Piston type compressor having arcuately shaped fluid port

Abstract

A suction port as a fluid port of a piston type compressor is contoured with reference to a middle line passing through a middle point of a maximum length of the suction port in the longitudinal direction of the suction valve and perpendicularly crossing a reference line extending in the longitudinal direction. The middle line divides the suction port into a first section positioned on the proximal end side and a second section positioned on the distal end side. An area of the second section is greater than an area of the first section. A width increasing region is disposed in which the width of the suction port becomes gradually greater from the proximal end side to the distal end side, and the length of the width increasing region occupies a major part of the maximum length of the suction port.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to a piston type compressor, having a gas flow structure, with a fluid port and a valve capable of flexural deformation for opening and closing the fluid port, for passing a gas through the fluid port, by pushing the valve open by the operation of each piston in the cylinder bore.

2. Description of the Related Art

When a gas is sucked from a suction chamber into a cylinder bore in a piston type compressor, the facility or ease of the inflow of the gas greatly affects the volumetric efficiency.

A suction port disclosed in Japanese Unexamined Patent Publication (Kokai) No. 57-97974 is circular and a suction port disclosed in Japanese Unexamined Patent Publication (Kokai) No. 2000-54961 is somewhat rounded and substantially triangular. A gas passing through the suction port from a suction chamber towards a cylinder bore exclusively flows in a direction perpendicular to a contour line of the suction port, as viewed from the reciprocating direction of a piston, (the circular port in Japanese Unexamined Patent-Publication (Kokai) No. 57-97974 and the rounded triangular port in No. 2000-54961) and enters the cylinder bore. The opening gap of the suction valve relative to the valve plate becomes progressively greater towards the distal end of the suction valve. It is therefore effective to let the gas passing through the suction port flow in the longitudinal direction of the suction valve from its distal end side in order to improve the facility of the inflow of the gas. The gas passing through the suction port exclusively flows in the direction perpendicular to the contour line that forms the hole of the suction port. Therefore, it can be said, in connection with the contour line of the suction port, that the greater the length of the contour line on the distal end side of the suction valve, the easier it becomes for the gas to flow towards the distal end side of the suction valve. The suction port described in Japanese Unexamined Patent Publication (Kokai) No. 2000-54961 is superior to the circular suction port described in Japanese Unexamined Patent Publication (Kokai) No. 57-97974 because the gas passing through the suction port can flow more easily from the distal end side of the suction valve in its longitudinal direction in the former than in the latter. Therefore, the ease of the inflow of the gas is higher in the suction port of Japanese Unexamined Patent Publication (Kokai) No. 2000-54961 than in the circular suction port of the Japanese Unexamined Patent Publication (Kokai) No. 57-97974.

The cross section of the suction port described in Japanese Unexamined Patent Publication (Kokai) No. 2000-54961 is formed in such a shape that the center of gravity of the area of the suction port is shifted toward the side of the proximal end of the suction valve. In this shape of the suction port, in the case where the suction port is divided into two sections so that the length of one section in the longitudinal direction of the suction valve is the same as that of another section, the length of a portion of a contour line of the suction port located on the side of the proximal end of the suction valve is greater than that of a portion of the contour line of the suction port located on the side of the distal end of the suction valve. This length relationship between the portions of the contour line cannot be said to optimum for the easy inflow of the gas toward the distal end side of the suction valve.

SUMMARY OF THE INVENTION

The object of the present invention is to provide a piston type compressor which can improve the ease of the inflow of the gas through a fluid port such as a suction port or a discharge port.

To accomplish this object, the present invention provides a piston type compressor comprising a housing having cylinder bores, and fluid ports in communication with the cylinder bores, pistons reciprocatingly arranged in the cylinder bores, a drive shaft rotatably supported by the housing, a transmission mechanism operatively coupled to the drive shaft and the pistons for converting rotation of the drive shaft into reciprocal movement of the pistons, and valves to open and close the fluid ports. The valve has a longitudinal direction, a proximal end and a distal end at the opposite end to the proximal end. A middle line is provided which passes through a middle point of a maximum length of the fluid port in the longitudinal direction of the valve, extends transversely with respect to the fluid port and perpendicularly crosses a reference line extending in the longitudinal direction of the valve. The middle line divides the fluid port into a first section positioned on the side of the proximal end portion of the valve and a second section positioned on the side of the distal end of the valve. An area of the second section is greater than an area of the first section.

