US20050188839A1 - Oilless reciprocating air compressor - Google Patents
Oilless reciprocating air compressor Download PDFInfo
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- US20050188839A1 US20050188839A1 US11/069,371 US6937105A US2005188839A1 US 20050188839 A1 US20050188839 A1 US 20050188839A1 US 6937105 A US6937105 A US 6937105A US 2005188839 A1 US2005188839 A1 US 2005188839A1
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- Prior art keywords
- piston
- air compressor
- cylinder
- reciprocating air
- piston ring
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/0005—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00 adaptations of pistons
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/04—Measures to avoid lubricant contaminating the pumped fluid
- F04B39/041—Measures to avoid lubricant contaminating the pumped fluid sealing for a reciprocating rod
- F04B39/042—Measures to avoid lubricant contaminating the pumped fluid sealing for a reciprocating rod sealing being provided on the piston
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
- F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
- F04B39/12—Casings; Cylinders; Cylinder heads; Fluid connections
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J1/00—Pistons; Trunk pistons; Plungers
- F16J1/01—Pistons; Trunk pistons; Plungers characterised by the use of particular materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J10/00—Engine or like cylinders; Features of hollow, e.g. cylindrical, bodies in general
- F16J10/02—Cylinders designed to receive moving pistons or plungers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J10/00—Engine or like cylinders; Features of hollow, e.g. cylindrical, bodies in general
- F16J10/02—Cylinders designed to receive moving pistons or plungers
- F16J10/04—Running faces; Liners
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/12—Details
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2201/00—Metals
- F05C2201/02—Light metals
- F05C2201/021—Aluminium
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/08—Ceramics; Oxides
- F05C2203/0865—Oxide ceramics
- F05C2203/0882—Carbon, e.g. graphite
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2225/00—Synthetic polymers, e.g. plastics; Rubber
- F05C2225/04—PTFE [PolyTetraFluorEthylene]
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2251/00—Material properties
- F05C2251/04—Thermal properties
- F05C2251/042—Expansivity
Definitions
- the present invention relates to an oilless reciprocating air compressor.
- a piston in an oilless reciprocating air compressor is made of resin and has an annular groove on the outer circumference.
- a piston ring made of resin is fitted in the annular groove, and the piston reciprocates in a cylinder.
- oilless reciprocating air compressor In the oilless reciprocating air compressor, it is not necessary for lubricating oil to be fed into a piston ring, a piston or a cylinder. Lubricating oil is not introduced into a compression chamber in the cylinder, and is not contained in compressed air discharged from the compressor. Thus, oilless reciprocating air compressors are widely used in medical, food or oxygen-feeding field that do not like oil in compressed air, or among users who are troubled in feed and maintenance of lubricating oil.
- the cylinder is made from Al or Al alloy flattening, casting or die casting material, and to increase hardness in the inner surface of the cylinder, hard alumite is applied to the inner surface that is in sliding contact with the piston.
- Anode oxidation coating having the maximum thickness of about thirty microns is formed and grounded to finish the cylinder.
- a resin piston is fitted in the cylinder, and reciprocated with a resin piston ring and a resin rider ring.
- the resin piston ring exhibits desired performance for a long time without replacement. Even if the resin piston ring should fail to be replaced, operation will be able to be continued without fouling because the piston provides self-lubricating capability though air amount discharged from the compressor decreases.
- FIG. 1 is a vertical sectional front view of a known oilless reciprocating air compressor
- FIG. 2 is a vertical sectional view taken along the line II-II in FIG. 1 ;
- FIG. 3 is an enlarged view of the circle “A” in FIG. 2 ;
- FIG. 4 shows one embodiment of the present invention and is similar to FIG. 3 ;
- FIG. 5 shows another embodiment of the present invention and is corresponding to an enlarged horizontal sectional view taken along the line V-V in FIG. 2 .
- FIG. 1 At the upper end of an Al or Al alloy cylinder 1 , a cylinder head 4 is mounted via a sucking valve plate 2 and a spacer 3 .
