US20040247455A1 - Piston compressor - Google Patents
Piston compressor Download PDFInfo
- Publication number
- US20040247455A1 US20040247455A1 US10/808,831 US80883104A US2004247455A1 US 20040247455 A1 US20040247455 A1 US 20040247455A1 US 80883104 A US80883104 A US 80883104A US 2004247455 A1 US2004247455 A1 US 2004247455A1
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- Prior art keywords
- gasket
- hole
- imaginary circle
- cylinder block
- radius
- 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
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- 238000005452 bending Methods 0.000 claims abstract description 34
- 230000006835 compression Effects 0.000 claims description 14
- 238000007906 compression Methods 0.000 claims description 14
- 239000003507 refrigerant Substances 0.000 claims description 10
- 230000010354 integration Effects 0.000 claims 4
- 230000009471 action Effects 0.000 description 8
- 230000007246 mechanism Effects 0.000 description 6
- 238000007789 sealing Methods 0.000 description 6
- 238000004891 communication Methods 0.000 description 4
- 230000002093 peripheral effect Effects 0.000 description 4
- 230000004308 accommodation Effects 0.000 description 3
- 230000003247 decreasing effect Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- GVGLGOZIDCSQPN-PVHGPHFFSA-N Heroin Chemical compound O([C@H]1[C@H](C=C[C@H]23)OC(C)=O)C4=C5[C@@]12CCN(C)[C@@H]3CC5=CC=C4OC(C)=O GVGLGOZIDCSQPN-PVHGPHFFSA-N 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 229960002069 diamorphine Drugs 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000452 restraining effect Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B27/00—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
- F04B27/08—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B27/00—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
- F04B27/08—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis
- F04B27/10—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis having stationary cylinders
- F04B27/1036—Component parts, details, e.g. sealings, lubrication
- F04B27/1081—Casings, housings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B27/00—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
- F04B27/08—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis
- F04B27/10—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis having stationary cylinders
- F04B27/1036—Component parts, details, e.g. sealings, lubrication
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B27/00—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders
- F04B27/08—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis
- F04B27/10—Multi-cylinder pumps specially adapted for elastic fluids and characterised by number or arrangement of cylinders having cylinders coaxial with, or parallel or inclined to, main shaft axis having stationary cylinders
- F04B27/1036—Component parts, details, e.g. sealings, lubrication
- F04B27/1045—Cylinders
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/10—Adaptations or arrangements of distribution members
- F04B39/1066—Valve plates
Definitions
- the present invention relates to a piston compressor for a vehicular air conditioner and, more particularly, to a technology for restraining deformation of a cylinder block.
- Japanese Laid-Open Patent Publication No. 8-19160 discloses a gasket 101 as shown in FIG. 13.
- the gasket 101 is used for a piston compressor for a vehicular air conditioner.
- the gasket 101 is formed with a plurality of through holes 103 that substantially coincide with opening edges of cylinder bores 102 each containing a piston, a plurality of insertion holes 105 through which through bolts 104 are inserted, and a center hole 106 through which a drive shaft is inserted.
- a piston compressor provided with this gasket 101 , a piston compressor is known in which as shown in a partially enlarged cross-sectional view of FIG.
- a front housing member 108 is joined to a front end face (left-hand side in the figure) of a cylinder block 107
- a rear housing member 110 is joined to a rear end face (right-hand side in the figure) thereof via a valve plate 109
- these three elements are fastened to each other by the through bolts 104 .
- the gasket 101 is interposed between the cylinder block 107 and the valve plate 109 .
- the cylinder block 107 is formed with the cylinder bores 102 and an accommodation chamber 111 for accommodating a rotary valve for sucking refrigerant gas.
- the accommodation chamber 111 for the rotary valve is formed in the cylinder block 107 as shown in FIG. 15, the accommodation chamber 111 is easily deformed because the rigidity of the cylinder block 107 is low. Therefore, smooth rotation of the rotary valve can be hindered.
- An object of the present invention is to provide a piston compressor in which bending moment acting on a cylinder block is reduced to restrain deformation of the cylinder block, and the motion of a piston and a rotary valve is performed-smoothly to enhance the durability of the piston compressor.
- a piston compressor having a cylinder block, a front housing member, a rear housing member, a through bolt, a plurality of pistons, a drive shaft, and a gasket.
- the cylinder block has a plurality of cylinder bores.
- the cylinder block has two end faces at which the cylinder bores open.
- the front housing member is secured to one of the end faces of the cylinder block.
- the rear housing member is secured to the other one of the end faces of the cylinder block with a valve plate in between.
- the through bolt fastens the cylinder block, the rear housing member, and the front housing.
- Each piston is accommodated and reciprocates in one of the cylinder bores.
- the drive shaft drives the pistons, and is rotatably supported by the cylinder block. Reciprocation of the pistons compress and discharge refrigerant gas.
- the gasket is located between the cylinder block and the valve plate.
- the gasket has a center hole and a plurality of bore holes. Each bore hole is aligned with one of the cylinder bores.
- a first through hole is formed in the gasket to reduce bending moment generated in the cylinder block when the through bolt is fastened.
- the first through hole is located between an adjacent pair of the bore holes and in an imaginary circle.
- the center of the imaginary circle coincides with the center of the bore hole, and the radius of the imaginary circle is a first radius.
- the first radius is the distance from the center of tho gasket to the center of one of the bore holes.
- FIG. 1 is a cross-sectional view of a piston compressor in accordance with a first embodiment of the present invention
- FIG. 2 is a partially cross-sectional view of the compressor shown in FIG. 1;
- FIG. 3 is a front view of a gasket provided in the compressor shown in FIG. 1;
- FIG. 4 is a front view of a conventional gasket used for explanation of the first embodiment
- FIG. 5 is a graph showing a relationship between circumferential lengths of seal portions necessary for function and distances from the gasket center in a gasket;
- FIG. 6 is a graph showing a relationship between circumferential length of seal portions unnecessary for function and distances from the gasket center in a gasket;
- FIG. 7 is a graph showing a total change amount of bending moment generated in a cylinder block
- FIG. 8 is a cross-sectional view of a piston compressor in accordance with a second embodiment
- FIG. 9 is a front view of a gasket provided in the compressor shown in FIG. 8;
- FIG. 10 is a front view of a conventional gasket used for explanation of a second embodiment
- FIG. 11 is a front view of a gasket in a modified embodiment
- FIG. 12 is a front view of a gasket in another modified embodiment
- FIG. 13 is a front view of a prior art gasket
- FIG. 14 is a partially cross-sectional view of a prior art piston compressor.
