US20030075041A1 - Piston for fluid machine and the fluid machine having the same - Google Patents
Piston for fluid machine and the fluid machine having the same Download PDFInfo
- Publication number
- US20030075041A1 US20030075041A1 US10/272,118 US27211802A US2003075041A1 US 20030075041 A1 US20030075041 A1 US 20030075041A1 US 27211802 A US27211802 A US 27211802A US 2003075041 A1 US2003075041 A1 US 2003075041A1
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- United States
- Prior art keywords
- piston
- clock
- drive shaft
- guide wall
- wall
- 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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- 239000012530 fluid Substances 0.000 title claims abstract description 20
- 230000002787 reinforcement Effects 0.000 claims description 29
- 239000003507 refrigerant Substances 0.000 claims description 15
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 6
- 238000006073 displacement reaction Methods 0.000 description 16
- 238000003754 machining Methods 0.000 description 16
- 230000006835 compression Effects 0.000 description 10
- 238000007906 compression Methods 0.000 description 10
- 238000004512 die casting Methods 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000003825 pressing Methods 0.000 description 4
- 230000008569 process Effects 0.000 description 4
- 230000007704 transition Effects 0.000 description 4
- 238000013459 approach Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000004913 activation Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000005242 forging Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000007517 polishing process Methods 0.000 description 1
- 239000004575 stone Substances 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
- 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
- F04B27/0873—Component parts, e.g. sealings; Manufacturing or assembly thereof
- F04B27/0878—Pistons
Definitions
- the present invention relates to a piston for a fluid machine and to the fluid machine.
- the piston has a receiving wall for receiving side force and a guide wall between a head portion in a cylinder bore and a neck portion that is operatively connected to a cam plate.
- a cavity is conventionally formed in a connecting portion between a head portion and a neck portion of the piston to reduce the weight of the piston.
- Japanese Unexamined Patent Publication No. 2000-274350 discloses the above type of piston in which a cavity is formed in a portion corresponding to the connecting portion of the piston.
- a receiving wall for receiving side force is formed at the connecting portion on the downside of the head portion.
- a guide wall is formed at the connecting portion on the upside of the head portion.
- the receiving wall is formed on a preceding side in a rotating direction of a swash plate.
- the swash plate functions as a cam plate that reciprocates the piston. Thereby, the receiving wall effectively receives the side force from the inner circumferential surface of a cylinder bore.
- the upside of the head portion is further away from a drive shaft of a fluid machine while the downside is closer to the drive shaft.
- the receiving wall is not formed on a following side in the rotating direction of the swash plate.
- the receiving wall and the guide wall are not satisfactorily balanced with respect to a central axis of the head portion. Therefore, in the above structure, if the piston is polished and ground by a centerless machining process, it is hard to ensure the accuracy of machining.
- the centerless machining is a machining method of polishing and grinding by contacting a machining tool such as a grind stone with the piston under the condition that the rotary center of the piston as a work piece is not chucked but the outer circumferential surface of the piston is radially pressed by using a support member such as a roller.
- a support member such as a roller.
- the accuracy of machining is improved.
- the receiving wall and the guide wall are imbalanced with respect to the central axis of the head portion. Therefore, the pressing force of the support member and the machining tool hardly become equal to each other. Consequently, it becomes hard to ensure the accuracy of machining.
- the present invention is directed to a piston for a fluid machine and the its reduced manufacturing cost due to not only the reduced weight of the piston but also a centerless machining.
- a piston is used in a fluid machine.
- the fluid machine has a drive shaft and a cam plate that is operatively connected to the drive shaft.
- the drive shaft integrally rotates with the cam plate in a housing.
- the piston has a head portion, a neck portion, a receiving wall and a guide wall.
- the head portion is accommodated in a cylinder bore that is formed in the housing.
- the neck portion is operatively connected to the cam plate through a pair of shoes.
- the receiving wall integrally connects the head portion and the neck portion on the drive shaft side.
- the receiving wall is formed substantially on a preceding side in a rotating direction of the cam plate.
- the guide wall integrally connects the head portion and the neck portion on an opposite side of the drive shaft side.
- the guide wall is formed substantially on a following side in the rotating direction of the cam plate.
- a fluid machine has a housing, a drive shaft and a piston.
- the drive shaft is rotatably supported in the housing.
- the piston is operatively connected to the drive shaft and exerts pressure on fluid.
- the piston includes a head portion, a neck portion, a receiving wall and a guide wall.
- the head portion is accommodated in a cylinder bore that is formed in the housing.
- the neck portion is operatively connected to the drive shaft.
- the receiving wall integrally connects the head portion and the neck portion on the drive shaft side.
- the receiving wall is formed substantially on a preceding side in a rotating direction of the drive shaft.
- the guide wall integrally connects the head portion and the neck portion on an opposite side of the drive shaft side.
- the guide wall is formed substantially on a following side in the rotating direction of the drive shaft.
- a piston type compressor has a housing, a drive shaft, a cam plate and a plurality of pistons.
- the drive shaft is rotatably supported in the housing.
- the cam plate is supported by the drive shaft.
- the cam plate is rotated by the rotation of the drive shaft.
- the plurality of pistons is operatively connected to the cam plate and compresses refrigerant gas.
- the rotation of the cam plate is converted into a reciprocating movement of the piston.
- the piston includes a head portion, a neck portion, a receiving wall and a guide wall.
- the head portion is accommodated in a cylinder bore that is formed in the housing.
- the neck portion is operatively connected to the cam plate.
- the receiving wall integrally connects the head portion and the neck portion on a side of the drive shaft.
- the receiving wall is formed substantially on a preceding side in a rotating direction of the cam plate.
- the guide wall integrally connects the head portion and the neck portion on an opposite side of the drive shaft.
- the guide wall is formed substantially on a following side in the rotating direction of the cam plate.
- FIG. 1 is a cross-sectional view of a variable displacement single-head piston type compressor according to a preferred embodiment of the present invention
- FIG. 2 is a perspective view of a piston for use in the variable displacement single-head piston type compressor according to the preferred embodiment of the present invention
- FIG. 3 is an enlarged cross-sectional view of the piston taken along the line III-III in FIG. 1;
- FIG. 4A is a partial side view of a swash plate, a pair of shoes and the piston according to the preferred embodiment of the present invention.
- the piston is positioned near the top dead center while the piston is in transition from a bottom dead center toward a top dead center;
- FIG. 4B is a partial top view of the swash plate, the pair of shoes and the piston according to the preferred embodiment of the present invention.
- the piston is positioned near the top dead center while the piston is in transition from the bottom dead center toward the top dead center;
- FIG. 5A is a partial side view of the swash plate, the pair of shoes and the piston according to the preferred embodiment of the present invention.
- the piston is positioned at an early stage while the piston is in transition from the top dead center toward the bottom dead center;
- FIG. 5B is a partial top view of the swash plate, the pair of shoes and the piston according to the preferred embodiment of the present invention.
- the piston is positioned at the early stage while the piston is in transition from the top dead center toward the bottom dead center;
- FIG. 6 is a cross-sectional view of a connecting portion of the piston according to another preferred embodiment of the present invention.
- FIG. 7 is a cross-sectional view of a connecting portion of the piston according to yet another preferred embodiment of the present invention.
- FIG. 8 is an enlarged cross-sectional view of the piston taken in FIG. 3, which is manufactured by using movable dies and a stationary die.
- FIGS. 1 through 5 A piston for a fluid machine according to a preferred embodiment of the present invention will now be described with reference to FIGS. 1 through 5.
- FIG. 1 illustrates a variable displacement single-head piston type compressor C (hereinafter a compressor) or a fluid machine that is applied to a vehicle air conditioner.
- a compressor variable displacement single-head piston type compressor
- left and right sides of FIG. 1 respectively represents front and rear.
- a front housing 11 , a cylinder block 12 and a rear housing 13 form a housing of a compressor C or a compressor housing.
- the rear end of the front housing 11 is fixedly secured to the front end of the cylinder block 12 that is a center housing.
- the front end of the rear housing 13 is fixedly secured to the rear end of the cylinder block through a valve plate assembly 14 .
- FIG. 1 illustrates a variable displacement single-head piston type compressor C (hereinafter a compressor) or a fluid machine that is applied to a vehicle air conditioner.
- left and right sides of FIG. 1 respectively represents front and rear.
- a front housing 11 , a cylinder block 12 and a rear housing 13 form a housing of a compressor C or
- the compressor housing and the valve plate assembly 14 are fixedly secured by bolting the rear housing 13 with a plurality of bolts 10 through the front housing 11 , the cylinder block 12 and the valve plate assembly 14 .
- the front housing 11 and the cylinder block 12 define a crank chamber 15 .
- a drive shaft 16 that drives the compressor C is rotatably supported by the front housing 11 and the cylinder block 12 so as to pass through the crank chamber 15 .
- the drive shaft 16 is operatively connected to a vehicle engine that is an external drive source through a clutch mechanism such as an electromagnetic clutch.
- a lug plate 17 is fixedly mounted on the drive shaft 16 in the crank chamber 15 .
- a cam plate or a swash plate 18 is connected to the drive shaft 16 so that the swash plate 18 integrally rotates with the drive shaft 16 through a hinge mechanism 19 and inclines with respect to a central axis L of the drive shaft 16 .
- a plurality of cylinder bores 12 A is formed in the cylinder block 12 around the axis L of the drive shaft 16 although only one cylinder bore is illustrated in the drawing. Also, a piston for a fluid machine or a single-head piston 20 is accommodated in each cylinder bore 12 A.
- Each piston 20 is engaged with the swash plate 18 through a pair of shoes 21 .