- the cylinder head 4 is separated into a suction chamber 6 and a discharge chamber 7 by a partition wall 5 .
- An inlet 8 is formed in the side wall of the suction chamber 6 and an outlet 9 is formed in the side wall of the discharging chamber 7 .
- a sucking bore 10 is formed through the bottom of the suction chamber 6 , and discharge bores 11 , 12 are formed through the spacer 3 and the sucking valve plate 2 to communicate with the discharge chamber 7 .
- a discharge valve plate 13 is mounted on the spacer 3 at the upper end of the discharge bore 11 and opens to communicate with the discharge chamber 7 .
- a hard alumite layer 14 is formed on the inner surface of the cylinder 1 , and an Al alloy piston 15 is slidably fitted in the cylinder 1 .
- a piston pin 16 which radially extends in the piston 15 is connected to a crankshaft 18 via a connecting rod 17 .
- An annular groove 19 is formed on the piston 15 and a resin piston ring 20 is fitted in the annular groove 19 to move slightly.
- crankshaft 18 is rotated to allow the piston 15 to reciprocate via the connecting rod 17 , so that air sucked through the inlet 8 and the sucking bore 10 is compressed and discharged through the discharge bore 12 , 11 and the outlet 9 .
- sealing capability of the resin piston ring 20 becomes poor to decrease discharge performance of the oilless reciprocating air compressor. Furthermore leakage is likely to generate abnormal sound. High temperature air on a compression chamber thermally gives adverse effects to a bearing of the piston, thereby decreasing the lives of the piston pin 16 , the end of the connecting rod 17 and the bearing.
- the piston ring In high-pressure and high-temperature operation, the piston ring is abnormally worn to decrease sealing capability and is then worn locally to breakage. To prevent abnormal sound during operation and prevent the life of the bearing from reducing owing to heat by leaked high-temperature compressed air, the piston ring has to be replaced at an earlier stage.
- one or more labyrinth grooves are formed on the upper and lower surfaces of the annular groove, and small pieces of worn piston ring are introduced into the labyrinth grooves to keep piston-ring function for a long time. A gas leaked along the bottom surface of the piston ring is decreased owing to labyrinth action of the annular groove.
- the inventor of the present invention thought that a layer different from Al might be formed to obtain no minute bores in the inner surface of the cylinder.
- Metal plating such as Ni or Cr is applied to the inner surface of the cylinder, but coating of Ni and Cr decreases sliding performance and seizure resistance. Especially in high-pressure and high-temperature operation, it does not improve the life of the piston ring.
- an object of the invention to provide an oilless reciprocating air compressor operable at high-pressure and high-temperature of 2 to 3 MPa over 1 MPa to prevent generation of small resin pieces from a piston ring which slidably reciprocates in a cylinder to keep sealing capapility of the piston ring for a long time, to prevent abnormal sounds caused by leakage and to prevent heat from transmitting to a bearing of a piston, further avoiding damages or fauling during reciprocation of the piston ring or piston to greatly extend the life of the piston ring to keep its performance for a long time.
- An oilless reciprocating air compressor according to the present invention provides structural features as below:
- COPNA resin of which the piston is made is a thermosetting resin prepared by crosslinking a polycyclic aromatic hydrocarbon, such as naphthalene, anthracene, phenanthrene, pyrene or coal tar pitch, by paraxylene glycol in the presence of an acid catalyst.
- COPNA is an abbreviation of “condensed polynuclear aromatic” and is known in U.S. Pat. No. 5,605,401.
- Graphite in both the piston and the piston ring has heat resistance and increases sliding performance. Teflon of the piston ring provides self-lubricating property.
- the inner surface of a cylinder 1 made of Al or Al alloy is worked and a SiC coating 21 is formed on the inner surface.
- the minimum thickness of the coating is advantageous for manufacturing cost.