The construction in which the area of the second section is greater than the area of the first section makes it easier for the gas passing through the fluid port to flow from the distal end side of the valve.

Preferably, a width increasing region is disposed in which the width of the fluid port in a direction of the middle line becomes gradually greater from the proximal end side to the distal end side of the valve in the longitudinal direction of the valve, and the length of the width increasing region in the direction of the reference line occupies a major part of the maximum length of the fluid port in the direction of the reference line.

The existence of the width increasing region makes it easier for the gas passing through the fluid port to flow towards the distal end side of the valve.

Preferably, a maximum width of the fluid port in the direction of the middle line exists in the second section and is greater than the maximum length of the fluid port in the direction of the reference line.

The construction in which the maximum length of the fluid port in the direction of the reference line is smaller than the maximum width of the fluid port in the direction of the middle line and the maximum width of the fluid port in the direction of the middle line exists on the side of the second section is convenient for increasing the length of the contour line of the fluid port on the distal end side of the valve.

Preferably, the fluid port has a contour line comprising a proximal end line positioned on the side of the proximal end of the valve, a distal end line positioned on the side of the distal end of the valve and a pair of right and left side lines, and the distal end line is longer than the proximal end line.

The construction wherein the length of the distal end line is greater than that of the proximal end line makes it easier for the gas passing through the fluid port to flow towards the distal end side of the valve.

Preferably, the distal end line comprises a convex curve protruding from the proximal end side to the distal end side of the valve.

The construction in which the distal end line comprises a convex curve is advantageous in bringing the distal end line closer to the circle of the circumferential surface of the cylinder bore. The closer the distal end line is to the circle of the circumferential surface of cylinder bore, the greater is the opened gap between the distal end line and the valve in the open condition.

Preferably, the contour line of the fluid port includes a pair of first connection lines connecting the proximal end line to the pair of side lines and a pair of second connection lines connecting the distal end line to the pair of side lines, the pair of first connection lines being smoothly connected to the proximal end line and the pair of said side lines, the pair of second connection lines being smoothly connected to the distal end line and the pair of side lines.

Preferably, the contour line of the suction port is an annular line with no corner. The construction wherein the contour line of the fluid port is an annular line with no corner is advantageous for preventing backflow of the gas in the fluid port.

Preferably, the contour line of the suction port is an annular convex line with no corner.

Preferably, the reference line extends substantially along the radial line of the circle of the circumferential surface of the cylinder bore.

The construction wherein the reference line extends substantially along the radial line of the circle of the circumferential surface of the cylinder bore is advantageous for bringing the contour line of the fluid port on the distal end side of the valve closer to the circle of the circumferential surface of the cylinder bore.

BRIEF DESCRIPTION OF THE DRAWINGS

The present invention will become more apparent from the following description of the preferred embodiments, with reference to the accompanying drawings, in which:

FIG. 1A is a sectional view of a compressor according to the first embodiment of the present invention, taken along the line IA—IA in FIG. 5 ;

FIG. 1B is an enlarged sectional view of a portion of FIG. 1A ;

FIG. 2 is a sectional view of the compressor, taken along line II—II in FIG. 1B ;

FIG. 3 is an enlarged perspective view of a portion of the compressor;

FIG. 4 is an enlarged view of the suction port;

FIG. 5 is a sectional view of a compressor according to the embodiment of the present invention;

FIG. 6A is an enlarged sectional view of a portion of a compressor according to the second embodiment of the present invention;

FIG. 6B is an enlarged view of the suction port of FIG. 6A ;

FIG. 7 is an enlarged view of the suction port according to the third embodiment;

FIG. 8 is an enlarged view of the suction port according to the fourth embodiment;

FIG. 9 is an enlarged view of the suction port according to the fifth embodiment;

FIG. 10 is an enlarged view of the suction port according to the sixth embodiment;

FIG. 11 is an enlarged view of the suction port according to the seventh embodiment; and

FIG. 12 is an enlarged view of the suction port according to the eighth embodiment.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

The first embodiment of the present invention applied to a variable capacity type compressor will now be explained with reference to FIGS. 1A to 5 .