- the rotary motion of the drive shaft 16 is converted into the reciprocation of each piston 20 along the respective cylinder bores 12 A through the lug plate 17 , the hinge mechanism 19 , the swash plate 18 and the shoes 21 .
- the drive shaft 16 , the lug plate 17 , the hinge mechanism 19 and the shoes 21 constitute a driving unit of the piston 20 .
- Refrigerant gas is compressed by the reciprocating motion.
- a suction chamber 22 and a discharge chamber 23 are defined between the rear housing 13 and the valve plate assembly 14 .
- the valve plate assembly 14 further includes a suction port 24 , a suction valve 25 , a discharge port 26 and a discharge valve 27 .
- the refrigerant gas in the suction chamber 22 is drawn into the corresponding cylinder bore 12 A through the associated suction port 24 by pushing away the associated suction valve 25 while the piston 20 moves frontward (or from right to left in FIG. 1).
- the refrigerant gas drawn into the cylinder bore 12 A is compressed to a predetermined pressure level and is discharged into the corresponding discharge chamber 23 through the associated discharge port 26 by pushing away the associated suction valve 27 while the piston 20 moves rearward (or from left to right in FIG. 1).
- a supply passage 28 connects the discharge chamber 23 with the crank chamber 15 .
- a bleed passage 29 connects the crank chamber 15 with the suction chamber 22 .
- a displacement control valve 30 is placed in the supply passage 28 .
- a pressure sensing passage 31 connects the displacement control valve 30 with the suction chamber 22 .
- the displacement control valve 30 further includes a diaphragm 30 A and a valve body 30 B.
- the valve body 30 B is opened and closed by diaphragm 30 A that reacts to the pressure in the suction chamber 22 through the pressure sensing passage 31 .
- the opening degree of the supply passage 28 is varied to control the amount of the refrigerant gas that is introduced into the crank chamber 15 .
- the refrigerant gas in the crank chamber 15 is introduced into the suction chamber 22 through the bleed passage 29 .
- the pressure in the crank chamber 15 is varied. Since the pressure differential between the crank chamber 15 and the cylinder bore 12 A applied to the piston 20 changes, the inclination angle of the swash plate 18 is also varied. Consequently, a piston stroke is varied, and a displacement is adjusted.
- a spring is placed between the lug plate 17 that is mounted on the drive shaft 16 and the swash plate 18 although not shown in the drawing.
- a circular clip 16 A is fixedly mounted on the drive shaft 16 behind the swash plate 18 .
- a minimum inclination angle of the swash plate 18 is restricted with respect to the perpendicular plane to the axis L of the drive shaft 16 .
- the swash plate 18 contacts with the circular clip 16 A, which is fixedly mounted on the drive shaft 16 .
- the compressor C is constructed in a such manner that the output displacement of the piston 20 is approximately zero per rotation of the drive shaft 16 .
- the piston 20 has a head portion 40 accommodated in the cylinder bore 12 A and a neck portion 41 connected to a distal portion of the swash plate 18 through the shoes 21 .
- the head portion 40 and the neck portion 41 are designed to have a predetermined distance in the axial direction of the piston 20 .
- the head portion 40 and the neck portion 41 are connected by and integrally formed with a connecting portion 42 .
- the head portion 40 is formed in a such manner that its outside cross-sectional diameter is approximately equal to the inside diameter of the cylinder bore 12 A.
- the neck portion 41 further includes a coupler 41 A, which partially forms a shoe inserted portion 41 B and a partially cut disk 41 C, which defines the outside diameter to approximately match the inside diameter of the cylinder bore 12 A.
- the outer circumferential surface between the head portion 40 and the partially cut disk 41 C constitute an outer circumferential surface of a hypothetical cylinder.
- a pair of concave spherical surfaces 41 D is provided at the front and rear sides of the piston 20 so as to face each other in the shoe inserted portion 41 B.
- the pair of shoes 21 is substantially in the shape of hemisphere and sandwiches the front and rear surfaces of the distal portion of the swash plate 18 .
- the shoes 21 are received respectively by the corresponding concave spherical surfaces 41 D in the shoe inserted portion 41 B so as to freely slide.
- the shoes 21 slide relative to the front and rear surfaces of the swash plate 18 and enable the piston 20 to reciprocate in the axial direction of the piston 20 based on the rotary motion of the swash plate 18 , which is integrally rotated with the drive shaft 16 .
- the piston 20 Since the piston 20 is connected to the swash plate 18 through the shoes 21 , the piston 20 is not prevented from rotating around the axis of the piston 20 or around a central axis of the head portion 40 .
- the piston 20 has a rotation restricting potion 41 E for restricting the rotation of the piston 20 around the axis of the piston 20 due to the contact with an inner circumferential surface 11 A of the front housing 11 as shown in FIG. 1.
- the rotation restricting portion 41 E is designed in a such manner that one of the circumferential ends of the rotation restricting portion 41 F contacts the inner circumferential surface 11 A of the front housing 11 as the piston 20 is about to rotate around the axis of the piston 20 .
- the connecting portion 42 has a receiving wall 42 A for receiving side force that extends from the downside of the head portion 40 to the partially cut disk 41 C of the neck portion 41 and a guide wall 42 B that extends from the upper side of the head portion 40 to the partially cut disk 41 C.
- the receiving wall 42 A and the guide wall 42 B are formed in a such manner that the outer circumferential surfaces of the receiving wall 42 A and the guide wall 42 B around the axis of the piston 20 constitute an outer circumferential surface of the hypothetical cylinder as previously described. Note that the upside of the head portion 40 is further away from the drive shaft 16 while the downside is closer to the drive shaft 16 .
- FIG. 3 illustrates the connecting portion 42 in a cross-sectional view in which a rotating direction of the drive shaft 16 or the swash plate 18 is clockwise.
- the receiving wall 42 A is formed on a preceding side in the rotating direction of the swash plate 18 or in the direction indicated by an arrow in FIG. 3.
- a hypothetical straight line Li extends through the central axes of the drive shaft 16 and the head portion 40 as indicated in a dotted line in FIG. 3.
- the hypothetical straight line L 1 and the outer circumferential surface of the head portion 40 intersect at intersectional points P 1 and P 2 .
- the intersectional point P 1 is further from the axis of the drive shaft 16 than the intersectional point P 2 .
- the outer circumferential surface of the receiving wall 42 A is formed substantially over a range of 3 o'clock to 6 o'clock.
- the guide wall 42 B is formed on a following side in the rotating direction of the swash plate 18 or on an opposite side to the preceding side in the rotating direction of the swash plate 18 .
- the outer circumferential surface of the guide wall 42 B is formed substantially over a range of a 9'oclock position to a 12'oclock position.
- the receiving wall 42 A is connected to the guide wall 42 B by a flat reinforcement 42 C.
- the reinforcement 42 C is formed in a such manner that it extends from the end of the receiving wall 42 A at the position of 3 o'clock to the end of the guide wall 42 B at the position of 9 o'clock
- the reinforcement 42 C also extends from the head portion 40 to the partially cut disk 41 C.
- the connecting portion 42 includes the receiving wall 42 A, the guide wall 42 B and the reinforcement 42 C.
- a cross section of the connecting portion 42 is substantially in the shape of S as shown in FIG. 3.
- the piston 20 is integrally molded with an aluminum alloy by die casting.
- the piston 20 is as a whole molded by a die unit during the molding process by die casting.
- the die unit includes a first movable die 43 , a second movable die 44 , a third movable die 45 and a stationary die 46 .
- the first movable die 43 , the second movable die 44 and the third movable die 45 are movable only in a direction between 3 o'clock and 9 o'clock and are drawn in turn. Therefore, each end of the receiving wall 42 A and the guide wall 42 B is formed so as not to prevent the dies from being drawn.
- the concave spherical surfaces 41 D is formed by cutting, and the outer circumferential surfaces of the head portion 40 , the neck portion 41 and the connecting portion 42 are ground or polished.
- the piston 20 experiences forces that include compression reactive force caused by the compression work of the refrigerant gas, inertia force caused by the reciprocating motion of the piston 20 and rotational force of the swash plate 18 caused by friction between the rotating swash plate 18 and the shoes 21 . Based on these forces, reactive force from the inner circumferential surface of the cylinder bore 12 A or side force also acts on the piston 20 .
- FIGS. 4A and 4B show a state in which the piston 20 is positioned near the top dead center where the piston 20 has moved the most rightward position in FIG. 1.
- FIGS. 4A and 4B show the state in which the piston 20 is moving from the bottom dead center side toward the top dead center side.
- the piston 20 receives the largest compression reactive force near the above-described top dead center.
- the piston 20 receives a reactive force Fr as shown in an arrow from the swash plate 18 through the shoe 21 in a perpendicular direction to a sliding surface between the swash plate 18 and the shoe 21 .
- a magnitude of the reactive force Fr meets the magnitude of the compression reactive force and the inertia force.
- the reactive force Fr is based on the inclining state of the swash plate 18 .
- the reactive force Fr is decomposed into a first component of force Fr 1 and a second component of force Fr 2 as shown by arrows on a plane that includes the hypothetical straight line L 1 and the longitudinal axis of the piston 20 in FIG. 4A.
- the first component force Fr 1 as indicated in the arrow acts in parallel to the longitudinal axis of the cylinder bore 12 A, although the cylinder bore 12 A is not illustrated in FIG. 4A but in FIG. 1.
- the second component force Fr 2 as shown by the arrow acts in parallel to the hypothetical straight line L 1 on a plane perpendicular to the longitudinal axis of the cylinder bore 12 A.