- the life of a resin piston ring 20 requires more than ten thousand hours and its thickness thus requires more than 10 ⁇ m as initial wear is 2 to 3 ⁇ m. Accordingly the thickness is determined to 15 ⁇ m.
- the thickness of the coating 21 may be more than 0.5 ⁇ m.
- the SiC coating is 0.5 ⁇ m thick at minimum, and 50 to 100 ⁇ m thick at maximum.
- the surface is ground to allow average surface roughness Ra to be 0.05 to 0.5 ⁇ m.
- SiC contained in the SiC coating 21 comprise minute ceramic particles having diameter of less than 1 ⁇ m, so that high-hardness dense flat surface layer is formed on the inner surface of the cylinder 1 . Therefore, coefficient of friction is decreased to improve sliding performance and wear resistance is greatly increased, thereby increasing the life of the piston ring 20 significantly and facilitating maintenance of an oilless reciprocating air compressor.
- SiC in the coating 21 increases heat-releasing effect.
- the piston ring 20 reciprocates with high lubricating property and reduces sliding resistance. Heat releasing capability of SiC contained in the coating 20 increases the life of the piston ring 20 . Furthermore, there is no resin powders 20 a separately generated from the piston ring 20 or significantly few compared with the prior art thereby effectively preventing a sliding portion from being damaged.
- FIG. 4 there is no resin small pieces 20 a from the piston ring 20 as shown in FIG. 3 , and the piston ring 20 always contacts the lower surface to prevent air from going down out of the piston 15 .
- the outer surface of the piston ring and the inner surface of the cylinder are both high lubricating property.
- the inner surface of the cylinder is flat and provides high hardness. Owing to heat-releasing effect of the SiC coating, the piston ring is initially worn by about 100 ⁇ m, but thereafter worn very slowly for a long time.
- SiC coating significantly increases the life of the resin piston ring to overcome the foregoing disadvantages not only at low pressure and low temperature but also at high pressure and high temperature.
- FIG. 5 shows another embodiment of the present invention
- the thickness “S 1 ” of a right-side SiC coating 21 at a portion to which higher side thrust acts by a piston 15 during operation is slightly greater than the thickness “S 2 ” at the other side.
- a receiving projection 19 a in an annular groove 19 is positioned at the thicker SiC coating 21 .
- An abutment 22 or a gap between the ends of a piston ring 20 is engaged on the side surfaces of the receiving projection 19 a , so that an opening of the abutment 22 is closed by the inner surface of a cylinder.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Compressor (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Abstract
In an oilless reciprocating air compressor, a piston reciprocates in a cylinder to compress a gas sucked from the outside and the compressed gas is discharged to the outside. The piston has an annular groove on the outer circumference, and a piston ring made of self-lubricating resin composite material is placed in the annular groove. The inner surface of the cylinder has SiC coating to increase the life of the piston ring, thereby allowing the compressor to be used at high pressure and high temperature efficiently to increase durability.
Description
- The present invention relates to an oilless reciprocating air compressor.
- In U.S. Pat. No. 5,117,742, a piston in an oilless reciprocating air compressor is made of resin and has an annular groove on the outer circumference. A piston ring made of resin is fitted in the annular groove, and the piston reciprocates in a cylinder.
- In the oilless reciprocating air compressor, it is not necessary for lubricating oil to be fed into a piston ring, a piston or a cylinder. Lubricating oil is not introduced into a compression chamber in the cylinder, and is not contained in compressed air discharged from the compressor. Thus, oilless reciprocating air compressors are widely used in medical, food or oxygen-feeding field that do not like oil in compressed air, or among users who are troubled in feed and maintenance of lubricating oil.
- When the resin piston is employed, the cylinder is made from Al or Al alloy flattening, casting or die casting material, and to increase hardness in the inner surface of the cylinder, hard alumite is applied to the inner surface that is in sliding contact with the piston. Anode oxidation coating having the maximum thickness of about thirty microns is formed and grounded to finish the cylinder.
