JP2010059889A - Booster compressor - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a booster compressor increased in weight and suppressed in the size of the machine body. <P>SOLUTION: The booster compressor includes a crank chamber 223 which is used to boost a compressed fluid from an external compressed fluid supply source and discharge the compressed fluid to the outside and defined in such a manner as to be isolated from the outside by a piston 222, a cylinder 14, and a crankcase 13, a crank chamber introduction passage for introducing the compressed fluid from the compressed fluid supply source to the crank chamber 223, and a relief valve 228 for releasing a pressure in the crank chamber 223 to the outside when the pressure in the crank chamber rises to a predetermined value or higher. <P>COPYRIGHT: (C)2010,JPO&INPIT

Description

  The present invention relates to a booster compressor.

There is a compressor that repeatedly expands and contracts the compression chamber defined by the cylinder and the piston and cylinder head by reciprocating the piston in the cylinder, and sucks, compresses and discharges the fluid. There is a so-called booster compressor that pressurizes compressed fluid from an external compressed fluid supply source and discharges the compressed fluid to the outside. In such a booster compressor, there is a technique in which a compressed fluid from an external compressed fluid supply source is introduced into a crank chamber defined by a crankcase, a piston, and a cylinder, and pressure is applied to the crank chamber side of the piston. (For example, refer to Patent Document 1).
Japanese Utility Model Publication No. 56-4690

  In the booster compressor that introduces the compressed fluid into the crank chamber as described above, the pressure resistance of the crank chamber needs to be improved, so that the weight tends to increase and the size of the machine body tends to increase.

  Therefore, an object of the present invention is to provide a booster compressor capable of suppressing an increase in weight and an increase in size of the airframe.

  In order to achieve the above object, the booster compressor of the present invention is provided with a relief valve for releasing the internal pressure to the outside when the internal pressure of the crank chamber rises to a predetermined value or more.

  According to the present invention, an increase in weight and an increase in body size can be suppressed.

  Embodiments according to the present invention will be described below with reference to the drawings.

“First Embodiment”
The booster compressor which is 1st Embodiment which concerns on this invention is demonstrated based on FIG. 1 and FIG.

  FIG. 1 is a side sectional view showing a booster compressor according to a first embodiment of the present invention. FIG. 2 is a front sectional view showing the booster compressor according to the first embodiment of the present invention.

  The booster compressor 11 according to the first embodiment shown in FIGS. 1 and 2 is supplied with compressed gas (fluid) that has been pressurized in advance from a compressed fluid supply source (not shown) outside the machine body, and compresses the introduced compressed gas. It is recompressed in the room, further boosted and discharged outside the aircraft. The booster compressor 11 is coupled to the crankshaft 12, a crankcase 13 that accommodates the crankshaft 12 and rotatably supports the crankshaft 12, and a posture along a direction perpendicular to the crankshaft 12. The cylinder 14 has a cylinder head 15 mounted on the opposite side of the cylinder 14 from the crankcase 13. Further, as shown in FIG. 1, the booster compressor 11 is mounted on one horizontal side of the crankcase 13 and is opposite to the electric motor portion 18 that drives the crankshaft 12 and the crankcase 13 of the motor portion 18. An end cover 19 attached to the side, a case cover 20 detachably attached to the horizontal opposite side of the crankcase 13, and a crankshaft 12 that is connected to the crankshaft 12 while swinging in the cylinder 14 by eccentric rotation of the crankshaft 12 And a swinging member 21 that reciprocates. The swing member 21 defines a compression chamber 22 with the cylinder head 15 and the cylinder 14.

  The crankcase 13 is integrally formed into a substantially bottomed cylindrical shape having a substantially cylindrical case body 25 parallel to the crankshaft 12 and a case bottom 26 formed on one side of the case body 25 in the axial direction. Yes.

  The crankcase 13 is installed with the axis of the case body 25 arranged in the horizontal direction, and an installation leg 27 is formed at the lower part of the case body 25, A mounting base 28 for mounting the cylinder 14 is formed on the upper portion of the case body 25. A circular cylinder mounting hole 29 is formed in the center of the mounting base 28 so as to penetrate the crankshaft 12 in the vertical direction and to which the cylinder 14 is mounted. An annular seal groove 31 is formed around the cylinder mounting hole 29 of the mounting base 28 so as to be coaxial with the cylinder mounting hole 29 and recessed in the axial direction. A seal ring 32 made of an elastic material such as rubber is disposed.