Referring to FIG. 5 , a front housing 12 is coupled to the front end of a cylinder block 11 , and a rear housing 13 is fixed to the rear end of the cylinder block 11 via a partition plate 14 , valve-forming plates 15 and 16 and a retainer-forming plate 17 . A drive shaft 18 is rotatably supported by the front housing 12 and the cylinder block 11 which together form a control pressure chamber 121 . The drive shaft 18 protruding outward from the control pressure chamber 121 receives a driving force from an external driving source such as a car engine (not shown) through a pulley (not shown) and a belt (not shown).

A rotation support member 19 is anchored to the drive shaft 18 . The drive shaft 18 supports a swash plate 20 in such a fashion that the swash plate 20 can slide in an axial direction with respect to the drive shaft 18 and can incline. The swash plate 20 can incline with respect to the axis of the drive shaft 18 and can rotate with the drive shaft 18 , by the cooperation of a pair of guide pins 21 fixed to the swash plate 20 and a pair of guide holes 191 in the rotation support member 19 . The inclination movement of the swash plate 20 is guided by the slide guide relation between the guide hole 191 and the guide pin 21 as well as the slide support operation of the drive shaft 18 .

When the radial center portion of the swash plate 20 moves towards the rotation support member 19 , the angle of inclination of the swash plate 20 increases. When the radial center portion of the swash plate 20 moves towards the cylinder block 11 , the angle of inclination of the swash plate decreases. The minimum angle of inclination of the swash plate 20 is defined by the abutment of a circlip 22 fitted to the drive shaft 18 against the swash plate 20 . The maximum angle of inclination of the swash plate 20 is defined by the abutment of the rotary support member 19 against the swash plate 20 . The position of the swash plate 20 indicated by the solid line represents the position of the minimum angle of inclination of the swash plate 20 . The position of the swash plate 20 indicated by the chain line represents the position of the maximum angle of inclination of the swash plate 20 .

As shown in FIG. 1A , a plurality of cylinder bores 111 (five, in this embodiment) are formed in the cylinder block 11 . The cylinder bores 111 are disposed equidistantly about the drive shaft 18 . Pistons 23 are arranged in the cylinder bores 111 , as shown in FIG. 5 . The rotating motion of the swash plate 20 is converted into the reciprocating motion of the pistons 23 through shoes 24 , and the pistons 23 move back and forth in the cylinder bores 111 .

A suction chamber 131 and a discharge chamber 132 are defined in the rear housing 13 . The discharge chamber 132 surrounds the suction chamber 131 through a partition wall 133 . A supply passage 25 is arranged in the rear wall of the rear housing 13 .

As shown in FIGS. 2 and 5 , suction ports 26 , as fluid ports, are formed in the partition plate 14 , the valve-forming plate 16 . and the retainer-forming plate 17 corresponding to the cylinder bores 111 . Discharge ports 27 are formed in the partition plate 14 at positions corresponding to cylinder bores 111 . Suction valves 151 , as opening and closing valves, are formed in the valve-forming plate 15 , and discharge valves 161 are formed in the valve-forming plate 16 . Each of the suction valves 151 and the discharge valves 161 is integral with the associated valve-forming plate, and is thus fixed at its proximal end to the valve-forming plate while the substantial part thereof is flexible. A window 152 is formed in the proximal end portion of the suction valve 151 corresponding to the discharge port 27 . The distal end portion of the suction valve 151 , that undergoes flexural deformation, comes into, and out of, contact with the contact surface 141 of the partition plate 14 on the one side thereof and opens and closes the suction port 26 . The distal end portion of the discharge valve 161 , that undergoes flexural deformation, comes into, and out of, contact with the contact surface 142 of the partition plate 14 on the other side thereof and opens and closes the discharge port 27 . A maximum opening limiting recess 28 is formed in each cylinder bore 111 . The free end of the suction valve 151 can abut against the bottom of the maximum opening limiting recess 28 , and the maximum opening limiting recess 28 defines the maximum opening of the suction valve 151 .