- In the oilless reciprocating air compressor, a resin piston is fitted in the cylinder, and reciprocated with a resin piston ring and a resin rider ring. The resin piston ring exhibits desired performance for a long time without replacement. Even if the resin piston ring should fail to be replaced, operation will be able to be continued without fouling because the piston provides self-lubricating capability though air amount discharged from the compressor decreases.
- Recently oilless reciprocating air compressors usable under high-pressure range such as 2 to 3 MPa above 1 MPa have been demanded.
- However, when a compressor operates under high pressure of 2 to 3 MPa with a cylinder made of Al where hard alumite is applied to the inner surface to increase hardness and is ground on anode oxidization coating, the hard alumite layer on the inner surface of the cylinder decreases heat-releasing effect at high temperature and high pressure to increase temperature of the hard alumite layer and to expand openings of innumerable cellular minute bores generated on the inner surface of the cylinder owing to hard alumite treatment. Thus, the outer surface of the resin piston ring slidably reciprocates on the expanded openings of the bores, so that the outer surface of the resin piston ring is chipped off to make the piston ring worn faster.
- Furthermore, small pieces which are peeled off the outer surface of the resin piston ring are put into a gap between the lower surface of the piston ring and the bottom surface of an annular groove as the piston ring goes up in the annular groove. When the piston ring goes down in the annular groove during rising compression stage, a space is created by the inserted small pieces so as to involve leakage between the piston and the cylinder.
-
FIG. 1 is a vertical sectional front view of a known oilless reciprocating air compressor -
FIG. 2 is a vertical sectional view taken along the line II-II inFIG. 1 ; -
FIG. 3 is an enlarged view of the circle “A” inFIG. 2 ; -
FIG. 4 shows one embodiment of the present invention and is similar toFIG. 3 ; and -
FIG. 5 shows another embodiment of the present invention and is corresponding to an enlarged horizontal sectional view taken along the line V-V inFIG. 2 . - Based on the drawings, a known oilless reciprocating air compressor will be described. As shown in
FIG. 1 , at the upper end of an Al orAl alloy cylinder 1, a cylinder head 4 is mounted via a suckingvalve plate 2 and a spacer 3. The cylinder head 4 is separated into asuction chamber 6 and adischarge chamber 7 by apartition wall 5. Aninlet 8 is formed in the side wall of thesuction chamber 6 and an outlet 9 is formed in the side wall of thedischarging chamber 7. - A
sucking bore 10 is formed through the bottom of thesuction chamber 6, anddischarge bores valve plate 2 to communicate with thedischarge chamber 7. - A
discharge valve plate 13 is mounted on the spacer 3 at the upper end of thedischarge bore 11 and opens to communicate with thedischarge chamber 7. - A
hard alumite layer 14 is formed on the inner surface of thecylinder 1, and anAl alloy piston 15 is slidably fitted in thecylinder 1. Apiston pin 16 which radially extends in thepiston 15 is connected to acrankshaft 18 via a connectingrod 17. - An
annular groove 19 is formed on thepiston 15 and aresin piston ring 20 is fitted in theannular groove 19 to move slightly. - The
crankshaft 18 is rotated to allow thepiston 15 to reciprocate via the connectingrod 17, so that air sucked through theinlet 8 and thesucking bore 10 is compressed and discharged through thedischarge bore - When the inner surface of the
cylinder 1 rises to high temperature and high pressure, temperature of the hardalumite layer 14 on the surface rises. Then, a large number of minute bores of thealumite layer 14 on the inner surface of thecylinder 1 expand. Thus, the outer surface of thepiston ring 20 slidably reciprocates on the expanded opening ends of the bores thereby causing the outer surface of theresin piston ring 20 to be shaved off, so that the life of thering 20 becomes shorter. - As shown in
FIG. 3 , a number ofsmall resin pieces 20 a peeled off the outer surface of theresin piston ring 20 come into a gap between theresin piston ring 20 and the lower surface of the piston-ring groove 19 to form an air path therebetween. As shown by an arrow inFIG. 3 , leakage occurs through the space to decrease compression efficiency and to cause noise. - Accordingly, sealing capability of the
resin piston ring 20 becomes poor to decrease discharge performance of the oilless reciprocating air compressor. Furthermore leakage is likely to generate abnormal sound. High temperature air on a compression chamber thermally gives adverse effects to a bearing of the piston, thereby decreasing the lives of thepiston pin 16, the end of the connectingrod 17 and the bearing. - In high-pressure and high-temperature operation, the piston ring is abnormally worn to decrease sealing capability and is then worn locally to breakage. To prevent abnormal sound during operation and prevent the life of the bearing from reducing owing to heat by leaked high-temperature compressed air, the piston ring has to be replaced at an earlier stage.