- the piston 20 receives a reactive force whose magnitude is equal to that of the second component force Fr 2 in the opposite direction to the second component force Fr 2 from the inner circumferential surface of the cylinder bore 12 A.
- the second component force Fr 2 is in the direction of the straight line that connects 12 o'clock to 6 o'clock.
- the reactive force Fr is decomposed into a third component of force Fr 3 and a fourth component of force Fr 4 as shown by arrows on a plane that includes a straight line connecting 3 o'clock to 9 o'clock and the longitudinal axis of the piston 20 or in FIG. 4B.
- the third component force Fr 3 acts in the axial direction of the cylinder bore 12 A.
- the fourth component force Fr 4 acts in a perpendicular direction to the hypothetical straight line L 1 in the plane perpendicular to the axial direction of the cylinder bore 12 A.
- the piston 20 receives a reactive force whose magnitude is equal to that of the fourth component force Fr 4 in the opposite direction to the fourth component force Fr 4 from the inner circumferential surface of the cylinder bore 12 A.
- the fourth component force Fr 4 is in the direction of the straight line that connects 3 o'clock to 9 o'clock.
- the frictional force caused by the rotating swash plate 18 and the shoes 21 is applied to the piston 20 in the rotating direction of the swash plate 18 .
- the frictional force is substantially in the direction from 9 o'clock toward the 3 o'clock.
- the second component force Fr 2 , the fourth component force Fr 4 and the above frictional force function to incline the piston 20 with respect to the axis of the cylinder bore 12 A.
- Reactive force generated from the inner circumferential surface of the cylinder bore 12 A due to the above combined force is effectively received by the receiving wall 42 A, which is formed on the preceding side in the rotating direction of the swash plate 18 on the lower portion of the head portion 40 .
- the inclination of the piston 20 is substantially restrained.
- a magnitude of the above reactive force that is applied from the inner circumferential surface of the cylinder bore 12 A to the piston 20 has a maximum value near the top dead center while the piston 20 moves from the bottom dead center to the top dead center.
- the above reactive force is mainly applied to the outer circumferential surface of the receiving wall 42 A in a range of 4 o'clock to 6 o'clock.
- the outer circumferential surface of the receiving wall 42 A over the range of 4 o'clock to 6 o'clock substantially extends towards the position of 3 o'clock for reinforcement.
- FIGS. 5A and 5B show another state in which the piston 20 starts to move from the top dead center toward the bottom dead center so as to perform a suction work. While the piston 20 moves from the top dead center toward the bottom dead center, the refrigerant gas is drawn from the suction chamber 22 into the cylinder bore 12 A. In an early stage of the movement until inertia force of the piston 20 exceeds in tensile force that is applied to the piston 20 rearward due to negative pressure in the cylinder bore 12 A, the piston 20 experiences force that meets the tensile force and the inertia force rearward. That is, as shown in FIG.
- the piston 20 receives a reactive force Fp from the swash plate 18 through the shoe 21 in a perpendicular direction to a sliding surface between the swash plate 18 and the shoes 21 as shown by an arrow.
- a magnitude of the reactive force Fp meets that of the rearward force.
- the reactive force Fp is based on an inclining angle of the swash plate 18 .
- the reactive force Fp is decomposed into a first component of force Fp 1 and a second component of force Fp 2 as shown by arrows on a plane that includes the hypothetical straight line L 1 and the longitudinal axis of the piston 20 in FIG. 5A.
- the first component force Fp 1 as indicated in the arrow acts in parallel to the longitudinal axis of the cylinder bore 12 A, although the cylinder bore 12 A is not illustrated in FIG. 5A but in FIG. 1.
- the second component force Fp 2 as shown by the arrow acts in parallel to the hypothetical straight line L 1 on a plane perpendicular to the longitudinal axis of the cylinder bore 12 A.
- the piston 20 receives a reactive force in the opposite direction to the second component force Fp 2 from the inner circumferential surface of the cylinder bore 12 A.
- the second component force Fp 2 is in the direction of the straight line that connects 12 o'clock to 6 o'clock.
- a magnitude of the reactive force is equal to that of the second component force Fp 2 .
- the reactive force Fp 1 functions as a tensile force to pull the connecting portion 42 through the coupler 41 A and an upper region of the partially cut disk 41 C frontward along the longitudinal axis of the piston 20 .
- the tensile force is effectively received by the guide wall 42 B.
- the reactive force Fp is decomposed into a third component of force Fp 3 and a fourth component of force Fp 4 as shown by arrows on a plane that includes a straight line connecting 3 o'clock to 9 o'clock and the longitudinal axis of the piston 20 in FIG. 5B.
- the third component force Fp 3 acts in the axial direction of the cylinder bore 12 A.
- the fourth component force Fr 4 acts in the perpendicular direction to the hypothetical straight line L 1 in the plane perpendicular to the axial direction of the cylinder bore 12 A.
- external force acts on the piston 20 in a such manner that the neck portion 41 is pulled downward in FIG.
- the fourth component force Fp 4 functions as a tensile force.
- the tensile force is applied to the connecting portion 42 substantially at the position of 9 o'clock of the piston 20 .
- the tensile force is effectively received by the guide wall 42 B, which is formed substantially at the position of 9 o'clock on the following side in the rotating direction of the swash plate 18 .
- the frictional force generated between the rotating swash plate 18 and the shoes 21 is further applied to the piston 20 in the rotating direction of the swash plate 18 or substantially in the direction from 9 o'clock toward 3 o'clock.
- the inclination angle of the swash plate 18 approaches to the minimum inclination angle by an urging force of the spring that is not illustrated in the drawings.
- the displacement approaches to zero.
- the swash plate 18 pushes the piston 20 to move from the bottom dead center toward the top dead center.
- the urge generates a component of force that pushes the piston 20 in an upward direction.
- the component force is effectively received by the guide wall 42 B substantially at the position of 12 o'clock. In a sense, the above component force could generate a twist of the piton 20 with respect to the cylinder bore 12 A.
- the guide wall 42 B longitudinally extends from the upside of the head portion 40 toward the neck portion 41 , the twist does not tend to occur. Therefore, the piston 20 smoothly moves toward the top dead center, and the swash plate 18 is also moved toward the minimum inclination angle. While the compressor C does not require the discharge or the compression of the refrigerant, the compressor C is stopped. In this state, the swash plate 18 is moved toward the minimum inclination angle to prepare for the next activation of the compressor C.
- the outer circumferential surface of the guide wall 42 B of the piston 20 is formed so as to substantially extend from 12 o'clock to 9 o'clock.
- the strength of the connecting portion 42 against the tensile force is sufficiently ensured by the guide wall 42 B.
- the outer circumferential surface of the connecting portion 42 of the piston 20 is formed to be substantially symmetrical with respect to the axis of the piston 20 by the guide wall 42 B. Thereby, the guide wall 42 B effectively functions when the piston 20 is machined by centerless machining.
- the connecting portion 42 that connects the head portion 40 to the neck portion 41 is formed by the receiving wall 42 A, the guide wall 42 B and the flat reinforcement 420 .
- the weight of the piston 20 is reduced in comparison to another structure whose connecting portion is formed to be a solid cylinder.
- the guide wall 42 B is formed on the following side in the rotating direction of the swash plate 18 on the upper portion of the piston 20 .
- the piston 20 is more accurately held when the piston 20 is machined by centerless machining in the above structure.
- the piston 20 is as a whole integrally molded by the die unit that includes the movable dies, which are movable only in a single direction. Thereby, the piston 20 is easily formed to be one structural piece by die casting. Therefore, as compared to a structure whose a head portion and a neck portion are two separate pieces, a process for bonding one piece to another piece is not required in order to form a piston in the current structure. Accordingly, manufacturing cost is also reduced.
- the receiving wall 42 A is connected to the guide wall 42 B by the reinforcement 42 C.
- the rigidity of the piston 20 is improved by the reinforcement 42 c . Therefore, the strength of the piston 20 is improved against the force in the axial direction of the piston 20 such as the compression reactive force.
- the cross section of the connecting portion 42 is substantially in the shape of S on the plane perpendicular to the axis of the piston 20 or the head portion 40 .
- the piston 20 when the piston 20 is molded by die casting, upon drawing the piston 20 from the die, it becomes relatively easy to set the direction of the movement of the die in a direction. Therefore, the structure of the die is simplified and the manufacturing cost is reduced.
- the outer circumferential surface of the receiving wall 42 A is formed substantially over the range of 3 o'clock to 6'oclock. Also, the outer circumferential surface of the guide wall 42 B is formed substantially over the range of 9 o'clock to 12 o'clock.
- side force is applied from the inner circumferential surface of the cylinder bore 12 A and is effectively received by the receiving wall 42 A.
- the piston 20 can be accurately held.
- the piston 20 is made of aluminum such as an aluminum alloy. Thus, the weight of the aluminum piston 20 is lighter than that of an iron piston.
- the reinforcement 42 C may not be necessarily formed so as to connect the receiving wall 42 A to the guide wall 42 B.
- the receiving wall 42 A, the guide wall 42 B and the reinforcement 42 C may be formed so as to leave a space between the receiving wall 42 A and the reinforcement 42 C and a space between the guide wall 42 B and the reinforcement 42 C. If the piston 20 maintains a predetermined strength level, the piston 20 does not necessarily require the reinforcement 42 C
- the connecting portion 42 is constituted as shown in FIG. 6. A cross-sectional view of a connecting portion 42 is viewed in a such manner that the rotating direction of the drive shaft 16 is clockwise. In FIG.
- the connecting portion 42 further includes only the receiving wall 42 A and the guide wall 42 B.