A refrigerant gas in the suction chamber 131 is sucked through the suction port 26 into the cylinder bore 111 , pushing the suction valve 151 , during the returning movement (movement from the right to the left in FIG. 5 ) of the piston 23 . The refrigerant gas in the cylinder bore 111 is discharged through the discharge port 27 into the discharge chamber 132 , pushing the discharge valve 161 during the forward movement (movement from the left to the right in FIG. 5 ) of the piston 23 . As the discharge valve 161 comes into contact with the retainer 171 on the retainer-forming plate 17 , its opening is restricted. The coolant discharged into the discharge chamber 132 is fed to a condenser 30 , an expansion valve 31 and an evaporator 32 on an external coolant circuit 29 outside the compressor and returned to the suction chamber 131 from the supply passage 25 .

A solenoid-operated capacity control valve 34 is arranged in a pressure feed passage 33 . (shown in FIG. 1A ) that connects the discharge chamber 132 to a control pressure chamber 121 . The pressure feed passage 33 supplies the refrigerant gas in the discharge chamber 132 to the control pressure chamber 121 . The solenoid-operated capacity control valve 34 is activated and inactivated by a controller (not shown), which controls activation and deactivation of the solenoid-operated capacity control valve 34 based on a detected compartment temperature detected by a compartment temperature sensor (not shown) detecting a compartment temperature of the car and a target compartment temperature set by a compartment temperature setter (not shown).

The refrigerant gas in the control pressure chamber 121 flows out to the suction chamber 131 through a pressure release passage 35 (shown in FIG. 1 A). When the solenoid-operated capacity control valve 34 is in the deactivated condition, the refrigerant gas in the discharge chamber 132 is not delivered to the control pressure chamber 121 . Therefore, the pressure difference between the control pressure in the control pressure chamber 121 and the suction pressure on opposite sides of the piston 23 becomes smaller, and the inclination angle of the swash plate 20 shifts towards the maximum angle side. When the solenoid-operated capacity control valve 34 is in the activated condition, the refrigerant gas in the discharge chamber 132 is delivered to the control pressure chamber 121 through the pressure feed passage 33 . Therefore, the pressure difference between the control pressure in the control pressure chamber 121 and the suction pressure on the opposite sides of the piston 23 becomes greater and the inclination angle of the swash plate 20 shifts to the minimum angle side.

As shown in FIG. 4 , the suction port 26 is formed in a shape similar to a sector with an apex portion of the sector removed. A contour line of the suction port 26 positioned on the contact surface 141 of the partition plate 14 includes a proximal end line 36 positioned on the side of the proximal end of the suction valve 151 (on the side of the window 152 ), a distal end line 37 positioned on the side of the distal end of the suction valve 151 , a pair of right and left side lines 39 and 38 , a first connection line 401 that interconnects the proximal end line 36 and the side line 38 , another first connection line 402 that interconnects the proximal end line 36 and the side line 39 , a second connection line 411 that interconnects the distal end line 37 and the side line 38 , and another second connection line 412 that interconnects the distal end line 37 and the side line 39 . The suction valve 151 has a symmetric shape with respect to a reference line X extending in the longitudinal direction of the suction valve 151 , and the suction port 26 has a symmetric shape with respect to the reference line X. In other words, the left and right halves of the suction port 26 are symmetrical.

The proximal end line 36 is a convex curve slightly protruding from the distal end side of the suction valve 151 toward the proximal end side of the suction valve 151 . The distal end line 37 is a convex curve protruding from the proximal end side of the suction valve 151 toward the distal end side of the suction valve. The side lines 38 and 39 are approximately straight lines extending substantially along the radial line of the circle C (shown in FIG. 3 ) associated with the circumferential surface of the cylinder bore 111 . The first connection line 401 is a curve smoothly connected to the proximal end line 36 and the side line 38 at positions L 1 and L 2 , and another first connection line 402 is a curve smoothly connected to the proximal end line 36 and the side line 39 at positions. R 1 and R 2 . The second connection line 411 is a curve smoothly connected to the distal end line 37 and the side line 38 at positions L 3 and L 4 , and another second connection line 412 is a curve smoothly connected to the distal end line 37 and the side line 39 at positions R 3 and R 4 .

The bending angle θ 2 of the second connection lines 411 and 412 is greater than the bending angle θ 1 of the first connection lines 401 and 402 . The bending angle θ 1 represents an angle formed by normal lines m 1 and m 2 at the positions L 1 and L 2 and an angle formed by normal lines n 1 and n 2 at the positions R 1 and R 2 . The bending angle θ 2 represents an angle formed by normal lines m 3 and m 4 at positions L 3 and L 4 and an angle formed by normal lines n 3 and n 4 at positions R 3 and R 4 .

In this embodiment, each of the proximal end line 36 , the distal end line 37 , the first connection lines 401 and 402 and the second connection lines 411 and 412 comprises a circular arc. The radius of curvature of the proximal end line 36 is greater than that of the distal end line 37 . The radius of curvature of the distal end line 37 is slightly smaller than the radius of the circle C.

The refrigerant gas passing through the suction port 26 from the side of the suction chamber 131 towards the side of the cylinder bore 111 flows between the contact surface 141 of the partition plate 14 and the suction valve 151 in the direction of the normal lines to the outer contour line of the suction port 26 or the contact surface 141 (the normal lines being represented by arrows N 1 , N 2 , N 3 and N 4 in FIG. 3 ).

The first embodiment provides the following effects.

(1-1) The area S encompassed by the proximal end line 36 , the distal end line 37 , the side lines 38 and 39 and the connection lines 401 , 402 , 411 and 412 is the flow sectional area of the suction port 26 . When the suction port 26 is viewed in the reciprocating direction of the piston 23 , a middle line T shown in FIG. 4 passes through the middle point Ho of the maximum length (represented by H in FIG. 4 ) of the suction port 26 in the longitudinal direction of the suction valve 151 (that is, in the direction of the reference line X), extends transversely with respect to the suction port 26 , and perpendicularly crosses the reference line X extending in the longitudinal direction of the suction valve 151 . When the suction port 26 is viewed in the reciprocating direction of the piston 23 , the middle line T assumed in this way divides the suction port 26 into first and second sections 261 and 262 . The area S 2 of the second section 262 positioned on the distal end side of the suction valve 151 is greater than the area S 1 of the first section 261 . The greater the area S 2 of the second section 262 is than the area S 1 of the first section 261 , the greater is the length of the contour line of the suction port 26 on the distal end side of the suction valve 151 . In other words, the move the center of gravity of the area of the suction port 26 is shifted towards the distal end side of the suction valve 151 , the greater is the length of the contour line of the suction port 26 on the distal end side of the suction valve 151 .

The opening gap δ of the suction valve 151 relative to the partition plate 14 becomes greater towards the distal end of the suction valve 151 , as shown in FIG. 2 . Therefore, the greater the ratio of a portion of the refrigerant gas passing through the suction port 26 on the distal end side of the suction valve 151 is relative to a portion of the refrigerant gas passing through the suction port 26 on the proximal end side thereof, the higher is the degree of improvement in the easy inflow of the refrigerant gas into the cylinder bore 111 from the suction chamber 131 . The longer the length of the contour line of the suction port 26 on the distal end side of the suction valve 151 is, the greater is the proportion of the flow of the refrigerant gas passing through the suction port 26 on the distal end side thereof relative to that on the proximal end side of the suction valve 151 . Therefore, the construction in which the area S 2 of the second-section 262 , is greater than the area S 1 of the first section 261 enables the gas to more easily flow through the suction port 26 between the suction valve 151 on the distal end side of the suction valve 151 and the contact surface 141 . As a result, the ease of inflow of the refrigerant gas when the refrigerant gas is sucked from the suction port 26 into the cylinder bore 111 can be improved, and the performance of the compressor can also be improved.

(1-2) The width of the suction port 26 (represented by W in FIG. 4 ) measured in the direction of the middle line T becomes gradually greater in the longitudinal direction of the suction valve 151 (in the direction of the reference line X) from the proximal end side to the distal end side of the suction valve 151 , within the range D shown in FIG. 4 . The region Do of the suction port 26 (hatched with chain hatching lines in FIG. 4 ) within the range D is a width increasing region where the width W becomes gradually greater in the direction of the reference line X from the proximal end side to the distal end side of the suction valve 151 . The length d of the width increasing region Do in the direction of the reference line occupies a major part of the maximum length H of the suction port 26 in the direction of the reference line X. The existence of such a width increasing region Do is convenient for making the area S 2 of the second section 262 greater than the area S 1 of the first section 261 , and the length of the contour line of the suction port 26 can be easily elongated as the width increasing region Do is disposed. Therefore, the existence of the width increasing region Do allows the refrigerant gas passing through the suction port 26 to more easily flow between the suction valve 151 and the contact surface 141 on the distal end side of the suction valve 151 .