- To solve such disadvantages, in Japanese Utility Model Pub. No. 35-14811, one or more labyrinth grooves are formed on the upper and lower surfaces of the annular groove, and small pieces of worn piston ring are introduced into the labyrinth grooves to keep piston-ring function for a long time. A gas leaked along the bottom surface of the piston ring is decreased owing to labyrinth action of the annular groove.
- However, as operation continues, the piston-ring small pieces in the labyrinth groove increase to come into the piston-ring groove, so that desired purposes cannot be attained after a certain time passes.
- To solve such disadvantages, the inventor of the present invention thought that a layer different from Al might be formed to obtain no minute bores in the inner surface of the cylinder. Metal plating such as Ni or Cr is applied to the inner surface of the cylinder, but coating of Ni and Cr decreases sliding performance and seizure resistance. Especially in high-pressure and high-temperature operation, it does not improve the life of the piston ring.
- In view of the disadvantages, it is an object of the invention to provide an oilless reciprocating air compressor operable at high-pressure and high-temperature of 2 to 3 MPa over 1 MPa to prevent generation of small resin pieces from a piston ring which slidably reciprocates in a cylinder to keep sealing capapility of the piston ring for a long time, to prevent abnormal sounds caused by leakage and to prevent heat from transmitting to a bearing of a piston, further avoiding damages or fauling during reciprocation of the piston ring or piston to greatly extend the life of the piston ring to keep its performance for a long time.
- An oilless reciprocating air compressor according to the present invention provides structural features as below:
- Cylinder
-
- Size: bore 50 mm, 75 mm
- Material: Al or Al alloy
- Inner surface: SiC coating formed by plating
- Hardness of the coating: Vickers Hv 1600 to 2400
- Thickness of the coating: 15 μm
- Average surface roughness: Ra mirror surface finishing of 0.05 to 0.5 μm
Piston
- Size: external diameter 50 mm, 75 mm, Height: 50 mm, 75 mm
- Material: Composite material of COPNA resin and graphite
Piston Ring - Size: nominal diameter 50 mm, 75 mm, width 4.53 mm, thickness 4.0 mm
- Material: Composite material of polytetrafluoroethylene resin (Teflon™) and graphite
- Features:
tension strength 13 to 35 MPa,compression strength 10 to 13 MPa, Vickers hardness: Hv 360 to 400 - COPNA resin of which the piston is made is a thermosetting resin prepared by crosslinking a polycyclic aromatic hydrocarbon, such as naphthalene, anthracene, phenanthrene, pyrene or coal tar pitch, by paraxylene glycol in the presence of an acid catalyst. “COPNA” is an abbreviation of “condensed polynuclear aromatic” and is known in U.S. Pat. No. 5,605,401. Graphite in both the piston and the piston ring has heat resistance and increases sliding performance. Teflon of the piston ring provides self-lubricating property.
- The features of a SiC coating as above are grounded as below.