- FIG. 15 is a partially cross-sectional view of a prior art piston compressor.
- FIGS. 1 to 7 A first embodiment of the present invention will now be described in detail with reference to FIGS. 1 to 7 .
- a front housing member 3 is joined to a front end face of a cylinder block 1 via a gasket 2 , and a crank chamber 4 serving as a control chamber is defined on the inside thereof.
- a rear housing member 6 is joined to a rear end face of the cylinder block 1 via a valve plate 5 , and a discharge chamber 1 arid a suction chamber 8 are defined on the inside thereof.
- a gasket 9 Between the cylinder block 1 and the valve plate 5 is interposed a gasket 9 , and between the valve plate 5 and the rear housing member 6 are interposed a discharge valve forming plate 10 formed integrally with a discharge valve and a retainer forming plate 11 for forming a retainer.
- the cylinder block 1 , the front housing member 3 , and the rear housing member 6 are fastened by through bolts 12 , not shown in FIG. 1.
- a drive shaft 13 is rotatably supported by radial bearings 14 a and 14 b .
- a shaft seal device 15 In a front end portion of the drive shaft 13 is provided a shaft seal device 15 .
- a lug plate 16 is fixed to the drive shaft 13 so as to be integrally rotatable, and a swash plate 17 serving as a cam plate is disposed in a state in which the drive shaft 13 is inserted through a through hole formed in the swash plate 17 .
- a hinge mechanism 18 is interposed between the lug plate 16 and the swash plate 17 .
- the swash plate 17 can be rotated in synchronism with the lug plate 16 and the drive shaft 13 by a hinge connection between the swash plate 17 and the lug plate 16 via the hinge mechanism 18 and the support of the drive shaft 13 , and also can be tilted with respect to the drive shaft 13 while sliding in an axial direction of the drive shaft 13 .
- a plurality of cylinder bores 19 arranged in a circumferential direction in the cylinder block 1 each contain a piston 20 capable of reciprocating. Between each piston 20 and the valve plate 5 , a compression chamber 21 whose volume is changed according to reciprocating motion of the piston 20 is defined. Each piston 20 is engaged with a peripheral edge portion of the swash plate 17 via a pair of shoe 22 . Therefore, rotational motion of the swash plate 17 performed via the lug plate 16 and the hinge mechanism 18 , which is caused by rotation of the drive shaft 13 , is converted to reciprocating motion of the pistons 20 performed via the shoes 22 .
- the lug plate 16 , the swash plate 17 , the hinge mechanism 18 , and the shoes 22 constitute a crank mechanism that converts the rotational motion 1 of the drive shaft 13 to compressive motion for compressing refrigerant gas in the compression chamber 21 .
- a rotary valve accommodating chamber 23 is formed in the cylinder block 1 , and in the rotary valve accommodating chamber 23 , a rotary valve 24 is connected to the drive shaft 13 via a coupling 25 so as to be rotatable in synchronism with the drive shaft 13 .
- a suction passage 26 that always communicates with the suction chamber 8 is formed, and an outlet 27 of the suction passage 26 is open in an outer peripheral surface of the rotary valve 24 .
- communication holes 28 are formed in the cylinder block 1 . Each communication hole corresponds to one of the compression chambers 21 and allows the outlet 27 of the rotary valve 24 to communicate with the corresponding compression chamber 21 .
- FIG. 2 forces acting on the cylinder block 1 in this embodiment are shown in FIG. 2.
- a specific pressure f 1 acts on a front end face of the cylinder block 1 from the front housing member 3 .
- a specific pressure f 2 acts on a rear end face of the cylinder block 1 from the gasket 9 .
- the gasket 9 in this embodiment is shown in FIG. 3.
- the gasket 9 is formed of a rigid base consisting of an iron-base metallic sheet and an elastic layer having sealing ability, such as rubber, with which both surfaces of the base are coated.
- the gasket 9 has a plurality of (six in this embodiment) bore holes 29 that substantially coincide with the opening edges of the cylinder bores 19 and a plurality of (six in this embodiment) bolt holes 30 through which the through bolts 12 are inserted.
- a through hole is formed which corresponds to a center hole 31 (in a circle indicated by dotted line in FIG.
- first through holes 32 and 33 are formed in the conventional gasket and first through holes 32 communicating with each other.
- second through holes 33 are formed between a circle having a radius of a distance Rb from the center of the gasket 9 and a circle having a radius Rc from the center of the gasket 9 .
- the specific pressure f 2 does not act on the cylinder block 1 , so that bending moment is not generated. Because the bending moment is larger at a position closer to the center of the gasket 9 , the provision of the through holes 32 and 33 can reduce the bending moment.
- FIG. 4 shows a conventional gasket 34 formed with bore holes 29 , bolt holes 30 , and a center hole 31 .
- solid line hatched portions are seal portions that are necessary for function of sealing the bore holes 29 , the bolt holes 30 , and the interior of the compressor. That is to say, in the gasket 34 , the range excluding the solid line hatched portions, the bore holes 29 , the bolt holes 30 , and the center hole 31 (dotted line hatched portions in FIG. 4) indicates portions that are unnecessary for the function of the gasket.
- the length of seal portions that are necessary for the function on the circumference of a circle whose radius is a certain distance x from the center O of the gasket 34 and the length of seal portions that are unnecessary for the function on the circumference of a circle whose radius is a certain distance x from the center O are represented by graphs of FIGS. 5 and 6, respectively.
- Rg indicates the radius of the gasket 34 .
- a complement is given to the description of “the length of seal portions on the circumference of a circle whose radius is a certain distance x from the center O of the gasket 34 ”.
- La and Lb are expressed as
- an area S of seal portions of the gasket 34 is calculated by the following formula (3).