- the receiving wall 42 A and the guide wall 42 B are formed in a such manner that a top-end surface 42 D of the receiving wall 42 A at the position of 3 o'clock does not exceed a bottom-end surface 42 E of the guide wall 42 B at the position of 9 o'clock.
- direction of the die movement corresponds to the direction of the straight line that connects 3 o'clock to 9 o'clock
- the direction of the die movement may not necessarily correspond to the direction of the straight line that connects 3 o'clock to 9 o'clock.
- a reinforcement 42 C may be formed in a such manner that an end of the receiving wall 42 A at the position of 6 o'clock is connected to an end of the guide wall 42 B at the position of 12 o'clock.
- FIG. 7 is a cross-sectional view of the connecting portion 42 that is viewed in a such manner that the rotating direction of the drive shaft 16 is clockwise.
- the cross section of the connecting portion 42 is substantially in the shape of Z.
- the connecting portion 42 is viewed in a such manner that the rotating direction of the drive shaft 16 is counterclockwise, the cross section is substantially in the shape of S.
- the reinforcement 42 C is formed in a such manner that the top end of the reinforcement 42 C at the position of 12 o'clock does not exceed to the right of the bottom end of the reinforcement 42 C at the position of 6 o'clock.
- the reinforcement 42 C is not angled with respect to the straight line that connects 12 o'clock to 6 o'clock.
- the piston 20 may be integrally molded by a molding device that includes a plurality of dies that is movable in different directions from each other.
- a connecting portion includes a receiving wall, a guide wall and a reinforcement, and the cross-sectional shape of the connecting portion along the plane perpendicular to the axis of the piston 20 has an increased degree of freedom.
- the piston 20 is not be necessarily integrally formed as a whole. That is, the piston 20 includes of a plurality of members. In this case, the weight of the piston 20 is also reduced in comparison to another piston whose connecting portion is formed to be substantially solid. Also, in comparison to a structure whose that the receiving wall is formed on the preceding side of the rotating direction of the swash plate 18 and that the guide wall is not formed on the following side of the rotating direction of the swash plate 18 , the piston 20 is accurately held when the piston 20 is machined by centerless machining.
- the piston 20 is not molded by die casting.
- the piston 20 is formed, for example, by casting, forging or cutting.
- the receiving wall 42 A is not formed over the range of 3 o'clock to 6 o'clock.
- the receiving wall 42 A is formed, for example, over a range of 4 o'clock to 6 o'clock.
- the receiving wall 42 A may be formed over a narrower range than the range of 3 o'clock to 6 o'clock
- the guide wall 42 B is not formed over the range of 9 o'clock to 12 o'clock.
- the guide wall 42 B may be formed, for example, over a range of 10 o'clock to 12 o'clock.
- the guide wall 42 B may be formed over a narrower range than the range of 10 o'clock to 12 o'clock.
- the piston 20 may be constituted of metal such as an iron other than aluminum.
- the displacement control valve 30 is replaced by another displacement control valve whose opening degree of the supply passage 28 is variable by controlling an external control device.
- a stroke volume of the piston 20 is reduced, for example, by completely opening the supply passage 28 by controlling the control device.
- the compressor C is designed that a displacement of the refrigerant is substantially zero per revolution of the drive shaft 16 .
- the compressor C is also designed that the displacement of the refrigerant is not substantially zero per revolution of the drive shaft 16 when the displacement of the refrigerant is close to zero.
- a double-headed piston type compressor is employed in place of the single-headed piston type compressor C whose single-headed piston performs a compression work.
- the double-headed piston performs a compression work in cylinder bores formed on the front and rear sides of a crank chamber.
- the compressor C may be a fixed displacement type of which stroke volume of the piston 20 is fixed.
- the compressor C is employed as a fluid machine.
- an oil pump and an air pump may be employed in place of the compressor C.
- 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 of the appended claims.
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Abstract
A piston is used in a fluid machine. The fluid machine has a drive shaft and a cam plate operatively connected to the drive shaft. The drive shaft integrally rotates with the cam plate in a housing. The piston has a head portion, a neck portion, a receiving wall and a guide wall. The head portion is accommodated in a cylinder bore in the housing. The neck portion is operatively connected to the cam plate. The receiving wall integrally connects the head portion and the neck portion on the drive shaft side. The receiving wall is formed substantially on a preceding side in a rotating direction of the cam plate. The guide wall integrally connects the head portion and the neck portion on an opposite side of the drive shaft side. The guide wall is formed substantially on a following side in the rotating direction of the cam plate.
Description
- The present invention relates to a piston for a fluid machine and to the fluid machine. The piston has a receiving wall for receiving side force and a guide wall between a head portion in a cylinder bore and a neck portion that is operatively connected to a cam plate.
- For example, in a piston type compressor that compresses a refrigerant by a reciprocation of a piston in a cylinder bore, a cavity is conventionally formed in a connecting portion between a head portion and a neck portion of the piston to reduce the weight of the piston. Japanese Unexamined Patent Publication No. 2000-274350 discloses the above type of piston in which a cavity is formed in a portion corresponding to the connecting portion of the piston. In addition, a receiving wall for receiving side force is formed at the connecting portion on the downside of the head portion. A guide wall is formed at the connecting portion on the upside of the head portion. The receiving wall is formed on a preceding side in a rotating direction of a swash plate. The swash plate functions as a cam plate that reciprocates the piston. Thereby, the receiving wall effectively receives the side force from the inner circumferential surface of a cylinder bore.
- Note that the upside of the head portion is further away from a drive shaft of a fluid machine while the downside is closer to the drive shaft. In the above structure, however, the receiving wall is not formed on a following side in the rotating direction of the swash plate. In other words, the receiving wall and the guide wall are not satisfactorily balanced with respect to a central axis of the head portion. Therefore, in the above structure, if the piston is polished and ground by a centerless machining process, it is hard to ensure the accuracy of machining. The centerless machining is a machining method of polishing and grinding by contacting a machining tool such as a grind stone with the piston under the condition that the rotary center of the piston as a work piece is not chucked but the outer circumferential surface of the piston is radially pressed by using a support member such as a roller. As a result, it is hard to accurately hold the piston. In contrast, as pressing force or contact pressure that is applied from the support member such as a roller and the machining tool to the piston is close to each other, the accuracy of machining is improved. In the above improved structure, however, the receiving wall and the guide wall are imbalanced with respect to the central axis of the head portion. Therefore, the pressing force of the support member and the machining tool hardly become equal to each other. Consequently, it becomes hard to ensure the accuracy of machining.
- The present invention is directed to a piston for a fluid machine and the its reduced manufacturing cost due to not only the reduced weight of the piston but also a centerless machining.
- According to the present invention, a piston is used in a fluid machine. The fluid machine has a drive shaft and a cam plate that is operatively connected to the drive shaft. The drive shaft integrally rotates with the cam plate in a housing. The piston has a head portion, a neck portion, a receiving wall and a guide wall. The head portion is accommodated in a cylinder bore that is formed in the housing. The neck portion is operatively connected to the cam plate through a pair of shoes. The receiving wall integrally connects the head portion and the neck portion on the drive shaft side. The receiving wall is formed substantially on a preceding side in a rotating direction of the cam plate. The guide wall integrally connects the head portion and the neck portion on an opposite side of the drive shaft side. The guide wall is formed substantially on a following side in the rotating direction of the cam plate.
- Furthermore, the present invention has a following second feature. A fluid machine has a housing, a drive shaft and a piston. The drive shaft is rotatably supported in the housing. The piston is operatively connected to the drive shaft and exerts pressure on fluid. The piston includes a head portion, a neck portion, a receiving wall and a guide wall. The head portion is accommodated in a cylinder bore that is formed in the housing. The neck portion is operatively connected to the drive shaft. The receiving wall integrally connects the head portion and the neck portion on the drive shaft side. The receiving wall is formed substantially on a preceding side in a rotating direction of the drive shaft. The guide wall integrally connects the head portion and the neck portion on an opposite side of the drive shaft side. The guide wall is formed substantially on a following side in the rotating direction of the drive shaft.
- Furthermore, the present invention has a following third feature. A piston type compressor has a housing, a drive shaft, a cam plate and a plurality of pistons. The drive shaft is rotatably supported in the housing. The cam plate is supported by the drive shaft. The cam plate is rotated by the rotation of the drive shaft. The plurality of pistons is operatively connected to the cam plate and compresses refrigerant gas. The rotation of the cam plate is converted into a reciprocating movement of the piston. The piston includes a head portion, a neck portion, a receiving wall and a guide wall. The head portion is accommodated in a cylinder bore that is formed in the housing. The neck portion is operatively connected to the cam plate. The receiving wall integrally connects the head portion and the neck portion on a side of the drive shaft. The receiving wall is formed substantially on a preceding side in a rotating direction of the cam plate. The guide wall integrally connects the head portion and the neck portion on an opposite side of the drive shaft. The guide wall is formed substantially on a following side in the rotating direction of the cam plate.