(1-3) The maximum width of the suction port 26 (represented by Wo in FIG. 4 ) in the direction of the middle line T exists in the second section 262 . The maximum width Wo is greater than the maximum length H of the suction port 26 in the direction of the reference line X. The construction in which the maximum length H of the suction port 26 in the direction of the reference line X is smaller than the maximum width Wo of the suction port 26 in the direction of the middle line T is more advantageous for elongating the contour line of the suction port 26 on the distal end side of the suction valve 151 than the case where H>Wo. The closer the position of the maximum width Wo of the suction port 26 is to the distal end of the suction valve 151 , the more it elongates the contour line of the suction port 26 on the distal end side of the suction valve 151 . In other words, the construction in which the maximum length H of the suction port 26 in the direction of the reference line X is smaller than the maximum width Wo of the suction port 26 in the direction of the middle line T and the maximum width Wo exists in the second section 262 is convenient for elongating the length of the contour line of the suction port 26 on the distal end side of the suction valve 151 .

(1-4) The distal end line 37 is longer than the proximal end line 36 . The construction in which the distal end line 37 is longer than the proximal end line 36 enables the refrigerant gas passing through the suction port 26 to more easily flow towards the distal end side of the suction valve 151 .

(1-5) The closer the distal end line 37 is to the circle C of the circumferential surface of the cylinder bore 111 , the greater is the opened gap δ (shown in FIG. 2 ) between the distal end line 37 and the suction valve 151 under the valve open condition. The greater the gap δ is between the distal end line 37 and the suction valve 151 , the easier it becomes for the refrigerant gas to flow into the cylinder bore 111 . The distal end line 37 is an arc protruding outward from the proximal end side to the distal end side of the suction valve 151 . The radius of curvature of the distal end line 37 is slightly smaller than the radius of the circle C of the circumferential surface of the cylinder bore 111 . The construction in which the distal end line 37 is the convex curve approximate to the circle C of the circumferential surface of the cylinder bore 111 is advantageous for bringing the distal end line 37 closer to the circle C of the circumferential surface of the cylinder bore 111 .

(1-6) The pressure in the cylinder bore 111 urges the suction valve 151 against the periphery wall of the suction port 26 , in the condition where the refrigerant gas in the cylinder bore 111 is discharged to the discharge chamber 132 , and the suction valve 151 closes the suction port 26 . If the urging force by the gas per unit length of the contour line of the suction port 26 is sufficient, the refrigerant gas will not leak from the cylinder bore 111 to the suction port 26 through the gap between the contact surface 141 and the suction valve 151 . However, if a corner exists at a part of the contour line of the suction port 26 , the urging force of the gas per unit length of the contour line at the proximity of this corner becomes small. Therefore, the construction in which the corner exists at a part of the contour line of the suction port 26 is likely to invite a backflow of the refrigerant gas from the cylinder bore 111 to the suction port 26 . The backflow of the refrigerant gas invites a drop in volumetric efficiency. The contour line of the suction port 26 comprising the proximal end line 36 , the distal end line 37 , the side lines 38 and 39 , the first connection lines 401 and 402 and the second connection lines 411 and 412 becomes an annular line without any corner. The construction in which the contour line of the suction port 26 is an annular line without any corner is advantageous for preventing the refrigerant gas from back-flowing from the cylinder bore 111 to the suction port 26 .

(1-7) The bending angle θ 2 of the second connection lines 411 and 412 is greater than the bending angle θ 1 of the first connection lines 401 and 402 . Unless the shapes of the proximal end line 36 , the distal end line 37 and the side lines 38 and 39 change greatly, the length of the distal end line 37 becomes greater as the bending angle θ 2 becomes greater than the bending angle θ 1 to the greater extent. The construction in which the bending angle θ 2 of the second connection lines 411 and 412 is greater than the bending angle θ 1 of the first connection lines 401 and 402 is convenient as a construction for increasing the length of the distal end line 37 .