- the function f(x) is a function for the graph of FIG. 5
- the function g(x) is a function for the range of 0 ⁇ x ⁇ Rb in the graph of FIG. 6
- the function h(x) is a function for the range of Rb ⁇ x ⁇ Rg in the graph of FIG. G.
- the total pressure F depends on the tightening force of bolt, and the shape, rigidity of the cylinder block and rear housing member, and it is thought that the total pressure F in this embodiment is equivalent to that of the conventional compressor.
- ⁇ f 2 F/S(x) ⁇ F/S using the above-described formulae (4) and (5).
- ⁇ M 1 taking the increase in bending moment as ⁇ M 1 , ⁇ M 1 can be expressed by the following formula (6) using the above-described formula (1) and the above-described ⁇ f 2 .
- ⁇ M 1 ⁇ O Rg ( ⁇ f 2 ⁇ x ) dx (6)
- ⁇ M is expressed by a graph shown in FIG. 7 using Formulae (6) and (7).
- FIG. 7 means that if through holes arc formed in a circle with the radius Rc from the center O, since the decrease in bending moment due to the through holes is larger than the increase in bending moment due to increased specific pressure, the total bending moment can be decreased.
- a seal portion for sealing the compressor internally and externally is provided in an outer peripheral portion of the gasket 9 .
- bending moment is not generated on a joint surface 35 between the cylinder block 1 and the gasket 9 , which faces a joint surface between the cylinder block 1 and the front housing member 3 in the axial direction of the drive shaft 13 . Therefore, it is desirable that the gasket 9 be formed with a seal surface in the range of the joint surface 35 so as to decrease the specific pressure ⁇ f 2 as much as possible.
- the bending moment acting on the cylinder block 1 is reduced, and hence the deformation of the cylinder block 1 is restrained.
- the deformation of the cylinder bore 19 is restrained, and hence the reciprocating motion of the piston 20 is made smooth.
- the deformation of the rotary valve accommodating chamber 23 for the rotary valve 24 is restrained, and hence the rotational motion of the rotary valve 24 is made smooth.
- the specific pressure of gasket is increased by reducing the seal surface, so that the sealing ability of gasket is improved, or sufficient sealing ability of gasket is secured even if the tightening force of bolts is decreased as compared with the conventional compressor. Therefore, the deformation of the cylinder block 1 can further be restrained by the decrease in bolt tightening force, and hence the durability of compressor is enhanced.
- FIGS. 8 to 10 a second embodiment will be described with reference to FIGS. 8 to 10 .
- the same reference numerals will be applied to the same or equivalent elements, and the explanation of the elements will be omitted.
- FIG. 8 shows a five-cylinder compressor.
- the rotary valve 24 and the rotary valve accommodating chamber 23 are not used as a suction structure for refrigerant gas, and instead a suction valve forming plate 36 is interposed between the cylinder block 1 and the valve plate 5 , and a gasket 37 is interposed between the suction valve forming plate 36 and the cylinder block 1 .
- a suction valve forming plate 36 is interposed between the cylinder block 1 and the valve plate 5
- a gasket 37 is interposed between the suction valve forming plate 36 and the cylinder block 1 .
- a corresponding suction valve is opened, and a refrigerant gas passes through a corresponding suction hole formed in the valve plate 5 and is sucked into the compression chamber 21 .
- the suction valve is closed, and the suction hole is closed and the refrigerant gas in the compression chamber 21 pushes away the discharge valve and is discharged to the discharge chamber 7 .
- FIG. 10 shows a conventional gasket 39 used for a five-cylinder piston compressor.
- hatched portions are seal portions that are necessary for function of sealing the bore holes 29 , the bolt holes 30 , and the interior of the compressor.
- seal portions that are unnecessary for the function are present even between the adjacent bore holes 29 .
- the integral through hole 38 it is possible to form the integral through hole 38 by allowing the center hole 31 , the first through holes, and the second through holes to communicate with each other. Thereby, the bending moment is reduced, and resultantly the deformation of the cylinder block 1 is restrained. Also, by forming the integral through hole 38 in this manner, a mold necessary for manufacturing the gasket 37 is formed easily, and the life of mold is extended, which also achieves an effect of reducing the manufacturing cost.
- the center hole 31 and the first through holes 32 may be separated from each other.
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- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressor (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
A gasket is provided between a cylinder block and a valve plate. By providing a through hole at a position near the center of the gasket, bending moment acting on the cylinder block is reduced, and hence deformation of the cylinder block is restrained. As a result, reciprocating motion of a piston and rotational motion of a rotary valve are performed smoothly.
Description
- The present invention relates to a piston compressor for a vehicular air conditioner and, more particularly, to a technology for restraining deformation of a cylinder block.
- For example, Japanese Laid-Open Patent Publication No. 8-19160 discloses a
gasket 101 as shown in FIG. 13. Thegasket 101 is used for a piston compressor for a vehicular air conditioner. - The
gasket 101 is formed with a plurality of throughholes 103 that substantially coincide with opening edges ofcylinder bores 102 each containing a piston, a plurality ofinsertion holes 105 through which throughbolts 104 are inserted, and acenter hole 106 through which a drive shaft is inserted. As a piston compressor provided with thisgasket 101, a piston compressor is known in which as shown in a partially enlarged cross-sectional view of FIG. 14, afront housing member 108 is joined to a front end face (left-hand side in the figure) of acylinder block 107, arear housing member 110 is joined to a rear end face (right-hand side in the figure) thereof via avalve plate 109, and these three elements are fastened to each other by thethrough bolts 104. In this piston compressor, thegasket 101 is interposed between thecylinder block 107 and thevalve plate 109. As shown in FIG. 15, thecylinder block 107 is formed with thecylinder bores 102 and anaccommodation chamber 111 for accommodating a rotary valve for sucking refrigerant gas. - In the piston compressor described in the above-described Publication, when the
through bolts 104 are tightened, thecylinder block 107 is subjected to bending moment and is thus deformed. Specifically, as shown in FIG. 14, in the state in which thethrough bolts 104 are tightened, on a joint surface between thecylinder block 107 and thefront housing member 108, a specific pressure f1 acts on the front end face of thecylinder block 107 from thefront housing member 108. Also, on a joint surface between thecylinder block 107 and a seal surface of thegasket 101, a specific pressure f2 acts on the rear end face of thecylinder block 107 from thevalve plate 109. - Taking one arbitrary point on the front end face of the
cylinder block 107, on which the specific pressure f1 acts, as action point P1, and taking one arbitrary point on the rear end face of thecylinder block 107, on which the specific pressure f2 acts, as action point P2, bending moment M acts around the center P3 of straight line H connecting P1 and P2. By this bending moment M, a force Fm in a radial direction of thegasket 101 is applied to both of the action points P1 and P2, by which thecylinder block 107 is deformed as indicated by two-dot chain lines shown in FIG. 15. As a result, there is a fear that smooth reciprocating motion of the piston is hindered by this deformation. - Also, in a case where the
accommodation chamber 111 for the rotary valve is formed in thecylinder block 107 as shown in FIG. 15, theaccommodation chamber 111 is easily deformed because the rigidity of thecylinder block 107 is low. Therefore, smooth rotation of the rotary valve can be hindered. - An object of the present invention is to provide a piston compressor in which bending moment acting on a cylinder block is reduced to restrain deformation of the cylinder block, and the motion of a piston and a rotary valve is performed-smoothly to enhance the durability of the piston compressor.
