump 1 , to the engine 6 in a high-pressure state.
- the pump 1 has a casing 7 and a lid 9 .
- the lid 9 is fixed to the opening end of the substantially bottomed cylindrical casing 7 , that is, at the left end as viewed in FIG. 1 via a plurality of bolts 8 .
- the casing 7 and the lid 9 constitute a pump housing of the pump 1 .
- the pump 1 is mounted on the vehicle in a state such that the left-hand side as viewed in FIG. 1 is the upper side and the right-hand side therein is the lower side.
- the casing 7 contains a motor section 10 fixed to the internal surface of the lid 9 and a pump section 11 connected to the motor section 10 .
- the pump 1 incorporates a motor 10 .
- the pump 1 requires no external drive source, and the interior of the pump 1 is sealed from the outside.
- a space outside the motor section 10 and the pump section 11 forms a sub tank 7 a .
- a drive shaft 12 is rotatably provided through these portions.
- the motor section 10 has a substantially bottomed cylindrical motor housing 10 a .
- the motor section 10 includes stators 10 b and a rotor 10 c .
- Each stator 10 b has a winding arranged along the inner circumferential surface of the motor housing 10 a .
- the rotor 10 c consists of an iron core arranged in a state of being surrounded by the stators 10 b .
- a space containing the stators 10 b and the rotor 10 c constitutes a motor chamber 60 .
- the rotor 10 c is fixed to and rotates integrally with the drive shaft 12 .
- each stator 10 b is connected to a terminal 15 .
- the drive shaft 12 is rotated by electromagnetic induction between the winding and the iron core of the rotor 10 c.
- the pump section 11 includes a base block 16 , a connection plate 19 , a side plate 20 , a connection plate 21 , and a tip-end plate 22 in that order from the motor section 10 .
- the base block 16 and the plates 19 to 22 are fixed to each other by a plurality of through bolts 23 (see FIGS. 2 and 3) in a state in which the drive shaft 12 is inserted.
- the pump section 11 is fixed to the motor section 10 by fixing a flange portion 16 a of the base block 16 to the motor housing 10 a via a plurality of bolts 24 (in FIG. 1, only one bolt is shown).
- the drive shaft 12 extends through the base block 16 and the plates 19 to 22 .
- the upper end (left end in FIG. 1) of the drive shaft 12 is supported by the motor housing 10 a via a bearing 13 .
- a recess 61 that opens toward the lid 9 is formed.
- the upper end of the drive shaft 12 and the bearing 13 are located in the recess 61 .
- the lower end (right end in FIG. 1) of the drive shaft 12 is supported by the tip-end plate 22 via a bearing 14 .
- the tip-end plate 22 is formed with a recess 62 .
- the lower end of the drive shaft 12 and the bearing 14 are located in the recess 62 .
- the bearings 13 and 14 each consist of a needle bearing serving as a roller bearing.
- a groove 12 a is formed in part of the outer circumferential surface that is in the vicinity of the lower end the drive shaft 12 .
- the groove 12 a extends in the axial direction of the drive shaft 12 .
- a key 25 having a substantially rectangular shape in cross section is arranged in the groove 12 a .
- a first drive gear 26 and a second drive gear 27 are provided in that order from the lower end along the axial direction of the drive shaft 12 .
- teeth 26 a and 27 a are formed, respectively.
- key grooves 26 b and 27 b are formed, respectively.
- the drive gears 26 and 27 each are made to be rotatable integrally with the drive shaft 12 by engaging the key 25 with the surface defining the key groove 26 b , 27 b.
- a driven shaft 29 is rotatably housed in parallel with the drive shaft 12 .
- the driven shaft 29 extends through the base block 16 constituting the pump section 11 and the plates 19 to 22 constituting the pump section 11 .
- the upper end (left end as viewed in FIG. 1) of the driven shaft 29 is supported by the base block 16 via a bearing 30 .
- the base block 16 is formed with a recess 63 .
- the upper end of the driven shaft 29 and the bearing 30 are located in the recess 63 .
- the lower end (right end in FIG. 1) of the driven shaft 29 is supported by the tip-end plate 22 via a bearing 31 .
- the tip-end plate 22 is formed with a recess 64 .
- the lower end of the driven shaft 29 and the bearing 31 are located in the recess 64 .
- the bearings 30 and 31 each consist of a needle bearing serving as a roller bearing.
- a first driven gear 32 and a second driven gear 33 are provided in that order from the lower end side along the axial direction of the driven shaft 29 .
- teeth 32 a and 33 a are formed, respectively.
- the first driven gear 32 is provided so as to be rotatable relatively to the driven shaft 29 .
- the second driven gear 33 is formed integrally with the driven shaft 29 .
- the first driven gear 32 meshes with the corresponding first drive gear 26 on the drive shaft 12
- the second driven gear 33 meshes with the corresponding second drive gear 27 on the drive shaft 12 .
- a suction connecting portion 35 On the outer circumferential surface of the casing 7 , a suction connecting portion 35 is provided.
- the suction connecting portion 35 has a suction port 35 a communicating with the sub tank 7 a , and is connected with the suction pipe 3 extending from the tank 2 (see FIG. 4).
- the DME in the tank 2 is introduced through the suction pipe 3 and the suction port 35 a , and is stored in the sub tank 7 a .
- the pump section 11 When the pump section 11 is operated, the pump section 11 sucks the DME in the sub tank 7 a .
- the pump section 11 increases the pressure of DME through a plurality of gear trains. That is, the pump section 11 is of a tandem type.
- the pump section 11 has a first-stage gear train 36 that is a first gear train, or a low-pressure side gear train, consisting of the first drive gear 26 and the first driven gear 32 , and a second-stage gear train 37 that is a second gear train consisting of the second drive gear 27 and the second driven gear 33 .
- the first-stage gear train 36 functions as a low-pressure side gear train.
- the second-stage gear train 37 functions as a high-pressure side gear train.
- the pump section 11 increases the pressure of DME stepwise by causing the DME to flow through the first-stage gear train 36 and the second-stage gear train 37 successively.
- a discharge connecting portion 39 is provided on the external surface of the lid 9 .
- the discharge connecting portion 39 has a discharge port 39 a , and is connected with the discharge pipe 4 extending from the injection pump 5 (see FIG. 4).
- the pump section 11 discharges the DME, the pressure of which has been increased, from the discharge port 39 a to the discharge pipe 4 through a first pump section internal passage (not shown).
- connection plate 21 has a hole 21 a for accommodating the first drive gear 26 and a hole 21 b for accommodating the first driven gear 32 .
- the connection plate 21 has an upstream passage 40 and a downstream passage 41 . Because having the upstream passage 40 and the downstream passage 41 , the connection plate 21 has some space on both sides of the meshed portions of the first drive gear 26 and the first driven gear 32 .
- the upstream passage 40 and the downstream passage 41 serve as passages for DME.
- the upstream passage 40 communicates with the sub tank 7 a through a second pump section internal passage (not shown).
- the connection plate 19 also has holes, an upstream passage, and a downstream passage, which are the same as the holes 21 a and 21 b , the upstream passage 40 , and the downstream passage 41 in the connection plate 21 .
- the drive shaft 12 rotates in the direction of a black arrow in FIG. 2, that is, in the clockwise direction.
- the driven shaft 29 rotates following the rotation of the drive shaft 12 via the gear trains 36 and 37 . That is to say, the driven shaft 29 rotates in the direction indicated by the white arrow in FIG. 2, that is, in the counterclockwise direction.
- the first-stage gear train 36 has a plurality of low-pressure pump chambers 36 a and 36 b .
- the DME having reached the first-stage gear train 36 is conveyed toward the downstream passage 41 through the pump chambers 36 a or 36 b .
- Each of the pump chambers 36 a is defined by the two adjacent teeth 26 a of the first drive gear 26 and the inner circumferential surface of the hole 21 a .
- Each of the pump chambers 36 b is defined by the two adjacent teeth 32 a of the first driven gear 32 and the inner circumferential surface of the hole 21 b.
- the side plate 20 has a hole 20 a for inserting the drive shaft 12 and a hole 20 b for inserting the driven shaft 29 , these two holes 20 a and 20 b being located adjacently.
- the diameter of the hole 20 a is set larger than the diameter of the drive shaft 12 . Therefore, a clearance is provided between the drive shaft 12 and the hole 20 a .
- the diameter of the hole 20 b is set larger than the diameter of the driven shaft 29 . Therefore, a clearance is provided between the driven shaft 29 and the hole 20 b.
- the side plate 20 has a communication passage 43 for connecting the downstream passage 41 of the first-stage gear train 36 to the upstream passage 42 of the second-stage gear train 37 .
- the communication passage 43 includes a first passage 43 a , a second passage 43 b , and a third passage 43 c .
- the first passage 43 a extends in the radial direction of the pump 1 .
- the second passage 43 b extends in the axial direction of the pump 1 from the downstream passage 41 of the first-stage gear train 36 and communicates with the first passage 43 a .
- the third passage 43 c extends in the axial direction of the pump 1 from the upstream passage 42 of the second-stage gear train 37 and communicates with the first passage 43 a .
- the DME the pressure of which has been increased by the first-stage gear train 36 , passes through the second passage 43 b , the first passage 43 a , and the third passage 43 c in that order from the downstream passage 41 and is sent to the upstream passage 42 of the second-stage gear train 37 .
- the second-stage gear train 37 has a plurality of high-pressure pump chambers 37 a and 37 b . As shown in FIG. 1A, the DME having reached the second-stage gear train 37 is conveyed to the discharge port 39 a through the pump chambers 37 a or 37 b .
- Each of the pump chambers 37 a is defined by the two adjacent teeth 27 a of the second drive gear 27 and the inner circumferential surface of the corresponding hole in the connection plate 19 .
- Each of the pump chambers 37 b is defined by the two adjacent teeth 33 a of the second driven gear 33 and the inner circumferential surface of the corresponding hole in the connection plate 19 .
- the DME which has been sent to the discharge port 39 a after the pressure thereof has been increased by the second-stage gear train 37 , is supplied to the injection pump 5 through the discharge pipe 4 . That is, the pump section 11 discharges fluid that has been drawn into a fluid conveying passage, which includes the pump chambers 36 a to 37 b , from the fluid conveying passage through the pump chambers 36 a to 37 b .
- the pressure at the starting point of the fluid conveying passage is the suction pressure of the pump section 11
- the pressure at the endpoint of the fluid conveying passage is the discharge pressure of the pump section 11 .