(1-8) The closer the contour line of the suction port 26 on the distal end side of the suction valve 151 is to the circumferential surface of the cylinder bore 111 , the easier it becomes for the refrigerant gas to flow into the cylinder bore 111 . Normally, the shapes of the suction valve 151 and the suction port 26 are set to symmetric shapes with respect to the reference line X, respectively. Then, the contour line of the suction port 26 on the distal end side of the suction valve 151 becomes symmetric with respect to the reference line X. When the distal end line 37 , which is symmetric with the reference line X, is brought closer to the circumferential surface of the cylinder bore 111 along the reference line X, the distal end line 37 can be brought most closely to the circumferential surface of the cylinder bore 111 when the reference line X is in conformity with the radial line of the circle C of the circumferential surface of the cylinder bore 111 . Therefore, the construction in which the reference line X is allowed to extend substantially along the radial line of the circle C of the circumferential surface of the cylinder bore 111 is advantageous for bringing the distal end line 37 closer to the circle C of the circumferential surface of the cylinder bore 111 .

(1-9) In the piston compressor, self-induced vibration may possibly occur during the shift of the suction valve from the position in which it closes the suction port to the maximum opening position, and this self-induced vibration invites suction pulsation. Suction pulsation causes the evaporator 32 in the external coolant circuit 29 to vibrate and to generate noise. In the variable capacity type compressor having the pistons 23 , the pistons 23 reciprocate with strokes corresponding to the angle of inclination of the tiltable swash plate 20 so that the capacity becomes small when the angle of inclination of the swash plate 20 becomes small. The average gas flow rate through the suction ports is small under the low capacity condition, and the suction valves may not abut against the bottoms of the maximum opening limiting recesses 28 . In consequence, self-induced vibration of the suction valve is likely to occur in the variable capacity type compressor.

In the construction in which the area S 2 of the second section 262 is greater than the area S 1 of the first section 261 , the flow of the refrigerant gas. flowing from the suction chamber 131 into the cylinder bore 111 is likely to more greatly concentrate on the distal end side remote from the proximal end of the suction valve 151 , compared with the case of a suction port such as the one described in Japanese Unexamined Patent Publication (Kokai) No. 2000-54961, for example. Therefore, the suction valve 151 may abut against the bottom of the maximum opening limiting recess 28 even under the low capacity condition, and self-induced vibration of the suction valve 151 will be less likely to occur.

Next, the second embodiment of the present invention will be explained with reference to FIGS. 6A and 6B , in which like reference numerals are used to identify elements similar to those in the first embodiment.

The contour line of the suction port 26 A comprises the proximal end line 36 , the distal end line 37 , the curved side lines 38 A and 39 A, the first connection lines 401 A and 402 A, and the second connection lines 411 A and 412 A. The radius of curvature of each of the first and second connection lines 401 A, 402 A, 411 A, and 412 A is greater than the radius of curvature of the first connection lines 401 and 402 in the first embodiment. The contour line of such a suction port 26 A is an annular line having no corner and no straight line. The construction in which the contour line of the suction port 26 A is an annular line having no corner and no straight line provides the same effect as that of the first embodiment. The construction in which the radius of curvature of the connection lines 401 A, 402 A, 411 A and 412 A is greater than the radius of curvature of the connection lines 401 and 402 in the first embodiment is much more advantageous than the first embodiment for preventing the refrigerant gas from back-flowing from the cylinder bore 111 to the suction port 26 A.

FIG. 7 shows the third embodiment and FIG. 8 shows the fourth embodiment. FIG. 9 shows the fifth embodiment and FIG. 10 shows the sixth embodiment. FIG. 11 shows the seventh embodiment and FIG. 12 shows the eighth embodiment. Like reference numerals are used in these drawings to identify similar elements in the first and second embodiments.

The proximal end line 36 B of the suction port 26 B shown in FIG. 7 is a concave curve recessed from the proximal end side to the distal end side of the suction valve 151 .

The distal end line 37 C of the suction port 26 C shown in FIG. 8 is a part of an ellipse. The distal end line 37 C and a pair of side lines 38 A and 39 A are smoothly connected at positions L 5 and R 5 .

The proximal end line 36 D of the suction port 26 D shown in FIG. 9 is a part of a circle and the distal end line 37 D is a part of an ellipse. The proximal end line 36 D and the distal end line 37 D are connected smoothly at positions L 6 and R 6 .

The suction port 26 E shown in FIG. 10 represents the shape formed by inverting the suction port described in Japanese Unexamined Patent Publication (Kokai) No. 2000-54961 in the direction of the reference line X. The proximal end line 36 E of the suction port 26 E is smoothly connected to a pair of connection lines 411 A and 412 A.

The distal end line 37 F of the suction port 26 F in FIG. 11 comprises a first distal end line 371 , a second distal end line 372 and a connection line 373 . The connection line 373 is smoothly connected to the first distal end line 371 and the second distal end line 372 at positions L 7 and R 7 .

The distal end line 37 G of the suction port 26 G shown in FIG. 12 is a part of a circle, and the proximal end line 36 G is a part of an ellipse. The distal end line 37 G and the proximal end line 36 G are smoothly connected at positions L 8 and R 8 .

The contour lines of the suction ports 26 B to 26 F in the embodiments shown in FIGS. 7 to 11 provide the same condition as the suction port 26 of the first embodiment as to the size of the first and second areas S 1 and S 2 of the first and second sections 261 and 262 , the length relationship of the maximum length H and the width Wo and the relationship of the length d of the width increasing region Do and the maximum length H.

Incidentally, the present invention can also be applied to suction ports having an asymmetric shape with respect to the reference line. Also, the present invention can be applied to the discharge port.

As described above in detail, the present invention provides the excellent effect in which facility of the flow of the gas through the fluid port (lack of resistance to inflow of the gas) can be improved.

Claims

1. A piston type compressor comprising:a housing having cylinder bores, and fluid ports in communication with the cylinder bores; pistons reciprocatingly arranged in said cylinder bores; a drive shaft rotatably supported by said housing; a transmission mechanism operatively coupled to said drive shaft and said pistons for converting rotation of said drive shaft into reciprocal movement of the pistons; valves to open and close the fluid ports, each said valve having a longitudinal direction, a proximal end and a distal end on the opposite side of the proximal end; and wherein a middle line is provided which passes through a middle point of a maximum length of each said fluid port in the longitudinal direction of each said valve, extends transversely with respect to said fluid port and perpendicularly crosses a reference line extending in the longitudinal direction of said valve, said middle line dividing said fluid port into a first section positioned on the side of the proximal end of said valve and a second section positioned on the side of said distal end of said valve, an area of said second section being greater than an area of said first section.

2. A piston type compressor according to claim 1, wherein a width increasing region is disposed in which the width of said fluid port in a direction of said middle line becomes gradually greater from the proximal end side to the distal end side of said valve in the longitudinal direction of said valve, and the length of said width increasing region in the direction of said reference line occupies a major part of the maximum length of said fluid port in the direction of said reference line.

3. A piston type compressor according to claim 2, wherein a maximum width of said fluid port in the direction of said middle line exists in said second section and is greater than a maximum length of said fluid port in the direction of said reference line.

4. A piston type compressor according to claim 1, wherein said fluid port has a contour line comprising a proximal end line positioned on the side of the proximal end of said valve, a distal end line positioned on the side of the distal end of said valve, and a pair of right and left side lines, and said distal end line is longer than said proximal end line.

5. A piston type compressor according to claim 4, wherein said distal end line comprises a convex curve protruding from the proximal end side toward the distal end side of said valve.

6. A piston type compressor according to claim 4, wherein said contour line of said fluid port includes a pair of first connection lines connecting said proximal end line to said pair of side lines, and a pair of second connection lines connecting said distal end line to said pair of side lines, said pair of first connection lines being smoothly connected to said proximal end line and said pair of said side lines, said pair of second connection lines being smoothly connected to said distal end line and said pair of side lines.

7. A piston type compressor according to claim 4, wherein said contour line of said fluid port is an annular convex curve with no corner.

8. A piston type compressor according to claim 1, wherein said reference line extends substantially along a radial line of a circle of a circumferential surface of said cylinder bore.

9. A piston type compressor according to claim 1, wherein the fluid port is formed in the shape of a portion of a sector with an apex portion of a sector removed.

10. A piston type compressor according to claim 1, further comprising a suction chamber, a discharge chamber, suction ports, discharge ports, suction valves, and discharge valves, wherein said fluid port comprises at least one of the suction port and the discharge port, and said valve comprises corresponding one of the suction valve and the discharge valve.