  A circular motor fitting portion 35 that fits the motor portion 18 is formed on the outer peripheral side of the case bottom portion 26 on one side in the axial direction of the crankshaft 12 in the crankcase 13. Further, a step-shaped bearing holding portion 38 is formed at the center of the case bottom portion 26 of the crankcase 13, and a through hole 39 penetrating the case bottom portion 26 in the axial direction is formed around the bearing holding portion 38. It is intermittently formed in the circumferential direction. An annular seal groove 40 is formed on the outer peripheral surface of the motor fitting portion 35 so as to be recessed inward in the radial direction. The seal groove 41 is made of an elastic material such as an annular rubber. Is arranged.

  The crankcase 13 is formed with a circular opening hole 45 of the case body 25 on the other side in the axial direction of the crankshaft 12. An annular sealing groove 46 that is coaxial with the opening hole 45 and is recessed in the axial direction is formed at an intermediate position in the radial direction of the end surface of the case body 25 on the opening hole 45 side. A seal ring 47 made of an elastic material such as an annular rubber is disposed.

  In the crankcase 13 described above, the opening hole 45, the motor fitting portion 35, and the cylinder mounting hole 29 are formed independently of each other.

  The cylinder 14 has a substantially cylindrical shape that is attached to the outside of the mounting base portion 28 of the crankcase 13 so as to be perpendicular (specifically vertical) to the axis of the case body 25. In the mounted state, the lower surface of the cylinder 14 comes into contact with the seal ring 32 in the seal groove 31, thereby sealing the gap between the crankcase 13 and the cylinder 14.

  The cylinder head 15 is mounted on the cylinder 14. The cylinder head 15 includes a partition plate 66 disposed on the cylinder 14 and a cylinder head body 68 disposed on the partition plate 66.

  The partition plate 66 is formed with a plurality of suction holes 72 and discharge holes 73 penetrating in the plate thickness direction. A plate-like suction valve 74 capable of opening and closing the suction hole 72 is attached to the partition plate 66 on the cylinder 14 side, and a plate-like discharge valve 75 capable of opening and closing the discharge hole 73 on the cylinder head main body 68 side. Is attached.

  The cylinder head body 68 is formed with two chambers, a suction chamber 81 and a discharge chamber 82. The cylinder head main body 68 is formed with a suction port 83 that communicates the suction chamber 81 with the outside and a discharge port 84 that communicates the discharge chamber 82 with the partition plate 66. In the cylinder head body 68, the suction chamber 81 always communicates with the suction hole 72 of the partition plate 66, and the discharge chamber 82 accommodates the discharge valve 75 and can communicate with the discharge hole 73 of the partition plate 66 via the discharge valve 75. It arrange | positions on the partition plate 66 so that it may become.

  The motor unit 18 is fixed to the cylindrical motor body 100 connected to the crankcase 13 by fitting the motor fitting part 35 of the crankcase 13 to one end side, and fixed to the inner peripheral surface of the motor body 100. And a support plate 102 attached so as to close the other end of the motor body 100. The seal ring 41 in the seal groove 40 formed in the motor fitting portion 35 of the crankcase 13 contacts the inner peripheral surface of the motor barrel portion 100 when the motor fitting portion 35 is fitted to the motor barrel portion 100. Thus, the gap between the motor body 100 and the motor fitting portion 35 of the crankcase 13 is sealed.

  The support plate 102 is formed with a leg portion 105 for installation at the lower portion, and a boss portion 106 projecting toward the motor body 100 side is formed at an intermediate portion thereof. A circular fitting portion 107 that is coaxial with the boss portion 106 and protrudes toward the motor body portion 100 is formed. A step-shaped bearing holding portion 110 is formed inside the boss portion 106. The booster compressor 11 is installed on an installation surface such as a floor surface by the legs 105 of the support plate 102 and the legs 27 of the crankcase 13.

  The fitting portion 107 is fitted to the motor body 100, and an annular seal groove 115 is formed on the outer peripheral surface thereof so as to be recessed inward in the radial direction. A seal ring 116 made of an elastic material such as an annular rubber is disposed in the seal groove 115, and the seal ring 116 seals a gap between the fitting portion 107 of the support plate 102 and the motor body 100. An annular seal groove 117 is formed on the opposite side of the support plate 102 from the motor body 100 so as to surround a through portion inside the boss portion 106. The seal groove 117 is made of an elastic material such as rubber. A seal ring 118 made of material is arranged.