- The inner surface of a
cylinder 1 made of Al or Al alloy is worked and aSiC coating 21 is formed on the inner surface. The minimum thickness of the coating is advantageous for manufacturing cost. - In an industrially usable oilless reciprocating air compressor, the life of a
resin piston ring 20 requires more than ten thousand hours and its thickness thus requires more than 10 μm as initial wear is 2 to 3 μm. Accordingly the thickness is determined to 15 μm. In a small load reciprocating air compressor, the thickness of thecoating 21 may be more than 0.5 μm. The SiC coating is 0.5 μm thick at minimum, and 50 to 100 μm thick at maximum. - After plating, the surface is ground to allow average surface roughness Ra to be 0.05 to 0.5 μm.
- SiC contained in the
SiC coating 21 comprise minute ceramic particles having diameter of less than 1 μm, so that high-hardness dense flat surface layer is formed on the inner surface of thecylinder 1. Therefore, coefficient of friction is decreased to improve sliding performance and wear resistance is greatly increased, thereby increasing the life of thepiston ring 20 significantly and facilitating maintenance of an oilless reciprocating air compressor. - SiC in the
coating 21 increases heat-releasing effect. - Along the
coating 21 containing silicon having high lubricating property on the inner surface of thecylinder 1, thepiston ring 20 reciprocates with high lubricating property and reduces sliding resistance. Heat releasing capability of SiC contained in thecoating 20 increases the life of thepiston ring 20. Furthermore, there is no resin powders 20 a separately generated from thepiston ring 20 or significantly few compared with the prior art thereby effectively preventing a sliding portion from being damaged. - In
FIG. 4 , there is no resinsmall pieces 20 a from thepiston ring 20 as shown inFIG. 3 , and thepiston ring 20 always contacts the lower surface to prevent air from going down out of thepiston 15. - Experiments
- In three air-cooling oilless reciprocating air compressors having the same size, the same volume and the same dimensions as the above and different surface treatment on a
cylinder 1, experiments are carried out at four kinds of hours under the following conditions: -
- Compressing air pressure: full load operation at 1.4 MPa
- Average sliding speed of the piston: 2 to 3 m/sec
- Discharge temperature: about 200° C.
- Time: 2,500 hours, 5,000 hours, 10,000 hours, 20,000 hours
- As a result of the experiments, with a cylinder having a SiC coating of high lubricating property and high hardness and a self-lubricating piston ring or a high-lubriating piston, the outer surface of the piston ring and the inner surface of the cylinder are both high lubricating property. The inner surface of the cylinder is flat and provides high hardness. Owing to heat-releasing effect of the SiC coating, the piston ring is initially worn by about 100 μm, but thereafter worn very slowly for a long time.
- Decrease in discharged air amount is very little, and neither noise nor damage occurs. Especially a resin piston ring of an oilless reciprocating air compressor operated at high pressure and high temperature can be used without replacement about five times as long as a conventional device having an alumite-treatment cylinder.
- Thus, in an oilless reciprocating air compressor having no lubricating oil between an resin piston and a resin piston ring, and a cylinder, SiC coating significantly increases the life of the resin piston ring to overcome the foregoing disadvantages not only at low pressure and low temperature but also at high pressure and high temperature.
-
FIG. 5 shows another embodiment of the present invention, The thickness “S1” of a right-side SiC coating 21 at a portion to which higher side thrust acts by apiston 15 during operation is slightly greater than the thickness “S2” at the other side. A receivingprojection 19 a in anannular groove 19 is positioned at thethicker SiC coating 21. Anabutment 22 or a gap between the ends of apiston ring 20 is engaged on the side surfaces of the receivingprojection 19 a, so that an opening of theabutment 22 is closed by the inner surface of a cylinder. - The foregoing merely relate to embodiments of the invention. Various changes and modifications may be made by a person skilled in the art without departing from the scope of claims wherein:
Claims (7)
1. An oilless reciprocating air compressor comprising:
a cylinder made of Al or Al alloy;
a piston that reciprocates in the cylinder so that a gas sucked from an outside is compressed and discharged from the cylinder, said piston having an annular groove on an outer circumferential surface; and
a piston ring fitted in the annular groove of the piston and made of composite material of self-lubricating resin and heat-resistant material for increasing sliding performance, an inner surface of the cylinder having SiC coating.