- The features of the present invention that are believed to be novel are set forth with particularity in the appended claims. 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 variable displacement single-head piston type compressor according to a preferred embodiment of the present invention;
- FIG. 2 is a perspective view of a piston for use in the variable displacement single-head piston type compressor according to the preferred embodiment of the present invention;
- FIG. 3 is an enlarged cross-sectional view of the piston taken along the line III-III in FIG. 1;
- FIG. 4A is a partial side view of a swash plate, a pair of shoes and the piston according to the preferred embodiment of the present invention. The piston is positioned near the top dead center while the piston is in transition from a bottom dead center toward a top dead center;
- FIG. 4B is a partial top view of the swash plate, the pair of shoes and the piston according to the preferred embodiment of the present invention. The piston is positioned near the top dead center while the piston is in transition from the bottom dead center toward the top dead center;
- FIG. 5A is a partial side view of the swash plate, the pair of shoes and the piston according to the preferred embodiment of the present invention. The piston is positioned at an early stage while the piston is in transition from the top dead center toward the bottom dead center;
- FIG. 5B is a partial top view of the swash plate, the pair of shoes and the piston according to the preferred embodiment of the present invention. The piston is positioned at the early stage while the piston is in transition from the top dead center toward the bottom dead center;
- FIG. 6 is a cross-sectional view of a connecting portion of the piston according to another preferred embodiment of the present invention;
- FIG. 7 is a cross-sectional view of a connecting portion of the piston according to yet another preferred embodiment of the present invention; and
- FIG. 8 is an enlarged cross-sectional view of the piston taken in FIG. 3, which is manufactured by using movable dies and a stationary die.
- A piston for a fluid machine according to a preferred embodiment of the present invention will now be described with reference to FIGS. 1 through 5.
- FIG. 1 illustrates a variable displacement single-head piston type compressor C (hereinafter a compressor) or a fluid machine that is applied to a vehicle air conditioner. In the drawing, left and right sides of FIG. 1 respectively represents front and rear. A
front housing 11, acylinder block 12 and arear housing 13 form a housing of a compressor C or a compressor housing. The rear end of thefront housing 11 is fixedly secured to the front end of thecylinder block 12 that is a center housing. The front end of therear housing 13 is fixedly secured to the rear end of the cylinder block through avalve plate assembly 14. Although only one blot is illustrated in FIG. 1, the compressor housing and thevalve plate assembly 14 are fixedly secured by bolting therear housing 13 with a plurality ofbolts 10 through thefront housing 11, thecylinder block 12 and thevalve plate assembly 14. Thefront housing 11 and thecylinder block 12 define a crankchamber 15. A drive shaft 16 that drives the compressor C is rotatably supported by thefront housing 11 and thecylinder block 12 so as to pass through thecrank chamber 15. Although not shown in the drawing, the drive shaft 16 is operatively connected to a vehicle engine that is an external drive source through a clutch mechanism such as an electromagnetic clutch. - Still referring to FIG. 1, rotation is converted into reciprocating motion. A lug plate17 is fixedly mounted on the drive shaft 16 in the
crank chamber 15. A cam plate or aswash plate 18 is connected to the drive shaft 16 so that theswash plate 18 integrally rotates with the drive shaft 16 through ahinge mechanism 19 and inclines with respect to a central axis L of the drive shaft 16. A plurality of cylinder bores 12A is formed in thecylinder block 12 around the axis L of the drive shaft 16 although only one cylinder bore is illustrated in the drawing. Also, a piston for a fluid machine or a single-head piston 20 is accommodated in each cylinder bore 12A. Eachpiston 20 is engaged with theswash plate 18 through a pair ofshoes 21. The rotary motion of the drive shaft 16 is converted into the reciprocation of eachpiston 20 along the respective cylinder bores 12A through the lug plate 17, thehinge mechanism 19, theswash plate 18 and theshoes 21. The drive shaft 16, the lug plate 17, thehinge mechanism 19 and theshoes 21 constitute a driving unit of thepiston 20. - Refrigerant gas is compressed by the reciprocating motion. A
suction chamber 22 and adischarge chamber 23 are defined between therear housing 13 and thevalve plate assembly 14. Thevalve plate assembly 14 further includes asuction port 24, asuction valve 25, adischarge port 26 and adischarge valve 27. The refrigerant gas in thesuction chamber 22 is drawn into the corresponding cylinder bore 12A through the associatedsuction port 24 by pushing away the associatedsuction valve 25 while thepiston 20 moves frontward (or from right to left in FIG. 1). The refrigerant gas drawn into the cylinder bore 12A is compressed to a predetermined pressure level and is discharged into thecorresponding discharge chamber 23 through the associateddischarge port 26 by pushing away the associatedsuction valve 27 while thepiston 20 moves rearward (or from left to right in FIG. 1). Asupply passage 28 connects thedischarge chamber 23 with thecrank chamber 15. Ableed passage 29 connects thecrank chamber 15 with thesuction chamber 22. Adisplacement control valve 30 is placed in thesupply passage 28. Apressure sensing passage 31 connects thedisplacement control valve 30 with thesuction chamber 22. - Still referring to FIG. 1, the compression is controlled by the
displacement control valve 30. Thedisplacement control valve 30 further includes adiaphragm 30A and avalve body 30B. Thevalve body 30B is opened and closed bydiaphragm 30A that reacts to the pressure in thesuction chamber 22 through thepressure sensing passage 31. Thereby, the opening degree of thesupply passage 28 is varied to control the amount of the refrigerant gas that is introduced into thecrank chamber 15. On the other hand, the refrigerant gas in thecrank chamber 15 is introduced into thesuction chamber 22 through thebleed passage 29. Thereby, the pressure in thecrank chamber 15 is varied. Since the pressure differential between thecrank chamber 15 and the cylinder bore 12A applied to thepiston 20 changes, the inclination angle of theswash plate 18 is also varied. Consequently, a piston stroke is varied, and a displacement is adjusted. - In the present embodiment, a spring is placed between the lug plate17 that is mounted on the drive shaft 16 and the
swash plate 18 although not shown in the drawing. On the other hand, acircular clip 16A is fixedly mounted on the drive shaft 16 behind theswash plate 18. Thereby, a minimum inclination angle of theswash plate 18 is restricted with respect to the perpendicular plane to the axis L of the drive shaft 16. At the minimum inclination angle of theswash plate 11 as shown in hypothetical two-dotted lines, theswash plate 18 contacts with thecircular clip 16A, which is fixedly mounted on the drive shaft 16. In addition, the compressor C is constructed in a such manner that the output displacement of thepiston 20 is approximately zero per rotation of the drive shaft 16. - Next, the constitution of the
piston 20 will be described in detail. As shown in FIGS. 1 and 2, thepiston 20 has ahead portion 40 accommodated in thecylinder bore 12A and aneck portion 41 connected to a distal portion of theswash plate 18 through theshoes 21. Thehead portion 40 and theneck portion 41 are designed to have a predetermined distance in the axial direction of thepiston 20. Thehead portion 40 and theneck portion 41 are connected by and integrally formed with a connectingportion 42. - The
head portion 40 is formed in a such manner that its outside cross-sectional diameter is approximately equal to the inside diameter of the cylinder bore 12A. Theneck portion 41 further includes acoupler 41A, which partially forms a shoe insertedportion 41B and a partially cutdisk 41C, which defines the outside diameter to approximately match the inside diameter of the cylinder bore 12A. The outer circumferential surface between thehead portion 40 and the partially cutdisk 41C constitute an outer circumferential surface of a hypothetical cylinder. - Still referring to FIGS. 1 and 2, a pair of concave
spherical surfaces 41D is provided at the front and rear sides of thepiston 20 so as to face each other in the shoe insertedportion 41B. The pair ofshoes 21 is substantially in the shape of hemisphere and sandwiches the front and rear surfaces of the distal portion of theswash plate 18. Theshoes 21 are received respectively by the corresponding concavespherical surfaces 41D in the shoe insertedportion 41B so as to freely slide. Thus, theshoes 21 slide relative to the front and rear surfaces of theswash plate 18 and enable thepiston 20 to reciprocate in the axial direction of thepiston 20 based on the rotary motion of theswash plate 18, which is integrally rotated with the drive shaft 16. - Since the
piston 20 is connected to theswash plate 18 through theshoes 21, thepiston 20 is not prevented from rotating around the axis of thepiston 20 or around a central axis of thehead portion 40. In the present embodiment, thepiston 20 has arotation restricting potion 41E for restricting the rotation of thepiston 20 around the axis of thepiston 20 due to the contact with an inner circumferential surface 11A of thefront housing 11 as shown in FIG. 1. For this reason, therotation restricting portion 41E is designed in a such manner that one of the circumferential ends of the rotation restricting portion 41F contacts the inner circumferential surface 11A of thefront housing 11 as thepiston 20 is about to rotate around the axis of thepiston 20. - As shown in FIGS. 1 through 3, the connecting
portion 42 has a receivingwall 42A for receiving side force that extends from the downside of thehead portion 40 to the partially cutdisk 41C of theneck portion 41 and aguide wall 42B that extends from the upper side of thehead portion 40 to the partially cutdisk 41C. The receivingwall 42A and theguide wall 42B are formed in a such manner that the outer circumferential surfaces of the receivingwall 42A and theguide wall 42B around the axis of thepiston 20 constitute an outer circumferential surface of the hypothetical cylinder as previously described. Note that the upside of thehead portion 40 is further away from the drive shaft 16 while the downside is closer to the drive shaft 16. - FIG. 3 illustrates the connecting
portion 42 in a cross-sectional view in which a rotating direction of the drive shaft 16 or theswash plate 18 is clockwise. The receivingwall 42A is formed on a preceding side in the rotating direction of theswash plate 18 or in the direction indicated by an arrow in FIG. 3. A hypothetical straight line Li extends through the central axes of the drive shaft 16 and thehead portion 40 as indicated in a dotted line in FIG. 3. The hypothetical straight line L1 and the outer circumferential surface of thehead portion 40 intersect at intersectional points P1 and P2. The intersectional point P1 is further from the axis of the drive shaft 16 than the intersectional point P2. In the present embodiment, when the position of the intersectional point P1 is referred to as 12 o'clock, the outer circumferential surface of the receivingwall 42A is formed substantially over a range of 3 o'clock to 6 o'clock. On the other hand, theguide wall 42B is formed on a following side in the rotating direction of theswash plate 18 or on an opposite side to the preceding side in the rotating direction of theswash plate 18. In the present embodiment, the outer circumferential surface of theguide wall 42B is formed substantially over a range of a 9'oclock position to a 12'oclock position. - The receiving
wall 42A is connected to theguide wall 42B by aflat reinforcement 42C. Thereinforcement 42C is formed in a such manner that it extends from the end of the receivingwall 42A at the position of 3 o'clock to the end of theguide wall 42B at the position of 9 o'clock Thereinforcement 42C also extends from thehead portion 40 to the partially cutdisk 41C. The connectingportion 42 includes the receivingwall 42A, theguide wall 42B and thereinforcement 42C. In addition, a cross section of the connectingportion 42 is substantially in the shape of S as shown in FIG. 3. - The
piston 20 is integrally molded with an aluminum alloy by die casting. In the present embodiment, as shown in FIG. 8, thepiston 20 is as a whole molded by a die unit during the molding process by die casting. The die unit includes a firstmovable die 43, a secondmovable die 44, a thirdmovable die 45 and astationary die 46. The firstmovable die 43, the secondmovable die 44 and the thirdmovable die 45 are movable only in a direction between 3 o'clock and 9 o'clock and are drawn in turn. Therefore, each end of the receivingwall 42A and theguide wall 42B is formed so as not to prevent the dies from being drawn. Then, the concavespherical surfaces 41D is formed by cutting, and the outer circumferential surfaces of thehead portion 40, theneck portion 41 and the connectingportion 42 are ground or polished. - Next, side force acting on the
piston 20 will be described in detail. Thepiston 20 experiences forces that include compression reactive force caused by the compression work of the refrigerant gas, inertia force caused by the reciprocating motion of thepiston 20 and rotational force of theswash plate 18 caused by friction between therotating swash plate 18 and theshoes 21. Based on these forces, reactive force from the inner circumferential surface of thecylinder bore 12A or side force also acts on thepiston 20. - FIGS. 4A and 4B show a state in which the
piston 20 is positioned near the top dead center where thepiston 20 has moved the most rightward position in FIG. 1. In detail, FIGS. 4A and 4B show the state in which thepiston 20 is moving from the bottom dead center side toward the top dead center side. Thepiston 20 receives the largest compression reactive force near the above-described top dead center. - As shown in FIG. 4A, the
piston 20 receives a reactive force Fr as shown in an arrow from theswash plate 18 through theshoe 21 in a perpendicular direction to a sliding surface between theswash plate 18 and theshoe 21. A magnitude of the reactive force Fr meets the magnitude of the compression reactive force and the inertia force. The reactive force Fr is based on the inclining state of theswash plate 18. The reactive force Fr is decomposed into a first component of force Fr1 and a second component of force Fr2 as shown by arrows on a plane that includes the hypothetical straight line L1 and the longitudinal axis of thepiston 20 in FIG. 4A. The first component force Fr1 as indicated in the arrow acts in parallel to the longitudinal axis of the cylinder bore 12A, although the cylinder bore 12A is not illustrated in FIG. 4A but in FIG. 1. The second component force Fr2 as shown by the arrow acts in parallel to the hypothetical straight line L1 on a plane perpendicular to the longitudinal axis of the cylinder bore 12A. In other words, thepiston 20 receives a reactive force whose magnitude is equal to that of the second component force Fr2 in the opposite direction to the second component force Fr2 from the inner circumferential surface of the cylinder bore 12A. Namely, the second component force Fr2 is in the direction of the straight line that connects 12 o'clock to 6 o'clock. - Also, as shown in a top view in FIG. 4B, the reactive force Fr is decomposed into a third component of force Fr3 and a fourth component of force Fr4 as shown by arrows on a plane that includes a straight line connecting 3 o'clock to 9 o'clock and the longitudinal axis of the
piston 20 or in FIG. 4B. The third component force Fr3 acts in the axial direction of the cylinder bore 12A. The fourth component force Fr4 acts in a perpendicular direction to the hypothetical straight line L1 in the plane perpendicular to the axial direction of the cylinder bore 12A. In other words, thepiston 20 receives a reactive force whose magnitude is equal to that of the fourth component force Fr4 in the opposite direction to the fourth component force Fr4 from the inner circumferential surface of the cylinder bore 12A. Namely, the fourth component force Fr4 is in the direction of the straight line that connects 3 o'clock to 9 o'clock. Furthermore, the frictional force caused by the rotatingswash plate 18 and theshoes 21 is applied to thepiston 20 in the rotating direction of theswash plate 18. Namely, the frictional force is substantially in the direction from 9 o'clock toward the 3 o'clock. - The second component force Fr2, the fourth component force Fr4 and the above frictional force function to incline the
piston 20 with respect to the axis of the cylinder bore 12A. Reactive force generated from the inner circumferential surface of the cylinder bore 12A due to the above combined force is effectively received by the receivingwall 42A, which is formed on the preceding side in the rotating direction of theswash plate 18 on the lower portion of thehead portion 40. Thereby, the inclination of thepiston 20 is substantially restrained. - Furthermore, a magnitude of the above reactive force that is applied from the inner circumferential surface of the cylinder bore12A to the
piston 20 has a maximum value near the top dead center while thepiston 20 moves from the bottom dead center to the top dead center. In addition, it is clearly confirmed by an experiment that the above reactive force is mainly applied to the outer circumferential surface of the receivingwall 42A in a range of 4 o'clock to 6 o'clock. In the present embodiment, the outer circumferential surface of the receivingwall 42A over the range of 4 o'clock to 6 o'clock substantially extends towards the position of 3 o'clock for reinforcement. - FIGS. 5A and 5B show another state in which the
piston 20 starts to move from the top dead center toward the bottom dead center so as to perform a suction work. While thepiston 20 moves from the top dead center toward the bottom dead center, the refrigerant gas is drawn from thesuction chamber 22 into the cylinder bore 12A. In an early stage of the movement until inertia force of thepiston 20 exceeds in tensile force that is applied to thepiston 20 rearward due to negative pressure in the cylinder bore 12A, thepiston 20 experiences force that meets the tensile force and the inertia force rearward. That is, as shown in FIG. 5A, thepiston 20 receives a reactive force Fp from theswash plate 18 through theshoe 21 in a perpendicular direction to a sliding surface between theswash plate 18 and theshoes 21 as shown by an arrow. A magnitude of the reactive force Fp meets that of the rearward force. - Still referring to FIG. 5A, the reactive force Fp is based on an inclining angle of the
swash plate 18. The reactive force Fp is decomposed into a first component of force Fp1 and a second component of force Fp2 as shown by arrows on a plane that includes the hypothetical straight line L1 and the longitudinal axis of thepiston 20 in FIG. 5A. The first component force Fp1 as indicated in the arrow acts in parallel to the longitudinal axis of the cylinder bore 12A, although the cylinder bore 12A is not illustrated in FIG. 5A but in FIG. 1. The second component force Fp2 as shown by the arrow acts in parallel to the hypothetical straight line L1 on a plane perpendicular to the longitudinal axis of the cylinder bore 12A. In other words, thepiston 20 receives a reactive force in the opposite direction to the second component force Fp2 from the inner circumferential surface of the cylinder bore 12A. Namely, the second component force Fp2 is in the direction of the straight line that connects 12 o'clock to 6 o'clock. A magnitude of the reactive force is equal to that of the second component force Fp2. - The reactive force Fp1 functions as a tensile force to pull the connecting
portion 42 through thecoupler 41A and an upper region of the partially cutdisk 41C frontward along the longitudinal axis of thepiston 20. The tensile force is effectively received by theguide wall 42B. - Also, as shown in a top view in FIG. 5B, the reactive force Fp is decomposed into a third component of force Fp3 and a fourth component of force Fp4 as shown by arrows on a plane that includes a straight line connecting 3 o'clock to 9 o'clock and the longitudinal axis of the
piston 20 in FIG. 5B. The third component force Fp3 acts in the axial direction of the cylinder bore 12A. The fourth component force Fr4 acts in the perpendicular direction to the hypothetical straight line L1 in the plane perpendicular to the axial direction of the cylinder bore 12A. In other words, external force acts on thepiston 20 in a such manner that theneck portion 41 is pulled downward in FIG. 5B by the fourth component force Fp4. In this state, the fourth component force Fp4 functions as a tensile force. The tensile force is applied to the connectingportion 42 substantially at the position of 9 o'clock of thepiston 20. The tensile force is effectively received by theguide wall 42B, which is formed substantially at the position of 9 o'clock on the following side in the rotating direction of theswash plate 18. Furthermore, the frictional force generated between therotating swash plate 18 and theshoes 21 is further applied to thepiston 20 in the rotating direction of theswash plate 18 or substantially in the direction from 9 o'clock toward 3 o'clock. - In the present embodiment, when the compressor C does not require discharge or compression of the refrigerant, the inclination angle of the
swash plate 18 approaches to the minimum inclination angle by an urging force of the spring that is not illustrated in the drawings. As a result, the displacement approaches to zero. At this time, theswash plate 18 pushes thepiston 20 to move from the bottom dead center toward the top dead center. Thereby, as theswash plate 18 is urged by the spring, the urge generates a component of force that pushes thepiston 20 in an upward direction. The component force is effectively received by theguide wall 42B substantially at the position of 12 o'clock. In a sense, the above component force could generate a twist of thepiton 20 with respect to the cylinder bore 12A. However, since theguide wall 42B longitudinally extends from the upside of thehead portion 40 toward theneck portion 41, the twist does not tend to occur. Therefore, thepiston 20 smoothly moves toward the top dead center, and theswash plate 18 is also moved toward the minimum inclination angle. While the compressor C does not require the discharge or the compression of the refrigerant, the compressor C is stopped. In this state, theswash plate 18 is moved toward the minimum inclination angle to prepare for the next activation of the compressor C. - In the present embodiment, the outer circumferential surface of the