  The motor unit 18 includes a large-diameter bearing 123 held by the bearing holding unit 38 of the crankcase 13, a small-diameter bearing 124 held by the bearing holding unit 110 of the support plate 102, and both ends of these bearings 123 and 124. It has a drive shaft 125 that is rotatably held, and a rotor 126 that is fixed to the drive shaft 125 and disposed inside the stator 101. When the rotor 126 is rotated by the magnetic force generated by the stator 101, the drive shaft 125 rotates integrally with the rotor 126.

  On the drive shaft 125, a balance weight 135 is attached to a protrusion 130 that protrudes outward from the bearing 123. A key 137 for fixing the balance weight 135 in the rotational direction with respect to the drive shaft 125 is fixed to the protrusion 130 of the drive shaft 125. Here, a screw hole 138 is formed in the balance weight 135 along the radial direction, and the balance weight 135 is fixed to the drive shaft 125 by the bolt 139 being screwed into the screw hole 138 and contacting the key 137. Is done.

  The end cover 19 has a cover main body 142 attached to the opposite side of the support plate 102 from the motor body 100. The cover main body 142 is formed with a recess 143 that is slightly smaller than the seal groove 117 at an intermediate portion that is inside the seal groove 117 of the support plate 102 when attached to the support plate 102. A substrate 148 is attached to the. Here, the seal ring 118 disposed in the seal groove 117 of the support plate 102 comes into contact with the outside of the recess 143 of the cover main body 142, and seals the gap between the support plate 102 and the cover main body 142. The cover main body 142 is fixed to the support plate 102 by a plurality of bolts 163 on the outer side of the seal portion by the seal ring 118.

  The case cover 20 closes the opening hole 45 for mounting components, and has a flat disk shape that abuts the end face of the crankcase 13 on the opening hole 45 side at the outer peripheral portion. The seal ring 47 of the seal groove 46 formed around the opening hole 45 of the crankcase 13 contacts the case cover 20 and seals the gap between the crankcase 13 and the case cover 20. The case cover 20 is fixed to the crankcase 13 by a plurality of bolts 173 on the outer side of the seal portion by the seal ring 47.

  The crankshaft 12 is formed by fitting the projecting portion 130 of the drive shaft 125 into the drive shaft 125 of the motor unit 18 and the eccentric hole 175 formed eccentrically with respect to the outer diameter center that is the center with respect to the outer diameter. A substantially disc-shaped crank member 176 that is attached to the shaft 125 in an eccentric state, and the key 137 that integrates the crank member 176 with respect to the drive shaft 125 in the rotational direction. Thus, the motor unit 18 is a direct drive type that directly drives the crankshaft 12 without a belt or the like. Here, the crank member 176 is fixed to the balance weight 135 with a bolt 180. Since the balance weight 135 is fixed to the drive shaft 125 with the bolts 139 as described above, the crank member 176 is fixed to the drive shaft 125 by fixing to the balance weight 135.

  The swing member 21 includes a bearing 185 for fitting the crank member 176 of the crankshaft 12 inside, a connecting rod 186 whose one end is rotatably connected to the crank member 176 via the bearing 185, and the connecting rod 186. A spacer 187 detachably provided at the other end of the piston, a piston head 188 detachably provided on the spacer 187, and a gap between the piston head 188 and the bore 58 of the cylinder 14 disposed on the outer peripheral side of the piston head 188. And a lip seal 189 for sealing.

  The connecting rod 186 is formed on one end side and has an annular large end 195 into which the bearing 185 described above is fitted. The connecting rod 186 has a relatively elongated shape and extends radially outward from the large end 195. The extending portion 196 is formed integrally with the extending portion 196 at the tip of the extending portion 196 and has a disk-shaped small end portion 197 formed so as to coincide with the central axis of the extending portion 196.

  As shown in FIG. 2, the spacer 187 is formed with a lower fitting recess 204 that is recessed in a circular shape within a predetermined central range in the radial direction on one side in the axial direction, and the connecting rod is connected to the lower fitting recess 204. The above-mentioned small end portion 197 of 186 is fitted. In addition, the spacer 187 is formed with an upper fitting recess 206 that is recessed in a circular shape in a predetermined range in the radial direction on the other side in the axial direction. As a result, a portion outside the bottom surface of the upper fitting recess 206 is formed. Is an annular base portion 209 that forms an annular shape and protrudes outward in the axial direction. Further, a central concave portion 207 that is further recessed in a circular shape is formed in a predetermined central range in the radial direction of the upper fitting concave portion 206.