- the lid 9 is fitted with a pipe connecting portion 54 .
- the pipe connecting portion 54 is connected with a leak pipe 55 extending from the tank 2 (see FIG. 4).
- the pipe connecting portion 54 has a leak port 56 for connecting the internal space of the recess 61 to the leak pipe 55 .
- the motor housing 10 a has a communication hole 65 for connecting the internal space of the recess 61 to the motor chamber 60 .
- the side wall of the motor housing 10 a is provided with a vent hole 57 for connecting the motor chamber 60 to the upper space of the sub tank 7 a.
- the sliding portions in the motor section 10 and the sliding portions in the pump section 11 generate heat by means of sliding operation. Being subjected to the influence of such heat generation, the DME in the sub tank 7 a and the DME leaking from the gear trains 36 and 37 into the motor chamber 60 may be vaporized.
- the interior of the pump 1 is sealed from the outside.
- the pump 1 incorporating the motor 10 is of a shaft enclosed type in which the drive shaft 12 is sealed in the casing 7 and the lid 9 . In the shaft enclosed type pump 1 , the vaporized DME is possibly accumulated in the sub tank 7 a or the motor chamber 60 .
- the vaporized DME in the sub tank 7 a moves to the motor chamber 60 through the vent hole 57 , and the vaporized DME in the motor chamber 60 is returned to the tank 2 through the communication hole 65 , the internal space of the recess 61 , the leak port 56 , and the leak pipe 55 in that order. Therefore, the occurrence of troubles, such as insufficient cooling of the motor section 10 caused by the filling of evaporated DME, is prevented.
- an internal space 51 is present around a cylindrical surface 12 b of the drive shaft 12 at a position adjacent to the drive gears 26 and 27 .
- the internal space 51 includes a first space 51 a , a second space 51 b , and a third space 51 c .
- the first space 51 a is located between the first drive gear 26 and the bearing 14 .
- the first space 51 a is a part of the recess 62 provided in the tip-end plate 22 .
- the second space 51 b is located between the drive gears 26 and 27 .
- the third space 51 c is located on the upper side of the second drive gear 27 .
- the diameter of a portion ranging from a midway point of the base block 16 to the lower end of the drive shaft 12 is smaller than that of the upper portion.
- the third space 51 c is located between this small-diameter portion on the lower end side of the drive shaft 12 and the base block 16 .
- the first space 51 a and the second space 51 b are connected to each other by some gap around the key 25 and the groove 12 a .
- the second space 51 b and the third space 51 c are connected to each other by some gap around the key 25 and the groove 12 a .
- a communication passage for connecting the first space 51 a to the second space 51 b may be formed in the first drive gear 26
- a communication passage for connecting the second space 51 b to the third space 51 c may be formed in the second drive gear 27 .
- a space 62 a is present on the lower end face of the drive shaft 12 beyond the bearing 14 .
- the space 62 a is connected to the first space 51 a through a gap that the bearing 14 has.
- the third space 51 c is connected to the motor chamber 60 through a gap between the base block 16 and the large-diameter portion of the drive shaft 12 , that is, a communication hole 76 .
- the internal space of the recess 61 of the motor housing 10 a is connected to the motor chamber 60 through the communication hole 65 in the motor housing 10 a .
- a space 61 a in which the upper end face of the drive shaft 12 is exposed, is connected to the motor chamber 60 through the communication hole 65 .
- the pressure atmosphere of the space 61 a exposed to the upper end face of the drive shaft 12 and the pressure atmosphere of the space 62 a exposed to the lower end face of the drive shaft 12 are the same as the pressure atmosphere of the motor chamber 60 .
- the pressure in the motor chamber 60 is approximately equal to the suction pressure of the pump section 11 . Therefore, the force based on the pressure in the recess 61 , which is applied to the upper end face of the drive shaft 12 , and the force based on the pressure in the recess 62 , which is applied to the lower end face of the drive shaft 12 , are balanced.
- the pressure atmosphere of the first space 51 a is the same as the pressure atmosphere of the second space 51 b located adjacently to the first space 51 a with the first drive gear 26 being held therebetween. Therefore, the opposing thrust loads applied to the first drive gear 26 due to the imbalance of the pressure in the first space 51 a and the pressure in the second space 51 b cancel each other. As a result, wear and other types of impairment of the first drive gear 26 are prevented.
- the pressure atmosphere of the second space 51 b is the same as the pressure atmosphere of the third space 51 c located adjacently to the second space 51 b with the second drive gear 27 being held therebetween. Therefore, opposing thrust loads applied to the second drive gear 27 due to the imbalance of the pressure in the third space 51 c and the pressure in the second space 51 b cancel each other. As a result, wear and other types of impairment of the second drive gear 27 are prevented.
- an internal space 52 is present around a cylindrical surface 29 a of the driven shaft 29 at a position adjacent to the driven gears 32 and 33 .
- the internal space 52 includes a first space 52 a , a second space 52 b , and a third space 52 c .
- the first space 52 a is located between the first driven gear 32 and the bearing 31 . That is, the first space 52 a is a part of the recess 64 provided in the tip-end plate 22 .
- the second space 52 b is located between the driven gears 32 and 33 .
- the third space 52 c is located between the second driven gear 33 and the bearing 30 . That is, the third space 52 c is a part of the recess 63 provided in the base block 16 .
- the first space 52 a and the second space 52 b are connected to each other by some gap between the first driven gear 32 and the cylindrical surface 29 a of the driven shaft 29 .
- a space 64 a is present on the lower end face of the driven shaft 29 .
- the space 64 a is connected to the first space 52 a through a gap that the bearing 31 has.
- a space 63 a is present on the upper end face of the driven shaft 29 .
- the space 63 a is connected to the third space 52 c through a gap that the bearing 30 has.
- the space 63 a exposed to the upper end face of the driven shaft 29 in the base block 16 is connected to the space 64 a exposed to the lower end face of the driven shaft 29 in the tip-end plate 22 through an in-shaft passage 66 formed in the driven shaft 29 .
- the in-shaft passage 66 extends along the axis of the driven shaft 29 .
- the pressure atmosphere of the space 63 a exposed to the upper end face of the driven shaft 29 is the same as the pressure atmosphere of the space 64 a exposed to the lower end face of the driven shaft 29 . Therefore, the force based on the pressure in the recess 63 , which is applied to the upper end face of the driven shaft 29 , and the force based on the pressure in the recess 64 , which is applied to the lower end face of the driven shaft 29 , are balanced. As a result, a thrust load applied to the driven shaft 29 due to the imbalance of the two forces is canceled.
- the pressure atmosphere of the second space 52 b is the same as the pressure atmosphere of the third space 52 c located adjacently to the second space 52 b with the second driven gear 33 being held therebetween. Therefore, opposing thrust loads applied to the second driven gear 33 , which are a thrust load due to the imbalance of pressure in the second space 52 b and pressure in the third space 52 c and a thrust load due to the imbalance of pressure in the recess 63 and pressure in the recess 64 , cancel each other. As a result, wear and other types of impairment of the second driven gear 33 are prevented.
- the pressure atmosphere of the first space 52 a is the same as the pressure atmosphere of the second space 52 b located adjacently to the first space 52 a with the first driven gear 32 being held therebetween. Therefore, opposing thrust loads applied to the first driven gear 32 due to the imbalance of the pressure in the first space 52 a and the pressure in the second space 52 b cancel each other. As a result, wear and other types of impairment of the first driven gear 32 are prevented.
- the pressure in the communication passage 43 for connecting the first-stage gear train 36 to the second-stage gear train 37 is equal to the discharge pressure of the first-stage gear train 36 , in other words, the suction pressure of the second-stage gear train 37 .
- the pressure in the communication passage 43 is higher than the suction pressure of the first-stage gear train 36 , i.e., the suction pressure of the pump section 11 , and is lower than the discharge pressure of the second-stage gear train 37 , i.e., the discharge pressure of the pump section 11 .
- the pressure atmosphere of the communication passage 43 is the pressure atmosphere of intermediate pressure of the pump section 11 .
- the communication passage 43 functions as an intermediate-pressure zone.
- the side plate 20 has a pressure introduction passage 67 .
- the pressure introduction passage 67 connects the first passage 43 a of the communication passage 43 to the second space 52 b of the internal space 52 , which is close to the driven shaft 29 .
- the intermediate pressure in the communication passage 43 is introduced to the second space 52 b through the pressure introduction passage 67 .
- the second space 52 b is connected to the internal space of the recess 64 in the tip-end plate 22 , that is, to the first space 52 a and the space 64 a .
- the internal space of the recess 64 is connected to the third space 52 c .
- the pressure atmosphere of the internal space 52 around the cylindrical surface 29 a of the driven shaft 29 , the pressure atmosphere of the space 63 a exposed to the upper end face of the driven shaft 29 , and the pressure atmosphere of the space 64 a exposed to the lower end face of the driven shaft 29 are the same as the pressure atmosphere of the communication passage 43 , i.e., the pressure atmosphere of intermediate pressure of the pump section 11 .
- the pressure atmosphere of the internal space 52 which is close to the driven shaft 29 of the pump section 11 , is the pressure atmosphere of intermediate pressure of the pump section 11 . Therefore, for example, when compared with the case where the pressure atmosphere of the internal space 52 is the same as the suction pressure or the discharge pressure of the pump section 11 , the maximum value of difference in pressure produced between the pump chambers 36 b , 37 b close to the driven shaft 29 and the internal space 52 is decreased.
- the pump 1 of this embodiment is suitable as a pump mounted on a vehicle.
- the internal space 52 is connected to the communication passage 43 , which functions as an intermediate-pressure zone, via the pressure introduction passage 67 . Therefore, the internal space 52 is made to have a pressure atmosphere of intermediate pressure by a simple construction such as the pressure introduction passage 67 .
- the communication passage 43 connecting the discharge side of the first-stage gear train 36 to the suction side of the second-stage gear train 37 forms an intermediate-pressure zone.
- a high pressure which is the discharge pressure of the first-stage gear train 36
- the internal space 52 is introduced to the internal space 52 . Therefore, the maximum difference in pressure produced between the pump chambers 36 b , 37 b and the internal space 52 is further decreased. As a result, the efficiency of the pump 1 is further improved.
- a shaft seal device 71 is provided between the base block 16 and the drive shaft 12 .
- the shaft seal device 71 disconnects the motor chamber 60 from the third space 51 c of the internal space 51 in the pump section 11 .
- the shaft seal device 71 includes, for example, a lip type seal.
- the side plate 20 has a pressure introduction passage 72 .
- the pressure introduction passage 72 connects the first passage 43 a of the communication passage 43 to the second space 51 b of the internal space 51 .
- the intermediate pressure of the communication passage 43 is introduced to the second space 51 b of the internal space 51 through the pressure introduction passage 72 . That is to say, the pressure atmosphere of the internal space 51 around the cylindrical surface 12 b of the drive shaft 12 and the pressure atmosphere of the space 62 a exposed to the lower end face of the drive shaft 12 are the same as the pressure atmosphere of intermediate pressure of the pump section 11 .
- the vent hole 57 in the motor housing 10 a and the pressure introduction passage 67 in the side plate 20 are eliminated from the above-described first embodiment.
- the space 63 a (see FIG. 1A) exposed to the upper end face of the driven shaft 29 in the recess 63 is connected to the motor chamber 60 through a communication hole 75 penetrating the base block 16 .
- the third space 51 c (see FIG. 1A) of the internal space 51 close to the drive shaft 12 is connected to the motor chamber 60 through the gap between the base block 16 and the large-diameter portion of the drive shaft 12 , that is, the communication hole 76 . Therefore, the pressure atmosphere of the internal spaces 51 and 52 is the same as the pressure atmosphere of the motor chamber 60 .
- a pressure regulating valve 77 is disposed at a midway point of the leak port 56 in the pipe connecting portion 54 .
- the pressure regulating valve 77 is a differential pressure regulating valve including a valve element 77 a and an urging spring 77 b .
- the pressure regulating valve 77 opens and closes the leak port 56 according to a difference between the pressure on the motor chamber 60 side applied to the valve element 77 a and the pressure on the tank 2 (see FIG. 4) side similarly applied to the valve element 77 a.
- the high-pressure pump chambers 37 a and 37 b function as a high-pressure zone.
- the pressure in the high-pressure zone is higher than the pressure in the internal spaces 51 and 52 .
- the pressure in the internal spaces 51 and 52 and the motor chamber 60 is increased due to the leakage of DME from the pump chambers 37 a and 37 b , that is, the pressure leakage, and the vaporization of DME in the motor chamber 60 .
- the valve element 77 a of the pressure regulating valve 77 moves in the valve opening direction against the urging force in the valve closing direction generated by the urging spring 77 b and a force in the valve closing direction generated by the pressure in the section connected to the tank 2 .
- the valve element 77 a releases the leak port 56 . Therefore, the pressure in the internal spaces 51 and 52 and the motor chamber 60 tends to be decreased by the sending-out of pressure to the tank 2 through the leak port 56 , so that the pressure returns to the aforementioned predetermined value.
- the pressure regulating valve 77 opens and closes the leak port 56 autonomously so as to keep the pressure in the internal spaces 51 and 52 and the motor chamber 60 at the predetermined value.
- the construction of the pressure regulating valve 77 of an autonomous type is simpler than that of a pressure regulating valve of, for example, an external control type.
- the aforementioned predetermined value that is, the target of regulation of the pressure in the internal spaces 51 and 52 and the motor chamber 60 accomplished by the pressure regulating valve 77 is set to the intermediate pressure of the pump section 11 in the steady-state operating condition, for example, to the discharge pressure of the first-stage gear train 36 .
- the setting of the pressure regulation target is concretely performed by the adjustment of the spring force of the urging spring 77 b .
- the internal spaces 51 and 52 have the pressure atmosphere of intermediate pressure of the pump section 11 . Therefore, the leakage of DME between the pump chambers 36 a , 36 b , 37 a , 37 b and the corresponding internal space 51 , 52 is decreased.
- the target value of the pressure in the internal spaces 51 and 52 is changed easily by changing the operating characteristics of the pressure regulating valve 77 , for example, the spring force of the urging spring 77 b . Therefore, the pressure in the internal spaces 51 and 52 , which varies from pump to pump, is corrected to a desired value by simple work.
- the pressure in the internal spaces 51 and 52 which varies from pump to pump, is corrected to a desired value by simple work.
- the pressure leakage from the pump section 11 is an inevitable phenomenon.
- the pressure leakage tends to increase the pressure in the internal spaces 51 and 52 .
- the internal spaces 51 and 52 are caused to have an intermediate pressure atmosphere by utilizing the tendency for the pressure in the internal spaces 51 and 52 to increase due to this inevitable pressure leakage from the pump section 11 .
- the internal spaces 51 and 52 need not be isolated from the motor chamber 60 .
- the DME leaking from, for example, from the second-stage gear train 37 is positively supplied to the motor chamber 60 through the internal spaces 51 and 52 and the communication holes 75 and 76 .
- the motor section 10 is cooled properly by the liquid DME supplied to the motor chamber 60 . Thereby, the operation of the motor section 10 is stabilized.
- the communication holes 75 and 76 , the motor chamber 60 , the communication hole 65 , the internal space of the recess 61 , the leak port 56 , and the leak pipe 55 function as a pressure regulation passage that connects the tank 2 functioning as a low-pressure zone to the internal spaces 51 and 52 .
- the pump 1 in accordance with a fourth embodiment is changed. Specifically, the upstream-side of the leak port 56 of the pipe connecting portion 54 is connected to the upper space of the sub tank 7 a .
- the lid 9 has an internal passage 79 for connecting the internal space of the recess 61 to the upper space of the sub tank 7 a .
- the vaporized DME in the motor chamber 60 is discharged through the communication hole 65 , the internal space of the recess 61 , and the internal passage 79 , and is returned to the tank 2 through the leak port 56 and the leak pipe 55 together with the DME vaporized in the sub tank 7 a.
- the pressure regulating valve 77 is disposed to regulate the pressure in the motor chamber 60 so as to be an intermediate pressure by the same operation as that in the above-described third embodiment.
- the sub tank 7 a functions as a low-pressure zone.
- the communication holes 75 and 76 , the motor chamber 60 , the communication hole 65 , the internal space of the recess 61 , and the internal passage 79 function as a pressure regulation passage that connects the internal spaces 51 and 52 to the low-pressure zone, i.e., the sub tank 7 a.
- the above-described third embodiment is changed. Specifically, the motor section 10 is arranged at the lower part (right-hand side as viewed in FIG. 8) of the casing 7 , and the pump section 11 is arranged at the upper part (left-hand side as viewed in FIG. 8) of the casing 7 . That is to say, the pump 1 is mounted on a vehicle in a state in which the pump section 11 is at the upper position and the motor section 10 is at the lower position.
- the pump section 11 and the discharge connecting portion 39 installed to the lid 9 are arranged so as to be close to each other. Therefore, the first pump section internal passage (not shown) for connecting the pump section 11 to the discharge connecting portion 39 is laid out easily, which is advantageous in decreasing the size of the pump 1 . Also, since the motor section 10 is arranged at the lower part of the casing 7 , the liquid level of DME in the motor chamber 60 is surely located at the upper part of the motor chamber 60 . Therefore, the stators 10 b and the rotor 10 c are less liable to be exposed above the liquid level of DME, so that they are cooled properly by DME (liquid).
- the upstream-side of the leak port 56 is connected to the internal space of the recess 62 in the tip-end plate 22 .
- the leak port 56 and the motor chamber 60 are connected to each other through the internal space 51 close to the drive shaft 12 and the communication hole 76 . Therefore, the vaporized DME in the motor chamber 60 is discharged into the tank 2 through the communication hole 76 , the internal space 51 , the leak port 56 , and the leak pipe 55 (see FIG. 4).
- the pressure in the internal space 51 tends to be increased under the influence of DME leakage from the high-pressure pump chambers 37 a and 37 b (see FIG. 1A), which function as high-pressure zones, and under the influence of vaporization of DME in the motor chamber 60 .
- the pressure in the internal space 51 is released into the tank 2 through the leak port 56 and the leak pipe 55 .
- the pressure regulating valve 77 regulates the pressure in the internal space 51 so as to be the intermediate pressure of the pump section 11 by regulating the opening of the leak port 56 and the degree of sending-out of pressure from the internal space 51 .
- the communication hole 75 is eliminated. That is to say, the internal space 52 close to the driven shaft 29 is isolated from the motor chamber 60 . However, the internal space 52 is connected to the communication passage 43 between the gear trains 36 and 37 through the pressure introduction passage 67 . That is to say, the internal space 52 close to the driven shaft 29 is made to have a pressure atmosphere of intermediate pressure of the pump section 11 by the same method as that in the above-described first embodiment.
- the pressure in the internal space 51 close to the drive shaft 12 is regulated directly by the pressure regulating valve 77 .
- the pressure in the motor chamber 60 is regulated directly, and resultantly the pressure in the motor chamber 60 is reflected to the pressure in the internal space 51 .
- the operation of the pressure regulating valve 77 is immediately reflected to the pressure in the internal space 51 . Therefore, the pressure in the internal space 51 is further stabilized. As a result, the leakage of DME between the low-pressure pump chambers 36 a , the high-pressure pump chamber 37 a and the internal space 51 close to the drive shaft 12 is restrained more effectively.
- the internal space of the recess 62 , the leak port 56 , and the leak pipe 55 function as a pressure regulation passage that connects the internal space 51 to the tank 2 .
- the invention may be embodied in the following forms.
- the pump chambers 36 a , 36 b , 37 a , 37 b during the conveyance under pressure are grasped as intermediate-pressure zones.
- the internal space 51 is connected to the intermediate-pressure zone through the pressure introduction passage.
- the internal spaces 51 and 52 are connected to the intermediate-pressure zone through the pressure introduction passage.
- the pressure introduction passage 67 is eliminated. That is to say, only the internal space 51 is made to have the intermediate pressure.
- the pressure regulating valve 77 is of an autonomous type (differential pressure regulating valve). By changing this, a valve of an external control type, such as a solenoid valve, is used as a pressure control valve.
- a pressure sensor and control means (described below).
- the pressure sensor detects the pressure in the corresponding internal spaces 51 and 52 or the pressure in a space having the same pressure atmosphere as that of the said space.
- the control means which is, for example, a computer, controls the opening and closing of the pressure control valve based on detected information sent from the pressure sensor.
- the pressure regulation passage that connects the internal spaces 51 and 52 to the low-pressure zone can be opened or closed according to the pressure in the corresponding internal spaces 51 and 52 without being affected by the pressure state on the low-pressure zone side. Therefore, the pressure in the corresponding internal spaces 51 and 52 can surely be regulated so as to have a predetermined value.
- the invention is embodied in the pump 1 of a type such as to be mounted outside the tank 2 .
- the invention is embodied in a gear pump of what is called an in-tank type, which is contained in the tank 2 .
- the casing 7 is eliminated.
- the fluid handled by the gear pump is not limited to DME.
- the invention may be embodied in a gear pump that handles a liquid (gas) other than DME.
- the invention is embodied in the two-stage gear pump.
- the invention is not limited to the gear pump of this type.
- the invention may be embodied in the gear pump of a plurality of stages other than two stages, such as three stages or four stages.
- the invention may be embodied in a one-stage gear pump.
- the gear pump is of a shaft enclosed type, i.e., a type such that the motor is incorporated.
- the gear pump may be of a shaft open type, i.e., a type such that the pump section is driven by an external motor.
- the gear pump in accordance with the present invention is not limited to a vehicular gear pump that sends a liquefied gas fuel under pressure to an internal combustion engine.
- the present invention may be applied to a gear pump used to send hydraulic fluid etc. under pressure, for example, in a machine tool.
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Abstract
A two-stage gear pump has a pump section. The pump section has an internal space that is located adjacent to a driven gear and about a cylindrical surface of the driven shaft. A discharge section of a first gear train is connected to a suction section of a second gear train with a communication passage. The internal space is connected to the communication passage with a pressure introduction passage. The pressure of the communication passage is introduced to the internal space by the pressure introduction passage, so that the pressure atmosphere of the internal space is an intermediate pressure atmosphere of the suction pressure and the discharge pressure of the pump section.
Description
- The present invention relates to a gear pump used to send fluid under pressure.
- Conventionally, a gear pump as disclosed, for example, in Japanese Laid-Open Patent Publication No. 2001-140770 has been known. This gear pump has a
pump section 101 as shown in FIG. 9. Thepump section 101 has two stages ofgear trains 111, and each of thegear trains 111 has two pairs of drive gears 111 a and drivengears 111 b meshing with each other. In thepump section 101, a plurality ofpump chambers 111 c for conveying fluid are defined by thegears 111 a and 111 b. Both drive gears 111 a are connected to adrive shaft 102 so as to be rotatable integrally with thedrive shaft 102, and both drivengears 111 b are supported by a drivenshaft 103. - When the
drive shaft 102 is rotated, both drive gears 111 a connected to theshaft 102 rotate. When the drive gear 111 a rotate, the corresponding drivengear 111 b supported by the drivenshaft 103, which meshes with the drive gear 111 a, rotates following the rotation of the drive gear 111 a. Therefore, thepump chambers 111 c convey the fluid, and thereby the pressure of the fluid is increased. - In the above-described gear pump, each end portion of the
drive shaft 102 and drivenshaft 103 is supported via abearing 104. For the reason of this support construction, a gap, i.e., aninternal space 105 exists around the cylindrical surface of each of theshafts gears 111 a and 111 b in thepump section 101. Therefore, there arises a problem in that the fluid leaks from thepump chambers 111 c into theinternal space 105, so that the efficiency of gear pump decreases. - There exists a fuel supply system for supplying a liquefied gas fuel such as dimethyl ether (hereinafter abbreviated to DME) to a vehicular internal combustion engine. This fuel supply system sometimes uses the above-described gear pump. The gear pump has no expansion stroke. Therefore, the gear pump is superior in handling DME that is easy to vaporize.
- DME has a low viscosity and hence is liable to leak. Therefore, leakage of fluid, i.e., leakage of DME from the above-described
pump chambers 111 c into theinternal space 105 poses a serious problem. The gear pump mounted on a vehicle is especially required to have a small size. Therefore, it is difficult to arrange a sealing member in a leakage path between thepump chambers 111 c and theinternal space 105. - An object of the present invention is to provide a gear pump in which fluid leakage from pump chambers to an internal space is reduced.
- To achieve the above-mentioned objective, the present invention provides a gear pump for sending fluid under pressure. The gear pump includes a pump section that draws fluid and discharges pressurized fluid. The pump section includes a gear train, a drive shaft and a driven shaft. The gear train has a pair of meshed gears. Each gear defines a plurality of pump chambers for conveying fluid in the pump section. The drive shaft has a cylindrical surface. One of the gears is coupled to the drive shaft such that the gear rotates integrally with the drive shaft. The driven shaft has a cylindrical surface. The driven shaft supports the other one of the gears. The pump section has an internal space that is located at a position adjacent to at least one of the gears and about the cylindrical surface of at least one of the drive shaft and the driven shaft. The pressure atmosphere of the internal space is an intermediate pressure atmosphere of the pressure of fluid drawn into the pump section and the pressure of fluid discharged from the pump section.
- Other aspects and advantages of the invention will become apparent from the following description, taken in conjunction with the accompanying drawings, illustrating by way of example the principles of the invention.
- The invention, together with objects and advantages thereof, may best be understood by reference to the following description of the presently preferred embodiments together with the accompanying drawings in which:
- FIG. 1 is a cross-sectional view of a pump in accordance with a first embodiment of the present invention;
- FIG. 1A is an enlarged view of a portion surrounded by a
chain line 1A in FIG. 1; - FIG. 2 is a sectional view taken along the line II-II of FIG. 1;
- FIG. 3 is a sectional view taken along the line III-III of FIG. 1;
- FIG. 4 is a schematic view of a fuel supply system provided with the pump shown in FIG. 1;
- FIG. 5 is an enlarged cross-sectional view of an essential portion of a pump in accordance with a second embodiment of the present invention;
- FIG. 6 is a cross-sectional view of a pump in accordance with a third embodiment of the present invention;
- FIG. 7 is a cross-sectional view of a pump in accordance with a fourth embodiment of the present invention;
- FIG. 8 is a cross-sectional view of a pump in accordance with a fifth embodiment of the present invention; and
- FIG. 9 is a cross-sectional view of a prior art pump.
- First to fifth embodiments of the present invention will now be described. In the second to fifth embodiments, only points different from the first embodiment are explained, that is, the same reference numerals are applied to the same or equivalent elements, and the explanation thereof is omitted.
- As shown in FIG. 4, a fuel supply system has a two-
stage gear pump 1. The fuel supply system supplies a fuel to an internal combustion engine (an engine), which is a driving source for running a vehicle. The suction side of thepump 1 is connected to atank 2 through a suction pipe 3. Thetank 2 stores DME (dimethyl ether) used as fluid, or as a liquefied gas fuel. The discharge side of thepump 1 is connected to aninjection pump 5 through adischarge pipe 4. An engine 6 is connected to the discharge side of theinjection pump 5. Theinjection pump 5 supplies the DME, which is sent under pressure from thepump 1, to the engine 6 in a high-pressure state. - As shown in FIG. 1, the
pump 1 has acasing 7 and alid 9. Thelid 9 is fixed to the opening end of the substantially bottomedcylindrical casing 7, that is, at the left end as viewed in FIG. 1 via a plurality ofbolts 8. Thecasing 7 and thelid 9 constitute a pump housing of thepump 1. Thepump 1 is mounted on the vehicle in a state such that the left-hand side as viewed in FIG. 1 is the upper side and the right-hand side therein is the lower side. Thecasing 7 contains amotor section 10 fixed to the internal surface of thelid 9 and apump section 11 connected to themotor section 10. Thus, thepump 1 incorporates amotor 10. That is to say, thepump 1 requires no external drive source, and the interior of thepump 1 is sealed from the outside. In thecasing 7, a space outside themotor section 10 and thepump section 11 forms asub tank 7 a. In themotor section 10 and thepump section 11, adrive shaft 12 is rotatably provided through these portions. - The
motor section 10 has a substantially bottomedcylindrical motor housing 10 a. Themotor section 10 includesstators 10 b and arotor 10 c. Eachstator 10 b has a winding arranged along the inner circumferential surface of themotor housing 10 a. Therotor 10 c consists of an iron core arranged in a state of being surrounded by thestators 10 b. In themotor section 10, that is, in themotor housing 10 a, a space containing thestators 10 b and therotor 10 c constitutes amotor chamber 60. Therotor 10 c is fixed to and rotates integrally with thedrive shaft 12. The winding of eachstator 10 b is connected to a terminal 15. When a current is caused to flow in the winding of thestators 10 b via theterminals 15 by the power supplied from the outside, thedrive shaft 12 is rotated by electromagnetic induction between the winding and the iron core of therotor 10 c. - As shown in FIGS. 1 and 1A, the
pump section 11 includes abase block 16, aconnection plate 19, aside plate 20, aconnection plate 21, and a tip-end plate 22 in that order from themotor section 10. Thebase block 16 and theplates 19 to 22 are fixed to each other by a plurality of through bolts 23 (see FIGS. 2 and 3) in a state in which thedrive shaft 12 is inserted. Thepump section 11 is fixed to themotor section 10 by fixing aflange portion 16 a of thebase block 16 to themotor housing 10 a via a plurality of bolts 24 (in FIG. 1, only one bolt is shown). - The
drive shaft 12 extends through thebase block 16 and theplates 19 to 22. The upper end (left end in FIG. 1) of thedrive shaft 12 is supported by themotor housing 10 a via abearing 13. On the end surface of themotor housing 10 a, arecess 61 that opens toward thelid 9 is formed. The upper end of thedrive shaft 12 and thebearing 13 are located in therecess 61. The lower end (right end in FIG. 1) of thedrive shaft 12 is supported by the tip-end plate 22 via abearing 14. The tip-end plate 22 is formed with arecess 62. The lower end of thedrive shaft 12 and thebearing 14 are located in therecess 62. Thebearings - As shown in FIG. 1A, a
groove 12 a is formed in part of the outer circumferential surface that is in the vicinity of the lower end thedrive shaft 12. Thegroove 12 a extends in the axial direction of thedrive shaft 12. In thegroove 12 a, a key 25 having a substantially rectangular shape in cross section is arranged. - As shown in FIGS.1 to 3, on the
drive shaft 12, afirst drive gear 26 and asecond drive gear 27 are provided in that order from the lower end along the axial direction of thedrive shaft 12. On the outer circumferential surfaces of the drive gears 26 and 27,teeth key grooves drive shaft 12 by engaging the key 25 with the surface defining thekey groove - In the
pump section 11, a drivenshaft 29 is rotatably housed in parallel with thedrive shaft 12. The drivenshaft 29 extends through thebase block 16 constituting thepump section 11 and theplates 19 to 22 constituting thepump section 11. The upper end (left end as viewed in FIG. 1) of the drivenshaft 29 is supported by thebase block 16 via abearing 30. Thebase block 16 is formed with arecess 63. The upper end of the drivenshaft 29 and thebearing 30 are located in therecess 63. The lower end (right end in FIG. 1) of the drivenshaft 29 is supported by the tip-end plate 22 via abearing 31. The tip-end plate 22 is formed with arecess 64. The lower end of the drivenshaft 29 and thebearing 31 are located in therecess 64. Thebearings - On the driven
shaft 29, a first drivengear 32 and a second drivengear 33 are provided in that order from the lower end side along the axial direction of the drivenshaft 29. On the outer circumferential surfaces of the driven gears 32 and 33,teeth gear 32 is provided so as to be rotatable relatively to the drivenshaft 29. The second drivengear 33 is formed integrally with the drivenshaft 29. The first drivengear 32 meshes with the correspondingfirst drive gear 26 on thedrive shaft 12, and the second drivengear 33 meshes with the correspondingsecond drive gear 27 on thedrive shaft 12. - On the outer circumferential surface of the
casing 7, asuction connecting portion 35 is provided. Thesuction connecting portion 35 has asuction port 35 a communicating with thesub tank 7 a, and is connected with the suction pipe 3 extending from the tank 2 (see FIG. 4). The DME in thetank 2 is introduced through the suction pipe 3 and thesuction port 35 a, and is stored in thesub tank 7 a. When thepump section 11 is operated, thepump section 11 sucks the DME in thesub tank 7 a. Thepump section 11 increases the pressure of DME through a plurality of gear trains. That is, thepump section 11 is of a tandem type. - Specifically, the
pump section 11 has a first-stage gear train 36 that is a first gear train, or a low-pressure side gear train, consisting of thefirst drive gear 26 and the first drivengear 32, and a second-stage gear train 37 that is a second gear train consisting of thesecond drive gear 27 and the second drivengear 33. The first-stage gear train 36 functions as a low-pressure side gear train. The second-stage gear train 37 functions as a high-pressure side gear train. Thepump section 11 increases the pressure of DME stepwise by causing the DME to flow through the first-stage gear train 36 and the second-stage gear train 37 successively. On the external surface of thelid 9, adischarge connecting portion 39 is provided. Thedischarge connecting portion 39 has adischarge port 39 a, and is connected with thedischarge pipe 4 extending from the injection pump 5 (see FIG. 4). Thepump section 11 discharges the DME, the pressure of which has been increased, from thedischarge port 39 a to thedischarge pipe 4 through a first pump section internal passage (not shown). - As shown in FIG. 2, the
connection plate 21 has ahole 21 a for accommodating thefirst drive gear 26 and ahole 21 b for accommodating the first drivengear 32. Theconnection plate 21 has anupstream passage 40 and adownstream passage 41. Because having theupstream passage 40 and thedownstream passage 41, theconnection plate 21 has some space on both sides of the meshed portions of thefirst drive gear 26 and the first drivengear 32. Theupstream passage 40 and thedownstream passage 41 serve as passages for DME. Theupstream passage 40 communicates with thesub tank 7 a through a second pump section internal passage (not shown). Although not illustrated, theconnection plate 19 also has holes, an upstream passage, and a downstream passage, which are the same as theholes upstream passage 40, and thedownstream passage 41 in theconnection plate 21. - The
drive shaft 12 rotates in the direction of a black arrow in FIG. 2, that is, in the clockwise direction. The drivenshaft 29 rotates following the rotation of thedrive shaft 12 via thegear trains shaft 29 rotates in the direction indicated by the white arrow in FIG. 2, that is, in the counterclockwise direction. When thedrive shaft 12 and the drivenshaft 29 rotate, the DME having been sent into thepump section 11 flows into the first-stage gear train 36 through theupstream passage 40. The first-stage gear train 36 has a plurality of low-pressure pump chambers stage gear train 36 is conveyed toward thedownstream passage 41 through thepump chambers pump chambers 36 a is defined by the twoadjacent teeth 26 a of thefirst drive gear 26 and the inner circumferential surface of thehole 21 a. Each of thepump chambers 36 b is defined by the twoadjacent teeth 32 a of the first drivengear 32 and the inner circumferential surface of thehole 21 b. - As shown in FIG. 3, the
side plate 20 has a hole 20 a for inserting thedrive shaft 12 and ahole 20 b for inserting the drivenshaft 29, these twoholes 20 a and 20 b being located adjacently. The diameter of the hole 20 a is set larger than the diameter of thedrive shaft 12. Therefore, a clearance is provided between thedrive shaft 12 and the hole 20 a. The diameter of thehole 20 b is set larger than the diameter of the drivenshaft 29. Therefore, a clearance is provided between the drivenshaft 29 and thehole 20 b. - The
side plate 20 has acommunication passage 43 for connecting thedownstream passage 41 of the first-stage gear train 36 to theupstream passage 42 of the second-stage gear train 37. Thecommunication passage 43 includes afirst passage 43 a, asecond passage 43 b, and athird passage 43 c. Thefirst passage 43 a extends in the radial direction of thepump 1. Thesecond passage 43 b extends in the axial direction of thepump 1 from thedownstream passage 41 of the first-stage gear train 36 and communicates with thefirst passage 43 a. Thethird passage 43 c extends in the axial direction of thepump 1 from theupstream passage 42 of the second-stage gear train 37 and communicates with thefirst passage 43 a. Therefore, the DME, the pressure of which has been increased by the first-stage gear train 36, passes through thesecond passage 43 b, thefirst passage 43 a, and thethird passage 43 c in that order from thedownstream passage 41 and is sent to theupstream passage 42 of the second-stage gear train 37. - The second-
stage gear train 37 has a plurality of high-pressure pump chambers stage gear train 37 is conveyed to thedischarge port 39 a through thepump chambers pump chambers 37 a is defined by the twoadjacent teeth 27 a of thesecond drive gear 27 and the inner circumferential surface of the corresponding hole in theconnection plate 19. Each of thepump chambers 37 b is defined by the twoadjacent teeth 33 a of the second drivengear 33 and the inner circumferential surface of the corresponding hole in theconnection plate 19. The DME, which has been sent to thedischarge port 39 a after the pressure thereof has been increased by the second-stage gear train 37, is supplied to theinjection pump 5 through thedischarge pipe 4. That is, thepump section 11 discharges fluid that has been drawn into a fluid conveying passage, which includes thepump chambers 36 a to 37 b, from the fluid conveying passage through thepump chambers 36 a to 37 b. The pressure at the starting point of the fluid conveying passage is the suction pressure of thepump section 11, and the pressure at the endpoint of the fluid conveying passage is the discharge pressure of thepump section 11. - The
lid 9 is fitted with apipe connecting portion 54. Thepipe connecting portion 54 is connected with aleak pipe 55 extending from the tank 2 (see FIG. 4). Thepipe connecting portion 54 has aleak port 56 for connecting the internal space of therecess 61 to theleak pipe 55. Themotor housing 10 a has acommunication hole 65 for connecting the internal space of therecess 61 to themotor chamber 60. The side wall of themotor housing 10 a is provided with avent hole 57 for connecting themotor chamber 60 to the upper space of thesub tank 7 a. - The sliding portions in the
motor section 10 and the sliding portions in thepump section 11, for example, thegears sub tank 7 a and the DME leaking from thegear trains motor chamber 60 may be vaporized. In this embodiment, the interior of thepump 1 is sealed from the outside. In other words, thepump 1 incorporating themotor 10 is of a shaft enclosed type in which thedrive shaft 12 is sealed in thecasing 7 and thelid 9. In the shaftenclosed type pump 1, the vaporized DME is possibly accumulated in thesub tank 7 a or themotor chamber 60. However, the vaporized DME in thesub tank 7 a moves to themotor chamber 60 through thevent hole 57, and the vaporized DME in themotor chamber 60 is returned to thetank 2 through thecommunication hole 65, the internal space of therecess 61, theleak port 56, and theleak pipe 55 in that order. Therefore, the occurrence of troubles, such as insufficient cooling of themotor section 10 caused by the filling of evaporated DME, is prevented. - In the
pump section 11, aninternal space 51 is present around acylindrical surface 12 b of thedrive shaft 12 at a position adjacent to the drive gears 26 and 27. Theinternal space 51 includes afirst space 51 a, asecond space 51 b, and athird space 51 c. Thefirst space 51 a is located between thefirst drive gear 26 and thebearing 14. Thefirst space 51 a is a part of therecess 62 provided in the tip-end plate 22. Thesecond space 51 b is located between the drive gears 26 and 27. Thethird space 51 c is located on the upper side of thesecond drive gear 27. In thedrive shaft 12, the diameter of a portion ranging from a midway point of thebase block 16 to the lower end of thedrive shaft 12 is smaller than that of the upper portion. Between this small-diameter portion on the lower end side of thedrive shaft 12 and thebase block 16, thethird space 51 c is located. - The
first space 51 a and thesecond space 51 b are connected to each other by some gap around the key 25 and thegroove 12 a. Similarly, thesecond space 51 b and thethird space 51 c are connected to each other by some gap around the key 25 and thegroove 12 a. As necessary, a communication passage for connecting thefirst space 51 a to thesecond space 51 b may be formed in thefirst drive gear 26, or a communication passage for connecting thesecond space 51 b to thethird space 51 c may be formed in thesecond drive gear 27. - In the
recess 62 in the tip-end plate 22, aspace 62 a is present on the lower end face of thedrive shaft 12 beyond thebearing 14. Thespace 62 a is connected to thefirst space 51 a through a gap that thebearing 14 has. Thethird space 51 c is connected to themotor chamber 60 through a gap between thebase block 16 and the large-diameter portion of thedrive shaft 12, that is, acommunication hole 76. As described above, the internal space of therecess 61 of themotor housing 10 a is connected to themotor chamber 60 through thecommunication hole 65 in themotor housing 10 a. Specifically, aspace 61 a, in which the upper end face of thedrive shaft 12 is exposed, is connected to themotor chamber 60 through thecommunication hole 65. - Therefore, the pressure atmosphere of the
space 61 a exposed to the upper end face of thedrive shaft 12 and the pressure atmosphere of thespace 62 a exposed to the lower end face of thedrive shaft 12 are the same as the pressure atmosphere of themotor chamber 60. The pressure in themotor chamber 60 is approximately equal to the suction pressure of thepump section 11. Therefore, the force based on the pressure in therecess 61, which is applied to the upper end face of thedrive shaft 12, and the force based on the pressure in therecess 62, which is applied to the lower end face of thedrive shaft 12, are balanced. As a result, opposing thrust loads applied to thedrive shaft 12 due to the imbalance of the pressure in therecess 61 and the pressure in therecess 62 cancel each other, so that the thrust load borne by thebearing 13 is alleviated, whereby the durability of thebearing 13 is enhanced. - Also, the pressure atmosphere of the
first space 51 a is the same as the pressure atmosphere of thesecond space 51 b located adjacently to thefirst space 51 a with thefirst drive gear 26 being held therebetween. Therefore, the opposing thrust loads applied to thefirst drive gear 26 due to the imbalance of the pressure in thefirst space 51 a and the pressure in thesecond space 51 b cancel each other. As a result, wear and other types of impairment of thefirst drive gear 26 are prevented. Similarly, the pressure atmosphere of thesecond space 51 b is the same as the pressure atmosphere of thethird space 51 c located adjacently to thesecond space 51 b with thesecond drive gear 27 being held therebetween. Therefore, opposing thrust loads applied to thesecond drive gear 27 due to the imbalance of the pressure in thethird space 51 c and the pressure in thesecond space 51 b cancel each other. As a result, wear and other types of impairment of thesecond drive gear 27 are prevented. - In the
pump section 11, aninternal space 52 is present around acylindrical surface 29 a of the drivenshaft 29 at a position adjacent to the driven gears 32 and 33. Theinternal space 52 includes afirst space 52 a, asecond space 52 b, and athird space 52 c. Thefirst space 52 a is located between the first drivengear 32 and thebearing 31. That is, thefirst space 52 a is a part of therecess 64 provided in the tip-end plate 22. Thesecond space 52 b is located between the driven gears 32 and 33. Thethird space 52 c is located between the second drivengear 33 and thebearing 30. That is, thethird space 52 c is a part of therecess 63 provided in thebase block 16. - The
first space 52 a and thesecond space 52 b are connected to each other by some gap between the first drivengear 32 and thecylindrical surface 29 a of the drivenshaft 29. In therecess 64 in the tip-end plate 22, aspace 64 a is present on the lower end face of the drivenshaft 29. Thespace 64 a is connected to thefirst space 52 a through a gap that thebearing 31 has. In therecess 63 in thebase block 16, aspace 63 a is present on the upper end face of the drivenshaft 29. Thespace 63 a is connected to thethird space 52 c through a gap that thebearing 30 has. Thespace 63 a exposed to the upper end face of the drivenshaft 29 in thebase block 16 is connected to thespace 64 a exposed to the lower end face of the drivenshaft 29 in the tip-end plate 22 through an in-shaft passage 66 formed in the drivenshaft 29. The in-shaft passage 66 extends along the axis of the drivenshaft 29. - Therefore, the pressure atmosphere of the
space 63 a exposed to the upper end face of the drivenshaft 29 is the same as the pressure atmosphere of thespace 64 a exposed to the lower end face of the drivenshaft 29. Therefore, the force based on the pressure in therecess 63, which is applied to the upper end face of the drivenshaft 29, and the force based on the pressure in therecess 64, which is applied to the lower end face of the drivenshaft 29, are balanced. As a result, a thrust load applied to the drivenshaft 29 due to the imbalance of the two forces is canceled. Further, the pressure atmosphere of thesecond space 52 b is the same as the pressure atmosphere of thethird space 52 c located adjacently to thesecond space 52 b with the second drivengear 33 being held therebetween. Therefore, opposing thrust loads applied to the second drivengear 33, which are a thrust load due to the imbalance of pressure in thesecond space 52 b and pressure in thethird space 52 c and a thrust load due to the imbalance of pressure in therecess 63 and pressure in therecess 64, cancel each other. As a result, wear and other types of impairment of the second drivengear 33 are prevented. - Also, the pressure atmosphere of the
first space 52 a is the same as the pressure atmosphere of thesecond space 52 b located adjacently to thefirst space 52 a with the first drivengear 32 being held therebetween. Therefore, opposing thrust loads applied to the first drivengear 32 due to the imbalance of the pressure in thefirst space 52 a and the pressure in thesecond space 52 b cancel each other. As a result, wear and other types of impairment of the first drivengear 32 are prevented. - The pressure in the
communication passage 43 for connecting the first-stage gear train 36 to the second-stage gear train 37 is equal to the discharge pressure of the first-stage gear train 36, in other words, the suction pressure of the second-stage gear train 37. Specifically, the pressure in thecommunication passage 43 is higher than the suction pressure of the first-stage gear train 36, i.e., the suction pressure of thepump section 11, and is lower than the discharge pressure of the second-stage gear train 37, i.e., the discharge pressure of thepump section 11. In other words, it can be said that the pressure atmosphere of thecommunication passage 43 is the pressure atmosphere of intermediate pressure of thepump section 11. In this embodiment, thecommunication passage 43 functions as an intermediate-pressure zone. - As shown in FIGS. 1A and 3, the
side plate 20 has apressure introduction passage 67. Thepressure introduction passage 67 connects thefirst passage 43 a of thecommunication passage 43 to thesecond space 52 b of theinternal space 52, which is close to the drivenshaft 29. The intermediate pressure in thecommunication passage 43 is introduced to thesecond space 52 b through thepressure introduction passage 67. As described above, thesecond space 52 b is connected to the internal space of therecess 64 in the tip-end plate 22, that is, to thefirst space 52 a and thespace 64 a. The internal space of therecess 64 is connected to thethird space 52 c. Therefore, the pressure atmosphere of theinternal space 52 around thecylindrical surface 29 a of the drivenshaft 29, the pressure atmosphere of thespace 63 a exposed to the upper end face of the drivenshaft 29, and the pressure atmosphere of thespace 64 a exposed to the lower end face of the drivenshaft 29 are the same as the pressure atmosphere of thecommunication passage 43, i.e., the pressure atmosphere of intermediate pressure of thepump section 11. - This embodiment having the above-described configuration has the following advantages.
- (1) The pressure atmosphere of the
internal space 52, which is close to the drivenshaft 29 of thepump section 11, is the pressure atmosphere of intermediate pressure of thepump section 11. Therefore, for example, when compared with the case where the pressure atmosphere of theinternal space 52 is the same as the suction pressure or the discharge pressure of thepump section 11, the maximum value of difference in pressure produced between thepump chambers shaft 29 and theinternal space 52 is decreased. - Thereupon, for example, when compared with the case where the pressure in the
internal space 52 is equal to the suction pressure of thepump section 11, the leakage of DME from the high-pressure pump chambers 37 b to theinternal space 52 is decreased. Also, for example, when compared with the case where the pressure in theinternal space 52 is equal to the discharge pressure of thepump section 11, the leakage of DME from theinternal space 52 to the low-pressure pump chambers 36 b is decreased. As a result, the efficiency of thepump 1 is improved in total. - Since the leakage of DME between the
pump chambers shaft 29 and theinternal space 52 is decreased without the use of a sealing member as described above, the size of thepump 1 is made small. Therefore, thepump 1 of this embodiment is suitable as a pump mounted on a vehicle. - (2) According to this embodiment, in the
pump section 11, theinternal space 52 is connected to thecommunication passage 43, which functions as an intermediate-pressure zone, via thepressure introduction passage 67. Therefore, theinternal space 52 is made to have a pressure atmosphere of intermediate pressure by a simple construction such as thepressure introduction passage 67. - (3) The
communication passage 43 connecting the discharge side of the first-stage gear train 36 to the suction side of the second-stage gear train 37 forms an intermediate-pressure zone. For example, when compared with the intermediate pressure in the case where the low-pressure pump chambers stage gear train 36 function as intermediate-pressure zones, a high pressure, which is the discharge pressure of the first-stage gear train 36, is introduced to theinternal space 52. Therefore, the maximum difference in pressure produced between thepump chambers internal space 52 is further decreased. As a result, the efficiency of thepump 1 is further improved. - Also, for example, when compared with the case where an intermediate-pressure zone is set in the
pump chambers pressure introduction passage 67 is simple, which is advantageous in decreasing the size of thepump 1. - As shown in FIG. 5, in a second embodiment, a
shaft seal device 71 is provided between thebase block 16 and thedrive shaft 12. Theshaft seal device 71 disconnects themotor chamber 60 from thethird space 51 c of theinternal space 51 in thepump section 11. Theshaft seal device 71 includes, for example, a lip type seal. Theside plate 20 has apressure introduction passage 72. Thepressure introduction passage 72 connects thefirst passage 43 a of thecommunication passage 43 to thesecond space 51 b of theinternal space 51. - Therefore, the intermediate pressure of the
communication passage 43 is introduced to thesecond space 51 b of theinternal space 51 through thepressure introduction passage 72. That is to say, the pressure atmosphere of theinternal space 51 around thecylindrical surface 12 b of thedrive shaft 12 and the pressure atmosphere of thespace 62 a exposed to the lower end face of thedrive shaft 12 are the same as the pressure atmosphere of intermediate pressure of thepump section 11. - In this embodiment, therefore, the maximum difference in pressure produced between the
pump chambers drive shaft 12, and theinternal space 51 is also decreased. As a result, in the relationship between thepump chambers internal space 51 close to thedrive shaft 12 as well, as in the case of the above-described first embodiment, that is, as in the relationship between thepump chambers internal space 52 close to the drivenshaft 29, an effect of decreasing DME leakage is achieved. Since the leakage of DME is decreased in both of the relationship between thepump chambers internal space 51 close to thedrive shaft 12 and the relationship between thepump chambers internal space 52 close to the drivenshaft 29, the efficiency of thepump 1 is further improved. - As shown in FIG. 6, in a third embodiment, the
vent hole 57 in themotor housing 10 a and thepressure introduction passage 67 in theside plate 20 are eliminated from the above-described first embodiment. Thespace 63 a (see FIG. 1A) exposed to the upper end face of the drivenshaft 29 in therecess 63 is connected to themotor chamber 60 through acommunication hole 75 penetrating thebase block 16. Thethird space 51 c (see FIG. 1A) of theinternal space 51 close to thedrive shaft 12 is connected to themotor chamber 60 through the gap between thebase block 16 and the large-diameter portion of thedrive shaft 12, that is, thecommunication hole 76. Therefore, the pressure atmosphere of theinternal spaces motor chamber 60. - At a midway point of the
leak port 56 in thepipe connecting portion 54, apressure regulating valve 77 is disposed. Thepressure regulating valve 77 is a differential pressure regulating valve including avalve element 77 a and an urgingspring 77 b. Thepressure regulating valve 77 opens and closes theleak port 56 according to a difference between the pressure on themotor chamber 60 side applied to thevalve element 77 a and the pressure on the tank 2 (see FIG. 4) side similarly applied to thevalve element 77 a. - The high-
pressure pump chambers internal spaces internal spaces motor chamber 60 is increased due to the leakage of DME from thepump chambers motor chamber 60. If the pressure in theinternal spaces motor chamber 60 becomes higher than a predetermined value, thevalve element 77 a of thepressure regulating valve 77 moves in the valve opening direction against the urging force in the valve closing direction generated by the urgingspring 77 b and a force in the valve closing direction generated by the pressure in the section connected to thetank 2. Thus, thevalve element 77 a releases theleak port 56. Therefore, the pressure in theinternal spaces motor chamber 60 tends to be decreased by the sending-out of pressure to thetank 2 through theleak port 56, so that the pressure returns to the aforementioned predetermined value. - In a state in which the
leak port 56 is open, if the pressure in theinternal spaces motor chamber 60 becomes lower than the predetermined value, thevalve element 77 a of thepressure regulating valve 77 is moved in the valve closing direction by the urging force in the valve closing direction of the urgingspring 77 b and a force in the valve closing direction generated by the pressure of the section connected to thetank 2, so that theleak port 56 is closed. Therefore, the pressure in theinternal spaces motor chamber 60 tends to be increased by the leakage and vaporization of DME, so that the pressure returns to the aforementioned predetermined value. - That is to say, the
pressure regulating valve 77 opens and closes theleak port 56 autonomously so as to keep the pressure in theinternal spaces motor chamber 60 at the predetermined value. The construction of thepressure regulating valve 77 of an autonomous type is simpler than that of a pressure regulating valve of, for example, an external control type. The aforementioned predetermined value, that is, the target of regulation of the pressure in theinternal spaces motor chamber 60 accomplished by thepressure regulating valve 77 is set to the intermediate pressure of thepump section 11 in the steady-state operating condition, for example, to the discharge pressure of the first-stage gear train 36. The setting of the pressure regulation target is concretely performed by the adjustment of the spring force of the urgingspring 77 b. Therefore, as in the case of the above-described second embodiment, theinternal spaces pump section 11. Therefore, the leakage of DME between thepump chambers internal space - In this embodiment, the target value of the pressure in the
internal spaces pressure regulating valve 77, for example, the spring force of the urgingspring 77 b. Therefore, the pressure in theinternal spaces internal spaces pressure introduction passages - The pressure leakage from the
pump section 11 is an inevitable phenomenon. The pressure leakage tends to increase the pressure in theinternal spaces internal spaces internal spaces pump section 11. Unlike thepump 1 of the second embodiment, in thepump 1 of this embodiment, theinternal spaces motor chamber 60. In thepump 1 of this embodiment, in which theinternal spaces motor chamber 60 communicate with each other, the DME leaking from, for example, from the second-stage gear train 37 is positively supplied to themotor chamber 60 through theinternal spaces motor section 10 is cooled properly by the liquid DME supplied to themotor chamber 60. Thereby, the operation of themotor section 10 is stabilized. - In this embodiment, the communication holes75 and 76, the
motor chamber 60, thecommunication hole 65, the internal space of therecess 61, theleak port 56, and the leak pipe 55 (see FIG. 4) function as a pressure regulation passage that connects thetank 2 functioning as a low-pressure zone to theinternal spaces - As shown in FIG. 7, in the
pump 1 in accordance with a fourth embodiment, thepump 1 of the above-described third embodiment is changed. Specifically, the upstream-side of theleak port 56 of thepipe connecting portion 54 is connected to the upper space of thesub tank 7 a. Thelid 9 has aninternal passage 79 for connecting the internal space of therecess 61 to the upper space of thesub tank 7 a. The vaporized DME in themotor chamber 60 is discharged through thecommunication hole 65, the internal space of therecess 61, and theinternal passage 79, and is returned to thetank 2 through theleak port 56 and theleak pipe 55 together with the DME vaporized in thesub tank 7 a. - In the
internal passage 79, thepressure regulating valve 77 is disposed to regulate the pressure in themotor chamber 60 so as to be an intermediate pressure by the same operation as that in the above-described third embodiment. In this embodiment, thesub tank 7 a functions as a low-pressure zone. The communication holes 75 and 76, themotor chamber 60, thecommunication hole 65, the internal space of therecess 61, and theinternal passage 79 function as a pressure regulation passage that connects theinternal spaces sub tank 7 a. - As shown in FIG. 8, in a fifth embodiment, the above-described third embodiment is changed. Specifically, the
motor section 10 is arranged at the lower part (right-hand side as viewed in FIG. 8) of thecasing 7, and thepump section 11 is arranged at the upper part (left-hand side as viewed in FIG. 8) of thecasing 7. That is to say, thepump 1 is mounted on a vehicle in a state in which thepump section 11 is at the upper position and themotor section 10 is at the lower position. - By this configuration, the
pump section 11 and thedischarge connecting portion 39 installed to thelid 9 are arranged so as to be close to each other. Therefore, the first pump section internal passage (not shown) for connecting thepump section 11 to thedischarge connecting portion 39 is laid out easily, which is advantageous in decreasing the size of thepump 1. Also, since themotor section 10 is arranged at the lower part of thecasing 7, the liquid level of DME in themotor chamber 60 is surely located at the upper part of themotor chamber 60. Therefore, thestators 10 b and therotor 10 c are less liable to be exposed above the liquid level of DME, so that they are cooled properly by DME (liquid). - In this embodiment, the upstream-side of the
leak port 56 is connected to the internal space of therecess 62 in the tip-end plate 22. Theleak port 56 and themotor chamber 60 are connected to each other through theinternal space 51 close to thedrive shaft 12 and thecommunication hole 76. Therefore, the vaporized DME in themotor chamber 60 is discharged into thetank 2 through thecommunication hole 76, theinternal space 51, theleak port 56, and the leak pipe 55 (see FIG. 4). - The pressure in the
internal space 51 tends to be increased under the influence of DME leakage from the high-pressure pump chambers motor chamber 60. On the other hand, the pressure in theinternal space 51 is released into thetank 2 through theleak port 56 and theleak pipe 55. Thepressure regulating valve 77 regulates the pressure in theinternal space 51 so as to be the intermediate pressure of thepump section 11 by regulating the opening of theleak port 56 and the degree of sending-out of pressure from theinternal space 51. - In this embodiment, the
communication hole 75 is eliminated. That is to say, theinternal space 52 close to the drivenshaft 29 is isolated from themotor chamber 60. However, theinternal space 52 is connected to thecommunication passage 43 between thegear trains pressure introduction passage 67. That is to say, theinternal space 52 close to the drivenshaft 29 is made to have a pressure atmosphere of intermediate pressure of thepump section 11 by the same method as that in the above-described first embodiment. - In this embodiment, the pressure in the
internal space 51 close to thedrive shaft 12 is regulated directly by thepressure regulating valve 77. Contrarily, for example, in the above-described third embodiment, the pressure in themotor chamber 60 is regulated directly, and resultantly the pressure in themotor chamber 60 is reflected to the pressure in theinternal space 51. In this embodiment, therefore, when compared with the above-described third embodiment, the operation of thepressure regulating valve 77 is immediately reflected to the pressure in theinternal space 51. Therefore, the pressure in theinternal space 51 is further stabilized. As a result, the leakage of DME between the low-pressure pump chambers 36 a, the high-pressure pump chamber 37 a and theinternal space 51 close to thedrive shaft 12 is restrained more effectively. - In this embodiment, the internal space of the
recess 62, theleak port 56, and the leak pipe 55 (see FIG. 4) function as a pressure regulation passage that connects theinternal space 51 to thetank 2. - The invention may be embodied in the following forms.
- By changing the above-described first or second embodiment, in the first-
stage gear train 36 or the second-stage gear train 37, thepump chambers internal space 51 is connected to the intermediate-pressure zone through the pressure introduction passage. In the case of the modification of the second embodiment, theinternal spaces - In the above-described second embodiment, the
pressure introduction passage 67 is eliminated. That is to say, only theinternal space 51 is made to have the intermediate pressure. - In the above-described third to fifth embodiments, the
pressure regulating valve 77 is of an autonomous type (differential pressure regulating valve). By changing this, a valve of an external control type, such as a solenoid valve, is used as a pressure control valve. In this case, the modification of the third to fifth embodiments is provided with a pressure sensor and control means (described below). The pressure sensor detects the pressure in the correspondinginternal spaces internal spaces internal spaces internal spaces - In the above-described embodiments, the invention is embodied in the
pump 1 of a type such as to be mounted outside thetank 2. By changing this, the invention is embodied in a gear pump of what is called an in-tank type, which is contained in thetank 2. In this case, thecasing 7 is eliminated. - The fluid handled by the gear pump is not limited to DME. The invention may be embodied in a gear pump that handles a liquid (gas) other than DME.
- In the above-described embodiments, the invention is embodied in the two-stage gear pump. However, the invention is not limited to the gear pump of this type. The invention may be embodied in the gear pump of a plurality of stages other than two stages, such as three stages or four stages. Alternatively, the invention may be embodied in a one-stage gear pump.
- In the above-described embodiments, the gear pump is of a shaft enclosed type, i.e., a type such that the motor is incorporated. However, the gear pump may be of a shaft open type, i.e., a type such that the pump section is driven by an external motor.
- The gear pump in accordance with the present invention is not limited to a vehicular gear pump that sends a liquefied gas fuel under pressure to an internal combustion engine. The present invention may be applied to a gear pump used to send hydraulic fluid etc. under pressure, for example, in a machine tool.
- The present examples and embodiments are to be considered as illustrative and not restrictive and the invention is not to be limited to the details given herein, but may be modified within the scope and equivalence of the appended claims.
Claims (13)
1. A gear pump for sending fluid under pressure, the gear pump comprising a pump section that draws fluid and discharges pressurized fluid, wherein the pump section includes:
a gear train having a pair of meshed gears, wherein each gear defines a plurality of pump chambers for conveying fluid in the pump section;
a drive shaft having a cylindrical surface, wherein one of the gears is coupled to the drive shaft such that the gear rotates integrally with the drive shaft; and
a driven shaft having a cylindrical surface, wherein the driven shaft supports the other one of the gears,
wherein the pump section has an internal space that is located at a position adjacent to at least one of the gears and about the cylindrical surface of at least one of the drive shaft and the driven shaft, and wherein the pressure atmosphere of the internal space is an intermediate pressure atmosphere of the pressure of fluid drawn into the pump section and the pressure of fluid discharged from the pump section.
2. The gear pump according to claim 1 , wherein the pump section has a fluid conveying passage that includes the pump chambers, wherein the pump section discharges fluid drawn into the fluid conveying passage from the fluid conveying passage through the pump chambers, wherein the fluid conveying passage has an intermediate-pressure zone, the pressure atmosphere of which is an intermediate pressure atmosphere of the pressure of fluid drawn into the fluid conveying passage and the pressure of fluid discharged from the fluid conveying passage, and wherein the pump section has a pressure introduction passage that connects the internal space with the intermediate-pressure zone.
3. The gear pump according to claim 2 , wherein the gear train is one of a plurality of gear trains that include at least a first gear train and a second gear train, wherein the fluid conveying passage includes a communication passage for guiding fluid discharged from the first gear train to the second gear train, and wherein the communication passage functions as the intermediate-pressure zone.
4. The gear pump according to claim 1 , further comprising a pressure regulating valve, wherein the pressure regulating valve is capable of releasing the pressure of the internal space, thereby adjusting the pressure of the internal space to an intermediate pressure of the pressure of fluid drawn into the pump section and the pressure of fluid discharged from the pump section.
5. The gear pump according to claim 4 , wherein the pump section has a fluid conveying passage that includes the pump chambers, wherein the pump section discharges fluid drawn into the fluid conveying passage from the fluid conveying passage through the pump chambers, wherein the fluid conveying passage has a high-pressure zone, the internal pressure of which is higher than the pressure of the internal space, and wherein the pressure regulating valve prevents the pressure of the internal space from being increased due to pressure leakage from the high-pressure zone to the internal space.
6. The gear pump according to claim 4 , wherein the internal space is connected to a tank with a pressure regulation passage, the tank storing fluid that is supplied to the pump section, and wherein the pressure regulating valve is located in the pressure regulation passage.
7. The gear pump according to claim 6 , further comprising:
a housing for accommodating the pump section; and
a sub tank, wherein the sub tank stores in the housing fluid supplied from the tank to supply the fluid to the pump section,
wherein the sub tank is provided in a section of the pressure regulating passage that is located between the pressure regulating valve and the tank.
8. The gear pump according to claim 6 , further comprising:
a motor for rotating the drive shaft; and
a housing for accommodating the pump section and the motor,
wherein the pump section has a gear housing for accommodating the gears, and
wherein the pump section is located between the pressure regulating valve and the motor, and wherein the gear housing has a passage for connecting the internal space with the pressure regulating valve.
9. The gear pump according to claim 1 , further comprising:
a motor for rotating the drive shaft; and
a housing for accommodating the pump section and the motor.
10. The gear pump according to claim 1 , wherein the internal space is one of a pair of internal spaces that are defined about the cylindrical surface of the drive shaft and about the cylindrical surface of the driven shaft, respectively, and wherein the pressure atmosphere of each internal space is an intermediate pressure atmosphere of the pressure of fluid drawn into the pump section and the pressure of fluid discharged from the pump section.
11. The gear pump according to claim 1 , wherein the fluid is liquefied gas fuel.
12. The gear pump according to claim 1 , wherein the gear pump is mounted on a vehicle.
13. A gear pump for sending fluid under pressure, the gear pump comprising a pump section that draws fluid and discharges pressurized fluid, wherein the pump section includes:
a plurality of gear trains that include at least a first gear train and a second gear train, wherein each gear train has a pair of meshed gears, wherein each gear defines a plurality of pump chambers for conveying fluid in the pump section;
a drive shaft having a cylindrical surface, wherein one of the gears of each gear train is coupled to the drive shaft such that the gear rotates integrally with the drive shaft;
a driven shaft having a cylindrical surface, wherein the driven shaft supports the other one of the gears of each gear train; and
a fluid conveying passage that includes the pump chambers, wherein the fluid conveying passage includes a communication passage for guiding fluid discharged from the first gear train to the second gear train,
wherein the pump section discharges fluid drawn into the fluid conveying passage from the fluid conveying passage through the pump chambers, wherein the pump section has an internal space that is located at a position adjacent to at least one of the gears and about the cylindrical surface of at least one of the drive shaft and the driven shaft, and wherein the pump section has a pressure introduction passage that connects the internal space with the communication passage.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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JP2003069529A JP2004278381A (en) | 2003-03-14 | 2003-03-14 | Gear pump |
JP2003-069529 | 2003-03-14 |
Publications (1)
Publication Number | Publication Date |
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US20040179953A1 true US20040179953A1 (en) | 2004-09-16 |
Family
ID=32767976
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US10/798,136 Abandoned US20040179953A1 (en) | 2003-03-14 | 2004-03-10 | Gear pump |
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US (1) | US20040179953A1 (en) |
EP (1) | EP1457678A1 (en) |
JP (1) | JP2004278381A (en) |
CN (1) | CN1299002C (en) |
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US9611847B2 (en) | 2009-04-16 | 2017-04-04 | Eaton Industrial Corporation | Aircraft main engine fuel pump with multiple gear stages using shared journals |
US20180072147A1 (en) * | 2016-01-26 | 2018-03-15 | Deere & Company | Recess-mounted hydraulic pump cartridge and work vehicle drivetrain therewith |
US10905973B2 (en) | 2013-02-27 | 2021-02-02 | C.C. Jensen A/S | Device for processing a liquid under vacuum pressure |
US11466649B2 (en) * | 2017-12-13 | 2022-10-11 | Robert Bosch Gmbh | Pumping unit for feeding fuel, preferably diesel fuel, to an internal combustion engine |
US20220403843A1 (en) * | 2021-06-22 | 2022-12-22 | Fte Automotive Gmbh | Gear pump and drive machine |
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JP2007315238A (en) * | 2006-05-24 | 2007-12-06 | Toyota Industries Corp | Gear pump |
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IT201600125212A1 (en) | 2016-12-12 | 2018-06-12 | Bosch Gmbh Robert | GEAR ELECTRIC PUMP |
IT201600129613A1 (en) * | 2016-12-21 | 2018-06-21 | Bosch Gmbh Robert | GEAR ELECTRIC PUMP |
IT201600130203A1 (en) * | 2016-12-22 | 2018-06-22 | Bosch Gmbh Robert | GEAR ELECTRIC PUMP |
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US20030012664A1 (en) * | 2001-05-17 | 2003-01-16 | Eugen Maier | Multi-stage internal gear fuel pump |
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GB8513684D0 (en) * | 1985-05-30 | 1985-07-03 | Boc Group Plc | Mechanical pumps |
JPH0914154A (en) * | 1995-06-26 | 1997-01-14 | Shimadzu Corp | Gear pump or motor |
JP3932595B2 (en) * | 1997-03-12 | 2007-06-20 | 株式会社日立製作所 | Gear pump |
JP3688535B2 (en) * | 1999-11-17 | 2005-08-31 | 上田鉄工株式会社 | Gear pump |
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2004
- 2004-03-10 US US10/798,136 patent/US20040179953A1/en not_active Abandoned
- 2004-03-11 EP EP04005946A patent/EP1457678A1/en not_active Withdrawn
- 2004-03-12 CN CNB2004100352327A patent/CN1299002C/en not_active Expired - Fee Related
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US20030012664A1 (en) * | 2001-05-17 | 2003-01-16 | Eugen Maier | Multi-stage internal gear fuel pump |
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US20070201989A1 (en) * | 2005-10-14 | 2007-08-30 | Parker-Hannifin | Low ripple gear pump/motor |
US9611847B2 (en) | 2009-04-16 | 2017-04-04 | Eaton Industrial Corporation | Aircraft main engine fuel pump with multiple gear stages using shared journals |
US20100266437A1 (en) * | 2009-04-16 | 2010-10-21 | Argo-Tech Corporation | Aircraft main engine fuel pump with multiple gear stages using shared journals |
US20110247454A1 (en) * | 2010-04-07 | 2011-10-13 | Gm Global Technology Operations, Inc. | Evacuated transmission case |
US9032840B2 (en) * | 2010-04-07 | 2015-05-19 | Gm Global Technology Operations, Llc | Evacuated transmission case |
US20140169995A1 (en) * | 2011-12-28 | 2014-06-19 | Kayaba Industry Co., Ltd | Electric oil pump |
US9581159B2 (en) * | 2011-12-28 | 2017-02-28 | Kyb Corporation | Electric oil pump |
US20150059328A1 (en) * | 2012-03-29 | 2015-03-05 | Kayaba Industry Co., Ltd. | Fluid pressure drive unit |
US20150064030A1 (en) * | 2012-03-29 | 2015-03-05 | Kayaba Industry Co., Ltd. | Fluid pressure drive unit |
US10905973B2 (en) | 2013-02-27 | 2021-02-02 | C.C. Jensen A/S | Device for processing a liquid under vacuum pressure |
US10415566B2 (en) * | 2014-10-16 | 2019-09-17 | Johnson Electric International AG | Gear pump |
US20160108914A1 (en) * | 2014-10-16 | 2016-04-21 | Johnson Electric S.A. | Gear pump |
US10612545B2 (en) | 2014-10-16 | 2020-04-07 | Johnson Electric International AG | Gear pump |
CN104361261A (en) * | 2014-12-08 | 2015-02-18 | 中国人民解放军防化学院 | Gear pump health state evaluation method based on profust reliability theory |
US20180072147A1 (en) * | 2016-01-26 | 2018-03-15 | Deere & Company | Recess-mounted hydraulic pump cartridge and work vehicle drivetrain therewith |
US10919376B2 (en) * | 2016-01-26 | 2021-02-16 | Deere & Company | Recess-mounted hydraulic pump cartridge and work vehicle drivetrain therewith |
US11466649B2 (en) * | 2017-12-13 | 2022-10-11 | Robert Bosch Gmbh | Pumping unit for feeding fuel, preferably diesel fuel, to an internal combustion engine |
US20220403843A1 (en) * | 2021-06-22 | 2022-12-22 | Fte Automotive Gmbh | Gear pump and drive machine |
US12305638B2 (en) * | 2021-06-22 | 2025-05-20 | Valeo Powertrain Gmbh | Gear pump and drive machine |
Also Published As
Publication number | Publication date |
---|---|
CN1299002C (en) | 2007-02-07 |
EP1457678A1 (en) | 2004-09-15 |
CN1534195A (en) | 2004-10-06 |
JP2004278381A (en) | 2004-10-07 |
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