- To achieve the foregoing and other objectives and in accordance with the purpose of the present invention, a piston compressor having a cylinder block, a front housing member, a rear housing member, a through bolt, a plurality of pistons, a drive shaft, and a gasket is provided. The cylinder block has a plurality of cylinder bores. The cylinder block has two end faces at which the cylinder bores open. The front housing member is secured to one of the end faces of the cylinder block. The rear housing member is secured to the other one of the end faces of the cylinder block with a valve plate in between. The through bolt fastens the cylinder block, the rear housing member, and the front housing. Each piston is accommodated and reciprocates in one of the cylinder bores. The drive shaft drives the pistons, and is rotatably supported by the cylinder block. Reciprocation of the pistons compress and discharge refrigerant gas. The gasket is located between the cylinder block and the valve plate. The gasket has a center hole and a plurality of bore holes. Each bore hole is aligned with one of the cylinder bores. A first through hole is formed in the gasket to reduce bending moment generated in the cylinder block when the through bolt is fastened. The first through hole is located between an adjacent pair of the bore holes and in an imaginary circle. The center of the imaginary circle coincides with the center of the bore hole, and the radius of the imaginary circle is a first radius. The first radius is the distance from the center of tho gasket to the center of one of the bore holes.
- 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 piston compressor in accordance with a first embodiment of the present invention;
- FIG. 2 is a partially cross-sectional view of the compressor shown in FIG. 1;
- FIG. 3 is a front view of a gasket provided in the compressor shown in FIG. 1;
- FIG. 4 is a front view of a conventional gasket used for explanation of the first embodiment;
- FIG. 5 is a graph showing a relationship between circumferential lengths of seal portions necessary for function and distances from the gasket center in a gasket;
- FIG. 6 is a graph showing a relationship between circumferential length of seal portions unnecessary for function and distances from the gasket center in a gasket;
- FIG. 7 is a graph showing a total change amount of bending moment generated in a cylinder block;
- FIG. 8 is a cross-sectional view of a piston compressor in accordance with a second embodiment;
- FIG. 9 is a front view of a gasket provided in the compressor shown in FIG. 8;
- FIG. 10 is a front view of a conventional gasket used for explanation of a second embodiment;
- FIG. 11 is a front view of a gasket in a modified embodiment;
- FIG. 12 is a front view of a gasket in another modified embodiment;
- FIG. 13 is a front view of a prior art gasket;
- FIG. 14 is a partially cross-sectional view of a prior art piston compressor; and
- FIG. 15 is a partially cross-sectional view of a prior art piston compressor.
- A first embodiment of the present invention will now be described in detail with reference to FIGS.1 to 7.
- In a variable displacement piston compressor in accordance with the first embodiment of the present invention, as shown in FIG. 1, a
front housing member 3 is joined to a front end face of acylinder block 1 via agasket 2, and acrank chamber 4 serving as a control chamber is defined on the inside thereof. Also, arear housing member 6 is joined to a rear end face of thecylinder block 1 via avalve plate 5, and adischarge chamber 1 arid asuction chamber 8 are defined on the inside thereof. Between thecylinder block 1 and thevalve plate 5 is interposed agasket 9, and between thevalve plate 5 and therear housing member 6 are interposed a discharge valve forming plate 10 formed integrally with a discharge valve and aretainer forming plate 11 for forming a retainer. Thecylinder block 1, thefront housing member 3, and therear housing member 6 are fastened by throughbolts 12, not shown in FIG. 1. - In shaft holes formed in central portions of the cylinder block land the
front housing member 3, adrive shaft 13 is rotatably supported byradial bearings drive shaft 13 is provided ashaft seal device 15. In thecrank chamber 4, alug plate 16 is fixed to thedrive shaft 13 so as to be integrally rotatable, and aswash plate 17 serving as a cam plate is disposed in a state in which thedrive shaft 13 is inserted through a through hole formed in theswash plate 17. Ahinge mechanism 18 is interposed between thelug plate 16 and theswash plate 17. Theswash plate 17 can be rotated in synchronism with thelug plate 16 and thedrive shaft 13 by a hinge connection between theswash plate 17 and thelug plate 16 via thehinge mechanism 18 and the support of thedrive shaft 13, and also can be tilted with respect to thedrive shaft 13 while sliding in an axial direction of thedrive shaft 13. - A plurality of
cylinder bores 19 arranged in a circumferential direction in thecylinder block 1 each contain apiston 20 capable of reciprocating. Between eachpiston 20 and thevalve plate 5, acompression chamber 21 whose volume is changed according to reciprocating motion of thepiston 20 is defined. Eachpiston 20 is engaged with a peripheral edge portion of theswash plate 17 via a pair ofshoe 22. Therefore, rotational motion of theswash plate 17 performed via thelug plate 16 and thehinge mechanism 18, which is caused by rotation of thedrive shaft 13, is converted to reciprocating motion of thepistons 20 performed via theshoes 22. Thelug plate 16, theswash plate 17, thehinge mechanism 18, and theshoes 22 constitute a crank mechanism that converts therotational motion 1 of thedrive shaft 13 to compressive motion for compressing refrigerant gas in thecompression chamber 21. - A rotary
valve accommodating chamber 23 is formed in thecylinder block 1, and in the rotaryvalve accommodating chamber 23, arotary valve 24 is connected to thedrive shaft 13 via acoupling 25 so as to be rotatable in synchronism with thedrive shaft 13. In therotary valve 24, asuction passage 26 that always communicates with thesuction chamber 8 is formed, and anoutlet 27 of thesuction passage 26 is open in an outer peripheral surface of therotary valve 24. In thecylinder block 1, communication holes 28 are formed. Each communication hole corresponds to one of thecompression chambers 21 and allows theoutlet 27 of therotary valve 24 to communicate with the correspondingcompression chamber 21. - When the
drive shaft 13 of the compressor is rotated by engine power, theswash plate 17 is rotated via thelug plate 16 and thehinge mechanism 18, so that thepistons 20 are reciprocated in the cylinder bores 19 via theshoes 22. On a suction stroke of thepiston 20, theoutlet 27 of therotary valve 24 is connected to eachcommunication hole 28, so that the refrigerant gas in thosuction chamber 8 is sucked into eachcompression chamber 21 through thesuction passage 26. Further, when eachpiston 20 takes compression stroke and discharge strokes, the correspondingcommunication hole 28 is closed by an outer peripheral surface of therotary valve 24, so that the refrigerant gas in thecompression chamber 21 pushes away the discharge valve and is discharged to thedischarge chamber 7. - Next, an essential point of the present invention will be described in detail. First, forces acting on the
cylinder block 1 in this embodiment are shown in FIG. 2. In a state in which the throughbolts 12 are tightened, on a joint surface between thecylinder block 1 and thefront housing member 3, a specific pressure f1 acts on a front end face of thecylinder block 1 from thefront housing member 3. Also, on a joint surface between thecylinder block 1 and a seal surface of thegasket 9, a specific pressure f2 acts on a rear end face of thecylinder block 1 from thegasket 9. - Taking one arbitrary point on the front end face of the
cylinder block 1, on which the specific pressure f1 acts, as action point P1, and taking one arbitrary point on the rear end face of thecylinder block 1, on which the specific pressure f2 acts, as action point P2, bending moment M acts around the center P3 of straight line H connecting P1 and P2. When the shortest distance between both of the action points P1 and P2 in a radial direction of thegasket 9 is taken as D1, the shortest distance therebetween in the axial direction of the throughbolt 12 is taken as D2, and a radial force generated at both of the action points P1 and P2 by the bending moment M is taken as Fm, the bending moment M is obtained by the following formulae: - Fm=
f 2·(D 1/D 2) (1) - M=Fm·
D 2=f 2·D 1 (2) - From these two formulae, it is found that the force Fm and the bending moment M increase as the specific pressure f2 acting on the rear end face of the
cylinder block 1 from thegasket 9 increases, or as the action point P2 is closer to the center of thegasket 9. - The
gasket 9 in this embodiment is shown in FIG. 3. Thegasket 9 is formed of a rigid base consisting of an iron-base metallic sheet and an elastic layer having sealing ability, such as rubber, with which both surfaces of the base are coated. Also, thegasket 9 has a plurality of (six in this embodiment) bore holes 29 that substantially coincide with the opening edges of the cylinder bores 19 and a plurality of (six in this embodiment) bolt holes 30 through which the throughbolts 12 are inserted. In a circle whose radius is a distance Rb from the center of thegasket 9 to the center of eachbore hole 29, a through hole is formed which corresponds to a center hole 31 (in a circle indicated by dotted line in FIG. 3) in the conventional gasket and first throughholes 32 communicating with each other. Between a circle having a radius of a distance Rb from the center of thegasket 9 and a circle having a radius Rc from the center of thegasket 9, second throughholes 33 are formed. As is apparent from FIG. 2, in the range in which the first throughholes 32 and the second throughholes 33 are provided, the specific pressure f2 does not act on thecylinder block 1, so that bending moment is not generated. Because the bending moment is larger at a position closer to the center of thegasket 9, the provision of the throughholes - The meaning of the radius Rc and a method for determining the same will be explained with reference to FIGS.4 to 7. FIG. 4 shows a
conventional gasket 34 formed with bore holes 29, bolt holes 30, and acenter hole 31. In FIG. 4, solid line hatched portions are seal portions that are necessary for function of sealing the bore holes 29, the bolt holes 30, and the interior of the compressor. That is to say, in thegasket 34, the range excluding the solid line hatched portions, the bore holes 29, the bolt holes 30, and the center hole 31 (dotted line hatched portions in FIG. 4) indicates portions that are unnecessary for the function of the gasket. The length of seal portions that are necessary for the function on the circumference of a circle whose radius is a certain distance x from the center O of thegasket 34 and the length of seal portions that are unnecessary for the function on the circumference of a circle whose radius is a certain distance x from the center O are represented by graphs of FIGS. 5 and 6, respectively. Rg indicates the radius of thegasket 34. Here, a complement is given to the description of “the length of seal portions on the circumference of a circle whose radius is a certain distance x from the center O of thegasket 34”. For example, when the length of seal portions that are necessary for the function on the circumference of a circle whose radius is a distance A from the center O is taken as La, and the length of seal portions that are unnecessary for the function thereon is taken as Lb, as is apparent from FIG. 4, La and Lb are expressed as - La=L 1+L 3+L
5 +L 7+L 9+L 11 - Lb=L 2+L 4+L
6 +L 8+L 10+L 12 - From FIGS. 5 and 6, an area S of seal portions of the
gasket 34 is calculated by the following formula (3). - S=∫ O Rg f(x)dx+∫ O Rb g(x)dx+∫ Rb Rg h(x)dx (3)
- In the above formula (3), the function f(x) is a function for the graph of FIG. 5, the function g(x) is a function for the range of 0≦x≦Rb in the graph of FIG. 6, and the function h(x) is a function for the range of Rb≦x≦Rg in the graph of FIG. G.
- Further, when the total pressure applied to the whole of a seal surface of the
gasket 34 at the time of tightening of the throughbolts 12 is taken as F, the specific pressure f2 per unit area of the seal surface is expressed as -
f 2=F/S - The total pressure F depends on the tightening force of bolt, and the shape, rigidity of the cylinder block and rear housing member, and it is thought that the total pressure F in this embodiment is equivalent to that of the conventional compressor.
- Next, it is assumed that through holes with a minute width Δx are provided in the portions that are unnecessary for the function (dotted line hatched portions in FIG. 4) on the circumference whose radius is a certain distance x from the center O. An area S(x) of seal portions at this time is calculated by the following two formulae.
- When the increase in specific pressure at the time when the through holes with a minute width Δx are provided is taken as Δf2, Δf2 can be expressed as Δf2=F/S(x)−F/S using the above-described formulae (4) and (5).
- Therefore, taking the increase in bending moment as ΔM1, ΔM1 can be expressed by the following formula (6) using the above-described formula (1) and the above-described Δf2.
-
ΔM 1=∫O Rg(Δf 2·x)dx (6) - Also, taking the decrease in bending moment due to the provision of through holes as ΔM2, from the above-described formula (2), ΔM2 is expressed as
-
ΔM 2=f 2·x (7) - Therefore, when the total change amount of bending moment at the time when the through holes are provided in the portions that are unnecessary for the function on the circumference whose radius is a certain distance x from the center O is taken as ΔM (=ΔM2−ΔM1), ΔM is expressed by a graph shown in FIG. 7 using Formulae (6) and (7). Rc is defined as a distance of a point at which ΔM1=ΔM2 (≠0) from the center O. In FIG. 7, Rc denotes a point at which ΔM=0 (excluding a case where ΔM1=ΔM2=0 is satisfied).
- FIG. 7 means that if through holes arc formed in a circle with the radius Rc from the center O, since the decrease in bending moment due to the through holes is larger than the increase in bending moment due to increased specific pressure, the total bending moment can be decreased.
- In this embodiment, a seal portion for sealing the compressor internally and externally is provided in an outer peripheral portion of the
gasket 9. As is apparent from FIG. 2, bending moment is not generated on ajoint surface 35 between thecylinder block 1 and thegasket 9, which faces a joint surface between thecylinder block 1 and thefront housing member 3 in the axial direction of thedrive shaft 13. Therefore, it is desirable that thegasket 9 be formed with a seal surface in the range of thejoint surface 35 so as to decrease the specific pressure Δf2 as much as possible. - By this embodiment, the bending moment acting on the
cylinder block 1 is reduced, and hence the deformation of thecylinder block 1 is restrained. As a result, the deformation of the cylinder bore 19 is restrained, and hence the reciprocating motion of thepiston 20 is made smooth. Also, the deformation of the rotaryvalve accommodating chamber 23 for therotary valve 24 is restrained, and hence the rotational motion of therotary valve 24 is made smooth. Further, the specific pressure of gasket is increased by reducing the seal surface, so that the sealing ability of gasket is improved, or sufficient sealing ability of gasket is secured even if the tightening force of bolts is decreased as compared with the conventional compressor. Therefore, the deformation of thecylinder block 1 can further be restrained by the decrease in bolt tightening force, and hence the durability of compressor is enhanced. - Next, a second embodiment will be described with reference to FIGS.8 to 10. In the second embodiment, only points different from the first embodiment shown in FIGS. 1 to 7 will be explained. Also, the same reference numerals will be applied to the same or equivalent elements, and the explanation of the elements will be omitted.
- FIG. 8 shows a five-cylinder compressor. In this compressor, the
rotary valve 24 and the rotaryvalve accommodating chamber 23 are not used as a suction structure for refrigerant gas, and instead a suction valve forming plate 36 is interposed between thecylinder block 1 and thevalve plate 5, and agasket 37 is interposed between the suction valve forming plate 36 and thecylinder block 1. On the suction stroke of eachpiston 20, a corresponding suction valve is opened, and a refrigerant gas passes through a corresponding suction hole formed in thevalve plate 5 and is sucked into thecompression chamber 21. Further, when thepiston 20 takes compression and discharge strokes, the suction valve is closed, and the suction hole is closed and the refrigerant gas in thecompression chamber 21 pushes away the discharge valve and is discharged to thedischarge chamber 7. - As shown in FIG. 9, in the
gasket 37 used in this embodiment, one throughhole 38 is formed in a state in which the center hole 31 (in a circle indicated by dotted line in FIG. 9), the first through holes, and the second through holes communicate with each other. In the piston compressor of this embodiment, the number of cylinders is decreased to five as compared with the above-described first embodiment. FIG. 10 shows aconventional gasket 39 used for a five-cylinder piston compressor. In FIG. 10, hatched portions are seal portions that are necessary for function of sealing the bore holes 29, the bolt holes 30, and the interior of the compressor. As is apparent from FIG. 10, in thegasket 39, seal portions that are unnecessary for the function are present even between the adjacent bore holes 29. Therefore, as in thegasket 37 of this embodiment, it is possible to form the integral throughhole 38 by allowing thecenter hole 31, the first through holes, and the second through holes to communicate with each other. Thereby, the bending moment is reduced, and resultantly the deformation of thecylinder block 1 is restrained. Also, by forming the integral throughhole 38 in this manner, a mold necessary for manufacturing thegasket 37 is formed easily, and the life of mold is extended, which also achieves an effect of reducing the manufacturing cost. - It should be apparent to those skilled in the art that the present invention may be embodied in many other specific forms without departing from the spirit or scope of the invention. Particularly, it should be understood that the invention may be embodied in the following forms.
- As shown in FIGS. 11 and 12, the
center hole 31 and the first throughholes 32 may be separated from each other. - In these examples as well, the deformation of the cylinder block is restrained by reducing bending moment, and hence the motion of the piston and rotary valve is made smooth, by which the durability of the piston compressor is enhanced.
- 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 heroin, but may be modified within the scope arid equivalence of the appended claims.
Claims (19)
1. A piston compressor comprising:
a cylinder block having a plurality of cylinder bores, wherein the cylinder block has two end faces at which the cylinder bores open;
a front housing member, which is secured to one of the end faces of the cylinder block;
a rear housing member, which is secured to the other one of the end faces of the cylinder block with a valve plate in between;
a through bolt for fastening the cylinder block, the rear housing member, and the front housing;
a plurality of pistons, each of which is accommodated and reciprocates in one of the cylinder bores;
a drive shaft for driving the pistons, wherein the drive shaft is rotatably supported by the cylinder block, wherein reciprocation of the pistons compress and discharge refrigerant gas; and
a gasket located between the cylinder block and the valve plate, wherein the gasket has a center hole and a plurality of bore holes, each bore hole being aligned with one of the cylinder bores, wherein a first through hole in formed in the gasket to reduce bending moment generated in the cylinder block when the through bolt is fastened, wherein the first through hole is located between an adjacent pair of the bore holes and in an imaginary circle, the center of the imaginary circle coinciding with the center of the bore hole and the radius of the imaginary circle being a first radius, and wherein the first radius is the distance from the center of the gasket to the center of one of the bore holes.
2. The compressor according to claim 1 , wherein the imaginary circle is a first imaginary circle, wherein a second imaginary circle having a second radius is assumed to exist about the center of the gasket, the second radius being greater than the first radius by a predetermined value, wherein a second through hole is formed in the gasket to reduce bending moment generated when the through bolt is fastened, and wherein the second through hole is located in a portion of the gasket between the second imaginary circle and the first imaginary circle.
3. The compressor according to claim 2 , wherein the first through hole communicates with the second through hole.
4. The compressor according to claim 1 , wherein the imaginary circle is a first imaginary circle, wherein a second imaginary circle having a second radius Rc is assumed to exist about the center of the gasket, the second radius Rc is different from the first radius, wherein a second through hole is formed in the gasket to reduce bending moment generated in the cylinder block when the through bolt is fastened, and wherein the second through hole is located in a portion of the gasket between the second imaginary circle and the first imaginary circle, and
wherein, with respect to a pressure applied to the cylinder bore by the gasket when the through bolt is fastened, if f denotes the pressure on the assumption that the gasket does not have the first and second through holes; Δf denotes the amount of increase of the pressure relative to the pressure f when a through hole is formed on the second imaginary circle of the gasket on the assumption that the gasket does not have the first and second through holes; and R denotes an arbitrary distance from the center of the gasket, the second radius Rc is determined such that f·Rc is equal to an integration value obtained by integrating Δf·R from the center of gasket over the range of the radius of the gasket.
5. The compressor according to claim 4 , wherein f·Rc represents a decrease amount of the bending moment when a through hole is formed on the second imaginary circle of the gasket on the assumption that the gasket does not have the first and second through holes, and wherein the integration value represents an increase amount of the bending moment when a through hole is formed on the second imaginary circle of the gasket on the assumption that the gasket does not have the first and second through holes.
6. The compressor according to claim 4 , wherein the first through hole communicates with the second through hole.
7. The compressor according to claim 1 , wherein the first through hole communicates with the center hole.
8. The compressor according to claim 1 , wherein a compression chamber is defined in each cylinder bore by the corresponding piston, wherein the compressor further comprising a suction pressure zone, the internal pressure of which is a suction pressure, and a rotary valve that rotates as the drive shaft rotates, and wherein the rotary valve has an introducing passage for successively introducing gas from the suction pressure zone to the compression chambers as the drive shaft rotates.
9. The compressor according to claim 2 , wherein the cylinder bores are provided about an axis of the cylinder block at equal angular intervals.
10. The compressor according to claim 9 , wherein the first through hole is one of a plurality of first through holes, the second through hole is one of a plurality of second through holes, wherein the first through holes are provided about the center of the gasket at equal angular intervals, and wherein each second through hole forms a pair with one of the first through holes.
11. A piston compressor comprising:
a cylinder block having a plurality of cylinder bores, wherein the cylinder block has two end faces at which the cylinder bores open;
a front housing member, which is secured to one of the end faces of the cylinder block;
a rear housing member, which is secured to the other one of the end faces of the cylinder block with a valve plate in between;
a through bolt for fastening the cylinder block, the rear housing member, and the front housing;
a plurality of pistons, each of which is accommodated and reciprocates in one of the cylinder bores;
a drive shaft for driving the pistons, wherein the drive shaft is rotatably supported by the cylinder block, wherein reciprocation of the pistons compress and discharge refrigerant gas; and
a gasket located between the cylinder block and the valve plate, wherein the gasket has a center hole and a plurality of bore holes, each bore hole being aligned with one of the cylinder bores, wherein the cylinder bores are provided about an axis of the cylinder block at equal angular intervals, wherein a through hole is formed in the gasket to reduce bending moment generated in the cylinder block when the through bolt is fastened, wherein the through hole is located in an imaginary circle, the radius of the imaginary circle being a first radius, wherein the first radius is the distance from the center of the gasket to the center of one of the bore holes, and wherein the through hole has a section that is located between an adjacent pair of the cylinder bores.
12. The compressor according to claim 11 , wherein the through hole is a first through hole, and the imaginary circle is a first imaginary circle, wherein a second imaginary circle having a second radius is assumed to exist about the center the gasket, the second radius being greater than the first radius by a predetermined value, wherein a second through hole is formed in the gasket to reduce bending moment generated when the through bolt is fastened, and wherein the second through hole is located in a portion of the gasket between the second imaginary circle and the first imaginary circle.
13. The compressor according to claim 12 , wherein the first through hole communicates with the second through hole.
14. The compressor according to claim 11 , wherein the through hole is a first through hole, and the imaginary circle is a first imaginary circle, wherein a second imaginary circle having a second radius Rc is assumed to exist about the center of the gasket, the second radius Rc is different from the first radius, wherein a second through hole is formed in the gasket to reduce bending moment generated in the cylinder block when the through bolt is fastened, and wherein the second through hole is located in a portion of the gasket between the second imaginary circle and the first imaginary circle, and
wherein, with respect to a pressure applied to the cylinder bore by the gasket when the through bolt is fastened, if f denotes the pressure on the assumption that the gasket does not have the first and second through holes; Δf denotes the amount of increase of the pressure relative to the pressure f when a through hole is formed on the second imaginary circle of the gasket on the assumption that the gasket does not have the first and second through holes; and R denotes an arbitrary distance from the center of the gasket, the second radius Rc is determined such that f·Rc is equal to an integration value obtained by integrating Δf·R from the center of gasket over the range of the radius of the gasket.
15. The compressor according to claim 14 , wherein f·Rc represents a decrease amount of the bending moment when a through hole is formed on the second imaginary circle of the gasket on the assumption that the gasket does not have the first and second through holes, and wherein the integration value represents an increase amount of the bending moment when a through hole is formed on the second imaginary circle of the gasket on the assumption that the gasket does not have the first and second through holes.
16. The compressor according to claim 14 , wherein the first through hole communicates with the second through hole.
17. The compressor according to claim 11 , wherein the first through hole communicates with the center hole.
18. The compressor according to claim 11 , wherein a compression chamber is defined in each cylinder bore by the corresponding piston, wherein the compressor further comprising a suction pressure zone, the internal pressure of which is a suction pressure, and a rotary valve that rotates as the drive shaft rotates, and wherein the rotary valve has an introducing passage for successively introducing gas from the suction pressure zone to the compression chambers as the drive shaft rotates.
19. The compressor according to claim 12 , wherein the first through hole is one of a plurality of first through holes, the second through hole is one of a plurality of second through holes, wherein the first through holes are provided about the center of the gasket at equal angular intervals, and wherein each second through hole forms a pair with one of the first through holes.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2003087295A JP2004293421A (en) | 2003-03-27 | 2003-03-27 | Piston type compressor |
JP2003-087295 | 2003-03-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
US20040247455A1 true US20040247455A1 (en) | 2004-12-09 |
Family
ID=32821535
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/808,831 Abandoned US20040247455A1 (en) | 2003-03-27 | 2004-03-25 | Piston compressor |
Country Status (6)
Country | Link |
---|---|
US (1) | US20040247455A1 (en) |
EP (1) | EP1462651A1 (en) |
JP (1) | JP2004293421A (en) |
KR (1) | KR20040086130A (en) |
CN (1) | CN1294358C (en) |
BR (1) | BRPI0401434A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040076535A1 (en) * | 1999-12-28 | 2004-04-22 | Ryosuke Izawa | Reciprocating refrigerant compressor |
US20080063550A1 (en) * | 2006-09-07 | 2008-03-13 | Masaki Inoue | Piston type compressor |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2011163177A (en) * | 2010-02-08 | 2011-08-25 | Sanden Corp | Reciprocating compressor |
KR20200059555A (en) * | 2018-11-21 | 2020-05-29 | 엘지전자 주식회사 | Compressor including cylinder block |
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US3731499A (en) * | 1970-08-05 | 1973-05-08 | Paulstra Sa | Flexible couplings |
US3985000A (en) * | 1974-11-13 | 1976-10-12 | Helmut Hartz | Elastic joint component |
US5556261A (en) * | 1994-06-27 | 1996-09-17 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressor |
US5782613A (en) * | 1995-03-20 | 1998-07-21 | Kabushiki Kaisha Toyoda Jodoshokki Seisakusho | Piston type compressor with structure for reducing cylinder bore deformation |
US6158974A (en) * | 1997-03-25 | 2000-12-12 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Reciprocating compressor |
US6227814B1 (en) * | 1998-05-29 | 2001-05-08 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Reciprocating type refrigerant compressor with an improved internal sealing unit |
US6231315B1 (en) * | 1996-06-24 | 2001-05-15 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Compressor having a value plate and a gasket |
US6454545B1 (en) * | 1996-11-25 | 2002-09-24 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Compressor |
Family Cites Families (1)
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FR2793188A1 (en) * | 1999-05-06 | 2000-11-10 | Michelin Soc Tech | MOLDING ELEMENT AND MOLD FOR MOLDING A CUT IN A TREAD |
-
2003
- 2003-03-27 JP JP2003087295A patent/JP2004293421A/en not_active Withdrawn
- 2003-11-26 KR KR1020030084292A patent/KR20040086130A/en not_active Application Discontinuation
-
2004
- 2004-03-25 US US10/808,831 patent/US20040247455A1/en not_active Abandoned
- 2004-03-25 BR BR0401434-0A patent/BRPI0401434A/en not_active IP Right Cessation
- 2004-03-26 EP EP04007411A patent/EP1462651A1/en not_active Withdrawn
- 2004-03-27 CN CNB2004100352666A patent/CN1294358C/en not_active Expired - Fee Related
Patent Citations (8)
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US3731499A (en) * | 1970-08-05 | 1973-05-08 | Paulstra Sa | Flexible couplings |
US3985000A (en) * | 1974-11-13 | 1976-10-12 | Helmut Hartz | Elastic joint component |
US5556261A (en) * | 1994-06-27 | 1996-09-17 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressor |
US5782613A (en) * | 1995-03-20 | 1998-07-21 | Kabushiki Kaisha Toyoda Jodoshokki Seisakusho | Piston type compressor with structure for reducing cylinder bore deformation |
US6231315B1 (en) * | 1996-06-24 | 2001-05-15 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Compressor having a value plate and a gasket |
US6454545B1 (en) * | 1996-11-25 | 2002-09-24 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Compressor |
US6158974A (en) * | 1997-03-25 | 2000-12-12 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Reciprocating compressor |
US6227814B1 (en) * | 1998-05-29 | 2001-05-08 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Reciprocating type refrigerant compressor with an improved internal sealing unit |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
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US20040076535A1 (en) * | 1999-12-28 | 2004-04-22 | Ryosuke Izawa | Reciprocating refrigerant compressor |
US7004734B2 (en) * | 1999-12-28 | 2006-02-28 | Zexel Valco Climate Control Corporation | Reciprocating refrigerant compressor |
US20080063550A1 (en) * | 2006-09-07 | 2008-03-13 | Masaki Inoue | Piston type compressor |
Also Published As
Publication number | Publication date |
---|---|
JP2004293421A (en) | 2004-10-21 |
CN1294358C (en) | 2007-01-10 |
EP1462651A1 (en) | 2004-09-29 |
KR20040086130A (en) | 2004-10-08 |
BRPI0401434A (en) | 2005-01-18 |
CN1534191A (en) | 2004-10-06 |
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