  The piston head 188 has a disk shape having the same diameter as the outer diameter of the spacer 187, and a fitting projection that protrudes in the axial direction by forming a coaxial annular shape in a predetermined central range in the radial direction on one side of the axial direction. A portion 212 is formed. As a result, the piston head 188 has a flange portion 213 having a larger diameter than the fitting convex portion 212 on the other side in the axial direction. The piston head 188 is fitted into the upper fitting concave portion 206 of the spacer 187 at the fitting convex portion 212.

  The lip seal 189 is sandwiched between the flange portion 213 of the piston head 188 and the annular base portion 209 of the spacer 187 in a state where the fitting convex portion 212 of the piston head 188 is fitted in the upper fitting concave portion 206 of the spacer 187. . The lip seal 189 is an annular seal ring made of an elastic material such as PTFE (tetrafluoroethylene resin), and the inner peripheral side engages the fitting convex portion 212 of the piston head 188 on the inside and the annular shape of the spacer 187. A flat plate-shaped annular clamping part 218 is sandwiched between the base part 209 and the flange part 213 of the piston head 188. The outer peripheral side protrudes outward from the clamping part 218 and bends toward the piston head 188 in the thickness direction. Thus, an annular lip portion 219 that covers the outer peripheral side of the flange portion 213 of the piston head 188 is formed. The lip seal 189 is in sliding contact with the bore 58 of the cylinder 14 at the lip portion 219.

  Here, the spacer 187 is fitted to the small end portion 197 of the connecting rod 186, the lip seal 189 is disposed on the spacer 187, and the piston head 188 is attached to the spacer 187 so as to sandwich the lip seal 189. In this state, the piston head 188, the lip seal 189, the spacer 187, and the connecting rod 186 are integrally connected by the plurality of screws 220 to form the swing member 21.

  In the oscillating member 21, the piston head 188, the spacer 187, and the lip seal 189 sandwiched between the piston head 188 and the lip seal 189 serve as a piston portion (piston) 222 disposed inside the cylinder 14, and at this time, the lip seal 189 is an annular lip. The portion 219 is slidably contacted with the bore 58 of the cylinder 14 with a tightening margin, thereby basically sealing the space between the cylinder 14 and the piston portion 222. A portion surrounded by the piston portion 222, the cylinder 14, and the partition plate 66 of the cylinder head 15 is the compression chamber 22 described above.

  In addition, a crank chamber 223 is defined by the piston portion 222, the cylinder 14, and the crankcase 13 so as to be isolated from the outside of the machine body.

  Here, as shown in FIG. 1, a cylinder mounting hole 29 in which the cylinder 14 is mounted, a motor fitting section 35 in which the motor section 18 is mounted, and an opening hole 45 for mounting parts are independent of each other. Therefore, the connecting portion between the crankcase 13 and the cylinder 14 can be sealed by the seal ring 32 provided around the cylinder mounting hole 29, and provided around the motor fitting portion 35. The connecting portion between the crankcase 13 and the motor unit 18 can be sealed by the seal ring 41, and the connecting portion between the crankcase 13 and the case cover 20 can be sealed by the seal ring 47 provided around the opening hole 45. Can do. That is, it is possible to improve the sealing performance of the connecting portion with the other parts of the crankcase 13. In addition, the motor portion 18 constituting one of the other parts is also sealed at the connecting portion between the support plate 102 and the motor body 100 with the seal ring 116, and the connecting portion between the support plate 102 and the end cover 19 is at the seal ring 118. Since it is sealed, the crank chamber 223 has a sealed structure that basically prevents gas from leaking to the outside.

  An inlet pipe 225 is connected to the suction port 83 of the cylinder head main body 68 for introducing a gas such as air or nitrogen whose pressure has been previously increased from the atmospheric pressure from an external compressed fluid supply source. A branch pipe (crank chamber introduction path) 226 is branched from the midway position of the introduction pipe 225, and this branch pipe 226 is connected to the crank chamber 223 via the case cover 20. As a result, the booster compressor 11 is introduced with the compression gas, which has been previously pressurized from the external compressed fluid supply source, into the crank chamber 223 via the branch pipe 226. Therefore, the pressure of this gas is applied to the side opposite to the compression chamber 22 of the piston part 222, and the load applied to the connecting rod 186, the bearing 185, etc. Reduce.