guide wall 42B of thepiston 20 is formed so as to substantially extend from 12 o'clock to 9 o'clock. The strength of the connectingportion 42 against the tensile force is sufficiently ensured by theguide wall 42B. In addition, the outer circumferential surface of the connectingportion 42 of thepiston 20 is formed to be substantially symmetrical with respect to the axis of thepiston 20 by theguide wall 42B. Thereby, theguide wall 42B effectively functions when thepiston 20 is machined by centerless machining. - In the present embodiment, the following advantageous effects are obtained. (1) The connecting
portion 42 that connects thehead portion 40 to theneck portion 41 is formed by the receivingwall 42A, theguide wall 42B and theflat reinforcement 420. In the above structure, the weight of thepiston 20 is reduced in comparison to another structure whose connecting portion is formed to be a solid cylinder. - (2) The
guide wall 42B is formed on the following side in the rotating direction of theswash plate 18 on the upper portion of thepiston 20. For example, as compared to another structure whose receiving wall is formed on the preceding side in the rotating direction of theswash plate 18 but a guide wall is not formed on the following side in the rotating direction of theswash plate 18, thepiston 20 is more accurately held when thepiston 20 is machined by centerless machining in the above structure. This is because when thepiston 20 is machined by centerless machining, pressing force is applied from the support member and the machining tool to the piston The pressing force that is applied to theguide wall 42B and the receivingwall 42A of thepiston 20 approaches each other by extending theguide wall 42B on the following side in the rotating direction of theswash plate 18. For this reason, thepiston 20 is accurately machined. Thus, thepiston 20 is manufactured at a relatively short cycle time. In other words, manufacturing cost is reduced. - (3) The
piston 20 is as a whole integrally molded by the die unit that includes the movable dies, which are movable only in a single direction. Thereby, thepiston 20 is easily formed to be one structural piece by die casting. Therefore, as compared to a structure whose a head portion and a neck portion are two separate pieces, a process for bonding one piece to another piece is not required in order to form a piston in the current structure. Accordingly, manufacturing cost is also reduced. - (4) The receiving
wall 42A is connected to theguide wall 42B by thereinforcement 42C. In the above structure, the rigidity of thepiston 20 is improved by the reinforcement 42 c. Therefore, the strength of thepiston 20 is improved against the force in the axial direction of thepiston 20 such as the compression reactive force. - (5) The cross section of the connecting
portion 42 is substantially in the shape of S on the plane perpendicular to the axis of thepiston 20 or thehead portion 40. In the constitution, when thepiston 20 is molded by die casting, upon drawing thepiston 20 from the die, it becomes relatively easy to set the direction of the movement of the die in a direction. Therefore, the structure of the die is simplified and the manufacturing cost is reduced. - (6) The outer circumferential surface of the receiving
wall 42A is formed substantially over the range of 3 o'clock to 6'oclock. Also, the outer circumferential surface of theguide wall 42B is formed substantially over the range of 9 o'clock to 12 o'clock. In the above construction, side force is applied from the inner circumferential surface of thecylinder bore 12A and is effectively received by the receivingwall 42A. In addition, when thepiston 20 is machined by the centerless machining, thepiston 20 can be accurately held. - (7) The
piston 20 is made of aluminum such as an aluminum alloy. Thus, the weight of thealuminum piston 20 is lighter than that of an iron piston. - In the present invention, the following alternative embodiments are also practiced. The
reinforcement 42C may not be necessarily formed so as to connect the receivingwall 42A to theguide wall 42B. In other words, the receivingwall 42A, theguide wall 42B and thereinforcement 42C may be formed so as to leave a space between the receivingwall 42A and thereinforcement 42C and a space between theguide wall 42B and thereinforcement 42C. If thepiston 20 maintains a predetermined strength level, thepiston 20 does not necessarily require thereinforcement 42C In the above structure, the connectingportion 42 is constituted as shown in FIG. 6. A cross-sectional view of a connectingportion 42 is viewed in a such manner that the rotating direction of the drive shaft 16 is clockwise. In FIG. 6, the connectingportion 42 further includes only the receivingwall 42A and theguide wall 42B. In the structure of FIG. 6, the receivingwall 42A and theguide wall 42B are formed in a such manner that a top-end surface 42D of the receivingwall 42A at the position of 3 o'clock does not exceed a bottom-end surface 42E of theguide wall 42B at the position of 9 o'clock. Thereby, if the dies are movable only in a direction, thewhole piston 20 is integrally molded in the process of die casting. Note that the above direction of the die movement corresponds to the direction of the straight line that connects 3 o'clock to 9 o'clock The direction of the die movement may not necessarily correspond to the direction of the straight line that connects 3 o'clock to 9 o'clock. - As shown in FIG. 7, a
reinforcement 42C may be formed in a such manner that an end of the receivingwall 42A at the position of 6 o'clock is connected to an end of theguide wall 42B at the position of 12 o'clock. FIG. 7 is a cross-sectional view of the connectingportion 42 that is viewed in a such manner that the rotating direction of the drive shaft 16 is clockwise. The cross section of the connectingportion 42 is substantially in the shape of Z. When the connectingportion 42 is viewed in a such manner that the rotating direction of the drive shaft 16 is counterclockwise, the cross section is substantially in the shape of S. In the above structure of FIG. 7, thereinforcement 42C is formed in a such manner that the top end of thereinforcement 42C at the position of 12 o'clock does not exceed to the right of the bottom end of thereinforcement 42C at the position of 6 o'clock. Thereinforcement 42C is not angled with respect to the straight line that connects 12 o'clock to 6 o'clock. Thereby, if the dies are movable only in a direction, thewhole piston 20 is integrally molded in the process of die casting. Note that the above direction of the die movement corresponds to the direction of the straight line that connects 6 o'clock to 12 o'clock. - The
piston 20 may be integrally molded by a molding device that includes a plurality of dies that is movable in different directions from each other. In this case, since thepiston 20 is not necessarily integrally molded by the dies that are movable only in a direction, the shape of thepiston 20 is not restricted. For example, a connecting portion includes a receiving wall, a guide wall and a reinforcement, and the cross-sectional shape of the connecting portion along the plane perpendicular to the axis of thepiston 20 has an increased degree of freedom. - In another alternative embodiment, the
piston 20 is not be necessarily integrally formed as a whole. That is, thepiston 20 includes of a plurality of members. In this case, the weight of thepiston 20 is also reduced in comparison to another piston whose connecting portion is formed to be substantially solid. Also, in comparison to a structure whose that the receiving wall is formed on the preceding side of the rotating direction of theswash plate 18 and that the guide wall is not formed on the following side of the rotating direction of theswash plate 18, thepiston 20 is accurately held when thepiston 20 is machined by centerless machining. - In yet another alternative embodiment, the
piston 20 is not molded by die casting. Thepiston 20 is formed, for example, by casting, forging or cutting. The receivingwall 42A is not formed over the range of 3 o'clock to 6 o'clock. The receivingwall 42A is formed, for example, over a range of 4 o'clock to 6 o'clock. As long as a predetermined strength of thepiston 20 is maintained, the receivingwall 42A may be formed over a narrower range than the range of 3 o'clock to 6 o'clock Similarly, theguide wall 42B is not formed over the range of 9 o'clock to 12 o'clock. Theguide wall 42B may be formed, for example, over a range of 10 o'clock to 12 o'clock. As long as a predetermined strength of thepiston 20 is maintained, theguide wall 42B may be formed over a narrower range than the range of 10 o'clock to 12 o'clock. Thepiston 20 may be constituted of metal such as an iron other than aluminum. - In other alternative embodiments, the
displacement control valve 30 is replaced by another displacement control valve whose opening degree of thesupply passage 28 is variable by controlling an external control device. In this case, a stroke volume of thepiston 20 is reduced, for example, by completely opening thesupply passage 28 by controlling the control device. - There are other alternative embodiments. The compressor C is designed that a displacement of the refrigerant is substantially zero per revolution of the drive shaft16. However, the compressor C is also designed that the displacement of the refrigerant is not substantially zero per revolution of the drive shaft 16 when the displacement of the refrigerant is close to zero. A double-headed piston type compressor is employed in place of the single-headed piston type compressor C whose single-headed piston performs a compression work. The double-headed piston performs a compression work in cylinder bores formed on the front and rear sides of a crank chamber. Furthermore, the compressor C may be a fixed displacement type of which stroke volume of the
piston 20 is fixed. - In the above-described embodiment, the compressor C is employed as a fluid machine. However, an oil pump and an air pump may be employed in place of the compressor C. 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 of the appended claims.
Claims (26)
1. A piston to be used in a fluid machine, the fluid machine having a drive shaft and a cam plate operatively connected to the drive shaft, the drive shaft integrally rotating with the cam plate in a housing, the piston comprising:
a head portion accommodated in a cylinder bore formed in the housing;
a neck portion operatively connected to the cam plate through a pair of shoes;
a receiving wall integrally connecting the head portion and the neck portion on the drive shaft side, the receiving wall being formed substantially on a preceding side in a rotating direction of the cam plate; and
a guide wall integrally connecting the head portion and the neck portion on an opposite side of the drive shaft side, the guide wall being formed substantially on a following side in the rotating direction of the cam plate.
2. The piston according to claim 1 wherein the piston is integrally molded as a whole by a die unit that includes a movable die, which is movable only in a direction.
3. The piston according to claim 1 further comprising a reinforcement for connecting the receiving wall to the guide wall.
4. The piston according to claim 3 wherein the receiving wall, the guide wall and the reinforcement substantially define a shape of S in a cross section along a plane perpendicular to a longitudinal axis of the piston.
5. The piston according to claim 1 wherein the piston is viewed in a cross section along a plane perpendicular to the axial direction of the drive shaft in a such manner that the drive shaft is rotated clockwise, an outer circumferential surface of the receiving wall being formed at least over a range of 4 o'clock to 6 o'clock, an outer circumferential surface of the guide wall being formed at least over a range of 10 o'clock to 12 o'clock, the 12 o'clock being located at the top of the cross section.
6. The piston according to claim 5 wherein the outer circumferential surface of the receiving wall is formed substantially over a range of 3 o'clock to 6 o'clock, the outer circumferential surface of the guide wall being formed substantially over a range of 9 o'clock to 12 o'clock.
7. The piston according to claim 6 further comprising a reinforcement for connecting the receiving wall at the position of 3 o'clock to the guide wall at the position of 9 o'clock.
8. The piston according to claim 6 further comprising a reinforcement for connecting the receiving wall at the position of 6 o'clock to the guide wall at the position of 12 o'clock.
9. The piston according to claim 1 , wherein the receiving wall and the guide wall are formed substantially symmetrically with respect to a longitudinal axis of the piston.
10. The piston according to claim 1 , wherein an outer circumferential surface of the receiving wall and the guide wall is slidable relative to an inner circumferential surface of the cylinder bore.
11. The piston according to claim 1 wherein the piston as a whole is made of aluminum.
12. A fluid machine comprising:
a housing;
a drive shaft rotatably supported in the housing; and
a piston operatively connected to the drive shaft for exerting pressure on fluid, the piston further including;
a head portion accommodated in a cylinder bore formed in the housing;
a neck portion operatively connected to the drive shaft;
a receiving wall connecting the head portion and the neck portion on the drive shaft side, the receiving wall being formed substantially on a preceding side in a rotating direction of the drive shaft; and
a guide wall connecting the head portion and the neck portion on an opposite side of the drive shaft side, the guide wall being formed substantially on a following side in the rotating direction of the drive shaft.
13. The piston according to claim 12 wherein the piston is integrally molded as a whole by a die unit that includes a movable die, which is movable only in a direction.
14. The piston according to claim 12 further comprising a reinforcement for connecting the receiving wall to the guide wall.
15. The piston according to claim 14 wherein the receiving wall, the guide wall and the reinforcement substantially define a shape of S in a cross section along a plane perpendicular to a longitudinal axis of the piston.
16. The piston according to claim 12 wherein the piston is viewed in a cross section along a plane perpendicular to the axial direction of the drive shaft in a such manner that the drive shaft is rotated clockwise, an outer circumferential surface of the receiving wall being formed at least over a range of 4 o'clock to 6 o'clock, an outer circumferential surface of the guide wall being formed at least over a range of 10 o'clock to 12 o'clock, the 12 o'clock being located at the top of the cross section.
17. The piston according to claim 12 wherein the piston as a whole is made of aluminum.
18. A piston type compressor comprising:
a housing;
a drive shaft rotatably supported in the housing;
a cam plate supported by the drive shaft, the cam plate being rotated by the rotation of the drive shaft; and
a plurality of pistons operatively connected to the cam plate for compressing refrigerant gas, the rotation of the cam plate being converted into a reciprocating movement of the piston, the piston further including,
a head portion accommodated in a cylinder bore formed in the housing;
a neck portion operatively connected to the cam plate;
a receiving wall connecting the head portion and the neck portion on the drive shaft side, the receiving wall being formed substantially on a preceding side in a rotating direction of the cam plate; and
a guide wall connecting the head portion and the neck portion on an opposite side of the drive shaft side, the guide wall being formed substantially on a following side in the rotating direction of the cam plate.
19. The piston according to claim 18 wherein the piston is as a whole integrally molded by a die unit that includes a movable die, which is movable only in a direction.
20. The piston according to claim 18 further comprising a reinforcement for connecting the receiving wall to the guide wall.
21. The piston according to claim 20 wherein the receiving wall, the guide wall and the reinforcement substantially define a shape of S in a cross section along a plane perpendicular to a longitudinal axis of the piston.
22. The piston according to claim 18 wherein the piston is viewed in a cross section along a plane perpendicular to the axial direction of the drive shaft in a such manner that the drive shaft is rotated clockwise, an outer circumferential surface of the receiving wall being formed at least over a range of 4 o'clock to 6 o'clock, an outer circumferential surface of the guide wall being formed at least over a range of 10 o'clock to 12 o'clock, the 12 o'clock being located at the top of the cross section.
23. The piston according to claim 22 wherein the outer circumferential surface of the receiving wall is formed substantially over a range of 3 o'clock to 6 o'clock, the outer circumferential surface of the guide wall being formed substantially over a range of 9 o'clock to 12 o'clock.
24. The piston according to claim 23 further comprising a reinforcement for connecting the receiving wall at the position of 3 o'clock to the guide wall at the position of 9 o'clock.
25. The piston according to claim 23 further comprising a reinforcement for connecting the receiving wall at the position of 6 o'clock to the guide wall at the position of 12 o'clock.
26. The piston according to claim 18 wherein the piston as a whole is made of aluminum.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2001322746A JP2003129954A (en) | 2001-10-19 | 2001-10-19 | Piston for fluid machinery and fluid machinery |
JPP2001-322746 | 2001-10-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
US20030075041A1 true US20030075041A1 (en) | 2003-04-24 |
Family
ID=19139743
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US10/272,118 Abandoned US20030075041A1 (en) | 2001-10-19 | 2002-10-16 | Piston for fluid machine and the fluid machine having the same |
Country Status (3)
Country | Link |
---|---|
US (1) | US20030075041A1 (en) |
JP (1) | JP2003129954A (en) |
DE (1) | DE10248724A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107651214A (en) * | 2017-10-10 | 2018-02-02 | 南京航空航天大学 | Multi-rotor unmanned aerial vehicle overall test device and its test method |
Citations (10)
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---|---|---|---|---|
US4470761A (en) * | 1980-11-27 | 1984-09-11 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Swash plate type compressor |
US4548254A (en) * | 1983-06-30 | 1985-10-22 | Borg-Warner Corporation | Method of manufacturing a die-cast wobble plate assembly |
US5765464A (en) * | 1996-03-19 | 1998-06-16 | Sanden Corporation | Reciprocating pistons of piston-type compressor |
US5899135A (en) * | 1996-05-21 | 1999-05-04 | Sanden Corporation | Reciprocating pistons of piston type compressor |
US5941161A (en) * | 1996-12-06 | 1999-08-24 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressor |
US5953980A (en) * | 1996-10-25 | 1999-09-21 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressors |
US6422129B1 (en) * | 1998-04-17 | 2002-07-23 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Swash plate type refrigerant compressor |
US6484621B1 (en) * | 1999-05-28 | 2002-11-26 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Swash plate type compressor wherein piston head has inner sliding portion for reducing local wear |
US6513417B1 (en) * | 1999-11-08 | 2003-02-04 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Single-headed swash-plate-type compressor with hollowed and ribbed piston |
US6575080B1 (en) * | 1999-09-24 | 2003-06-10 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Single-headed piston for swash plate type compressor wherein head portion has a curved surface at axial end |
-
2001
- 2001-10-19 JP JP2001322746A patent/JP2003129954A/en active Pending
-
2002
- 2002-10-16 US US10/272,118 patent/US20030075041A1/en not_active Abandoned
- 2002-10-18 DE DE10248724A patent/DE10248724A1/en not_active Withdrawn
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4470761A (en) * | 1980-11-27 | 1984-09-11 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Swash plate type compressor |
US4548254A (en) * | 1983-06-30 | 1985-10-22 | Borg-Warner Corporation | Method of manufacturing a die-cast wobble plate assembly |
US5765464A (en) * | 1996-03-19 | 1998-06-16 | Sanden Corporation | Reciprocating pistons of piston-type compressor |
US5899135A (en) * | 1996-05-21 | 1999-05-04 | Sanden Corporation | Reciprocating pistons of piston type compressor |
US5953980A (en) * | 1996-10-25 | 1999-09-21 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressors |
US5941161A (en) * | 1996-12-06 | 1999-08-24 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressor |
US6422129B1 (en) * | 1998-04-17 | 2002-07-23 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Swash plate type refrigerant compressor |
US6484621B1 (en) * | 1999-05-28 | 2002-11-26 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Swash plate type compressor wherein piston head has inner sliding portion for reducing local wear |
US6575080B1 (en) * | 1999-09-24 | 2003-06-10 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Single-headed piston for swash plate type compressor wherein head portion has a curved surface at axial end |
US6513417B1 (en) * | 1999-11-08 | 2003-02-04 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Single-headed swash-plate-type compressor with hollowed and ribbed piston |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107651214A (en) * | 2017-10-10 | 2018-02-02 | 南京航空航天大学 | Multi-rotor unmanned aerial vehicle overall test device and its test method |
Also Published As
Publication number | Publication date |
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JP2003129954A (en) | 2003-05-08 |
DE10248724A1 (en) | 2003-06-05 |
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AS | Assignment |
Owner name: KABUSHIKI KAISHA TOYOTA JIDOSHOKKI, JAPAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:ENOKIJIMA, FUMINOBU;KATO, TAKAYUKI;KATAYAMA, SEIJI;AND OTHERS;REEL/FRAME:013543/0066 Effective date: 20021031 |
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STCB | Information on status: application discontinuation |
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