2. An oilless reciprocating air compressor as claimed in claim 1 wherein the self-lubricating material of the piston ring comprises polytetrafluoroethylene and the heat-resistant material comprises graphite.
3. An oilless reciprocating air compressor as claimed in claim 1 wherein the piston is made of self-lubricating composite material.
4. An oilless reciprocating air compressor as claimed in claim 3 wherein the self-lubricating composite material comprises condensed polynuclear aromatic resin and graphite for increasing sliding performance.
5. An oilless reciprocating air compressor as claimed in claim 1 wherein the SiC coating is made by plating.
6. An oilless reciprocating air compressor as claimed in claim 1 wherein thickness of the SiC coating of a portion to which higher side thrust acts by the piston is greater than that at the other side.
7. An oilless reciprocating air compressor as claimed in claim 1 wherein a receiving projection in the annular groove of the piston is provided at a portion to which higher side thrust acts, the projection engaging in an abutment of the piston ring.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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JP2004-56632 | 2004-03-01 | ||
JP2004056632A JP2005248729A (en) | 2004-03-01 | 2004-03-01 | Oil-free reciprocating air compressor |
Publications (1)
Publication Number | Publication Date |
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US20050188839A1 true US20050188839A1 (en) | 2005-09-01 |
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Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/069,371 Abandoned US20050188839A1 (en) | 2004-03-01 | 2005-03-01 | Oilless reciprocating air compressor |
Country Status (5)
Country | Link |
---|---|
US (1) | US20050188839A1 (en) |
EP (1) | EP1577553A1 (en) |
JP (1) | JP2005248729A (en) |
KR (1) | KR20060043273A (en) |
CN (1) | CN1664365A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060060164A1 (en) * | 2004-09-20 | 2006-03-23 | Gerfast Sten R | Internal combustion engine without oil |
US20080242966A1 (en) * | 2007-03-27 | 2008-10-02 | Hideo Sagehashi | Air pulse discharging device for noncontact type tonometer and noncontact type tonometer having the same |
US9856866B2 (en) | 2011-01-28 | 2018-01-02 | Wabtec Holding Corp. | Oil-free air compressor for rail vehicles |
US20180372129A1 (en) * | 2017-06-26 | 2018-12-27 | Fujikoki Corporation | Pilot type solenoid valve |
US10837399B2 (en) | 2016-07-19 | 2020-11-17 | Tpr Co., Ltd. | Method of manufacturing internal combustion engine, internal combustion engine, and connected cylinder |
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JP5026689B2 (en) * | 2005-11-17 | 2012-09-12 | 株式会社日立産機システム | Reciprocating compressor |
KR100755945B1 (en) | 2006-04-28 | 2007-09-06 | 주식회사코핸즈 | Semi-Oiled Oilless Air Compressor |
US8359967B2 (en) * | 2006-09-29 | 2013-01-29 | Schlumberger Technology Corporation | Fluid end reinforced with a composite material |
TW201104074A (en) * | 2009-07-24 | 2011-02-01 | wen-san Zhou | Air compressor |
ITMI20110959A1 (en) * | 2011-05-27 | 2012-11-28 | Ceme Spa | OSCILLATING CURSOR TYPE ELECTRIC PUMP |
EP3176436B1 (en) * | 2012-02-20 | 2018-05-16 | Panasonic Corporation | Slide member, refrigerant compressor incorporating slide member, refrigerator and air conditioner |
KR20150103271A (en) * | 2013-01-31 | 2015-09-09 | 가부시키가이샤 도요다 지도숏키 | Compressor |
SG11201603955UA (en) * | 2013-12-26 | 2016-07-28 | Hitachi Ind Equipment Sys | Piston ring and compressor using the same |
JP6090303B2 (en) * | 2014-12-24 | 2017-03-08 | マツダ株式会社 | engine |