  And in 1st Embodiment, as shown in FIG. 2, the protrusion base part 227 which protrudes to a side along the radial direction is formed in the case trunk | drum 25 of the crankcase 13, This protrusion base part A relief valve 228 is attached to the upper surface of 227. That is, a through screw hole 229 communicating with the crank chamber 223 is formed through the upper portion of the protruding base 227, and the relief valve 228 is screwed into the through screw hole 229 from the outside of the machine. . The relief valve 228 opens when the internal pressure in the crank chamber 223 rises above a predetermined value, and releases the pressure in the crank chamber 223 to the outside air. The internal pressure in the crank chamber 223 is less than a predetermined value. Keep in range.

  In the booster compressor 11 described above, the crank member 176 of the crankshaft 12 is eccentrically rotated by the rotation of the drive shaft 125 driven by the motor unit 18, and the swinging member 21 is eccentrically rotated by the crank member 176. The piston portion 222 including the piston head 188, the spacer 187, and the lip seal 189 is guided by the bore 58 of the cylinder 14 and reciprocates in the axial direction of the cylinder 14.

  In the suction stroke to the bottom dead center where the piston portion 222 is separated from the partition plate 66, the compression chamber 22 is expanded by the movement of the piston portion 222, the discharge hole 73 is closed by the discharge valve 75, and the suction hole is closed by the suction valve 74. The compressed gas from the compressed fluid supply source is introduced into the compression chamber 22 from the suction port 83 through the suction chamber 81 and the suction hole 72 with the 72 in an open state. Subsequently, in the compression stroke up to the top dead center where the piston portion 222 approaches the partition plate 66, the compression chamber 22 is reduced by the movement of the piston portion 222 in the direction of the partition plate 66, and the suction hole 72 is opened by the suction valve 74. The discharge hole 73 is opened by the discharge valve 75 and the compressor body is further compressed and discharged from the compression chamber 22 to the discharge port 84 via the discharge chamber 82.

  According to the booster compressor 11 of the first embodiment described above, the compressed gas from the external compressed fluid supply source is introduced into the crank 223 chamber to apply pressure to the crank chamber 223 side of the piston portion 222. However, the provision of the relief valve 228 prevents the pressure in the crank chamber 223 from rising above a predetermined value. Therefore, it is not necessary to increase the pressure resistance performance of the crank chamber 223 more than necessary, and as a result, an increase in weight and an increase in the size of the fuselage can be suppressed.

  Further, when the relief valve 228 is activated, an exhaust sound for exhausting the compressed gas to the outside is generated with a relatively loud sound, so that the exhaust sound can notify the surroundings that the relief valve 228 is activated. .

“Second Embodiment”
Next, a second embodiment will be described mainly based on FIG. FIG. 3 is a side sectional view showing a booster compressor according to the second embodiment. In addition, about the site | part which is common in 1st Embodiment, it represents with the same name and the same code | symbol.

  In the second embodiment, as shown in FIG. 3, a through screw hole 20 </ b> A that penetrates in the plate thickness direction and communicates with the crank chamber 223 is formed in the center of the disc-shaped case cover 20 that closes the opening hole 45. ing. The relief valve 228 is attached to the case cover 20 by being screwed into the through screw hole 20A from the outside.

  According to the booster compressor 11 of the second embodiment described above, the relief valve 228 is provided on the extension of the central axis of the case body 25 of the crankcase 13, so that it is more disturbing than the case where it is provided on the side. It is hard to become. Of course, the present invention is not limited to the extension of the central axis, but may be provided on the case cover 20 so as to be offset from the central axis.

“Third Embodiment”
Next, a third embodiment will be described mainly based on FIG. FIG. 4 is a side sectional view showing a booster compressor according to the third embodiment. In addition, about the site | part which is common in 1st Embodiment, it represents with the same name and the same code | symbol.

  In the third embodiment, as shown in FIG. 4, an annular contact portion 230 is formed on the outer peripheral portion of the case cover 20 that closes the opening hole 45 and contacts the end surface of the crankcase 13 on the opening hole 45 side. And a cylindrical part 231 extending from the inner end of the contact part 230 toward the crank chamber 223 along the axial direction, and a disk-like part closing the opposite side of the cylindrical part 231 from the contact part 230 232. The cylindrical portion 231 and the disc-shaped portion 232 constitute a concave portion 233 that is recessed in the axial direction from the inner end portion of the contact portion 230 to the crank chamber 223 side. In the case cover 20, a boss portion 234 having a thickness greater than that of the periphery is formed at the center of the disc-shaped portion 232 that is the bottom of the recess 233. In the center of the boss portion 234, A through screw hole 235 that penetrates and communicates with the crank chamber 223 is formed. The relief valve 228 is attached to the case cover 20 by being screwed into the through screw hole 235 from the outside. The boss portion 234 is shorter than the cylindrical portion 231. As a result, the part of the relief valve 228 that is exposed to the outside of the machine is housed in the recess 233, and the amount of protrusion from the outer end position of the machine body is small. It has been made smaller.

  According to the booster compressor 11 of the third embodiment described above, since the recess 233 recessed in the crank chamber 22 is formed in the case cover 20, the volume of the crank chamber 223 can be reduced, and the drain water Can be suppressed.

  In addition, the relief valve 228 is partially accommodated in the recess 233, and the amount of protrusion from the outer end position of the fuselage is reduced, so that the booster compressor 11 is reduced in size. In addition, it is possible to prevent breakage due to an impact from the outside of the relief valve 228.

“Fourth Embodiment”
Next, a fourth embodiment will be described mainly based on FIG. FIG. 5 is a side sectional view showing a booster compressor according to the fourth embodiment. In addition, about the site | part which is common in 1st Embodiment, it represents with the same name and the same code | symbol.

  In the fourth embodiment, as shown in FIG. 5, the case cover 20 that closes the opening hole 45 is formed on the outer peripheral portion and is in contact with the end face on the opening hole 45 side of the crankcase 13. And a concave portion 240 that has a substantially hemispherical curved surface from the inner end portion of the contact portion 239 and is recessed toward the crank chamber 223 side. In the case cover 20, a boss portion 241 having a thicker plate thickness than the periphery is formed at the center that is the lowest bottom portion of the recess 240, and the crank pierces through the center of the boss portion 241 in the plate thickness direction. A through screw hole 242 communicating with the chamber 223 is formed. The relief valve 228 is attached to the case cover 20 by being screwed into the through screw hole 242 from the outside. The boss portion 241 is shorter than the depth of the concave portion 240, and as a result, the relief valve 228 is partially accommodated in the concave portion 240, and the amount of protrusion from the outer end position of the fuselage is reduced. It has been made smaller.

  According to the booster compressor 11 of the fourth embodiment described above, since the recess 240 is formed in the case cover 20 so as to be recessed in the crank chamber 22, the volume of the crank chamber 22 can be reduced. Can be suppressed.

  In addition, the relief valve 228 is partially accommodated in the recess 240, and the amount of protrusion from the outer end position of the fuselage is reduced, thereby reducing the size of the booster compressor 11. In addition, it is possible to prevent breakage due to an impact from the outside of the relief valve 228.

  In addition, since the concave portion 240 has a curved surface, the pressure resistance of the case cover 20 is improved, and the case cover 20 can be reduced in thickness and weight.

It is a sectional side view showing the booster compressor of a 1st embodiment concerning the present invention. It is a front sectional view showing a booster compressor of a 1st embodiment concerning the present invention. It is a sectional side view which shows the booster compressor of 2nd Embodiment which concerns on this invention. It is a sectional side view which shows the booster compressor of 3rd Embodiment which concerns on this invention. It is a sectional side view which shows the booster compressor of 4th Embodiment which concerns on this invention.

Explanation of symbols

DESCRIPTION OF SYMBOLS 11 Booster compressor 12 Crankshaft 13 Crankcase 14 Cylinder 15 Cylinder head 20 Case cover 22 Compression chamber 222 Piston part (piston)
223 Crank chamber 226 Branch piping (crank chamber introduction path)
228 Relief valve 233 Concave part 240 Concave part

Claims (3)

A cylinder,
A cylinder head mounted on the cylinder;
A piston that reciprocates in the cylinder;
A compression chamber defined by these cylinders, cylinder heads and pistons;
A crankshaft connected to the piston;
A crankcase coupled to the cylinder and accommodating the crankshaft therein;
In the booster compressor that recompresses the compressed fluid from the external compressed fluid supply source in the compression chamber and further pressurizes and discharges the compressed fluid to the outside.
A crank chamber defined to be isolated from the outside by the piston, the cylinder, and the crankcase;
A crank chamber introduction path for introducing the compressed fluid from the compressed fluid supply source into the crank chamber;
A booster compressor comprising a relief valve for releasing the internal pressure to the outside when the internal pressure of the crank chamber rises to a predetermined value or more.   The crankcase is provided with a detachable case cover, the case cover is formed with a recess, and the relief valve is attached to the bottom of the recess. Booster compressor.   The booster compressor according to claim 2, wherein the concave portion is formed in a curved surface shape.

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