CN105221392B (en) * | 2015-10-26 | 2017-09-19 | 珠海格力节能环保制冷技术研究中心有限公司 | Compressor lubricant oil injecting structure and compressor |
CN106523320B (en) * | 2017-01-13 | 2018-08-17 | 厦门闳图盛道科技有限公司 | A kind of oil-free silent air compressor of low energy consumption |
DE102017218156A1 (en) * | 2017-10-11 | 2019-04-11 | Mahle International Gmbh | Oil-free compressor |
CN112594153B (en) * | 2020-12-16 | 2023-08-15 | 浙江凯途机电有限公司 | Energy-saving gas oil-free compressor and multi-stage compression structure thereof |
JP7521131B2 (en) | 2022-03-24 | 2024-07-23 | 株式会社リケン | Sliding Mechanism |
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US5117742A (en) * | 1989-04-28 | 1992-06-02 | Iwata Air Compressor Mfg. Co. Ltd. | Piston of composite material with c-shaped ring groove |
US5605401A (en) * | 1994-10-31 | 1997-02-25 | Ntn Corporation | Rolling contact bearing |
US5941161A (en) * | 1996-12-06 | 1999-08-24 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressor |
US6457722B1 (en) * | 1997-06-02 | 2002-10-01 | Maschinenfabrik Sulzer-Burckhardt | Sealing element for dry running systems and the use of a sealing element of this kind |
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DE1273826B (en) * | 1963-08-20 | 1968-07-25 | Erdoelchemie Gmbh | Process for the production of porous metal bodies, in particular for use as catalysts |
JPS58183881A (en) * | 1982-04-19 | 1983-10-27 | Matsushita Electric Ind Co Ltd | Compressor |
-
2004
- 2004-03-01 JP JP2004056632A patent/JP2005248729A/en active Pending
-
2005
- 2005-02-24 EP EP05003997A patent/EP1577553A1/en not_active Withdrawn
- 2005-02-25 CN CN2005100089459A patent/CN1664365A/en active Pending
- 2005-02-28 KR KR1020050016752A patent/KR20060043273A/en not_active Ceased
- 2005-03-01 US US11/069,371 patent/US20050188839A1/en not_active Abandoned
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5117742A (en) * | 1989-04-28 | 1992-06-02 | Iwata Air Compressor Mfg. Co. Ltd. | Piston of composite material with c-shaped ring groove |
US5605401A (en) * | 1994-10-31 | 1997-02-25 | Ntn Corporation | Rolling contact bearing |
US5941161A (en) * | 1996-12-06 | 1999-08-24 | Kabushiki Kaisha Toyoda Jidoshokki Seisakusho | Piston type compressor |
US6457722B1 (en) * | 1997-06-02 | 2002-10-01 | Maschinenfabrik Sulzer-Burckhardt | Sealing element for dry running systems and the use of a sealing element of this kind |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060060164A1 (en) * | 2004-09-20 | 2006-03-23 | Gerfast Sten R | Internal combustion engine without oil |
US20080242966A1 (en) * | 2007-03-27 | 2008-10-02 | Hideo Sagehashi | Air pulse discharging device for noncontact type tonometer and noncontact type tonometer having the same |
US9856866B2 (en) | 2011-01-28 | 2018-01-02 | Wabtec Holding Corp. | Oil-free air compressor for rail vehicles |
US10837399B2 (en) | 2016-07-19 | 2020-11-17 | Tpr Co., Ltd. | Method of manufacturing internal combustion engine, internal combustion engine, and connected cylinder |
US20180372129A1 (en) * | 2017-06-26 | 2018-12-27 | Fujikoki Corporation | Pilot type solenoid valve |
Also Published As
Publication number | Publication date |
---|---|
KR20060043273A (en) | 2006-05-15 |
JP2005248729A (en) | 2005-09-15 |
EP1577553A1 (en) | 2005-09-21 |
CN1664365A (en) | 2005-09-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: ANEST IWATA CORPORATION, JAPAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:INOUE, HIROSHI;REEL/FRAME:016349/0639 Effective date: 20050210 |
|
STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |