AU604258B2 - Orbit gas compressor - Google Patents

Description

nis ij _~.ur.u 6iD^ F S F Ref: 36841 FORM COMMONWEALTH OF AUSTRALIA PATENTS ACT 1952 COMPLETE SPECIFICATION This document contains the amendments made under Section 49 and is correct for printing

(ORIGINAL)

FOR OFFICE USE: Class Int Class Complete Specification Lodged: Accepted: Published: Priority: S Related Art: A Name and Address of Applicant: *-w Hansen Engine Corporation 14920 Minnetonka Industrial Road Minnetonka Minnesota 55345 UNITED STATES OF AMERICA w n it jr Address for Service:

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Spruson Ferguson, Patent Attorneys Level 33 St Martins Tower, 31 Market Street Sydney, New South Wales, 2000, Australia Complete Specification for the invention entitled: Orbit Gas Compressor The following statement is a full description of this invention, including the best method of performing it known to me/us

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I-i i L ii i -LCLL_ -I i) -2- FIELD OF INVENTION The invention relates to devices for pumping fluids. The device is an orbital pump for compressing a gas, such as air.

BACKGROUND OF THE INVENTION Rotary pumps have rotatable members including vanes for moving a fluid, such as air, through a compression chamber. These pumps have seal structures interposed between the movable and stationary parts to reduce leakage and enhance the compressors efficiency. The engaging parts of these rotary pumps are subject to high sliding speeds which may result in wear and considerable friction which limit the efficiency and useful life of the pumps. Examples of rotary piston compressors are shown in Lawton in I *j Patent No. 2,423,507 and Jerneas in U.S. Patent No. 3,221,664.

SUMMARY OF INVENTION The present invention in one broad form provides an orbital piston pump in which an orbital piston is movable in an eccentric cyclic path within a housing by means of a first eccentric member comprising a rotary drive shaft having an eccentric portion coacting with the piston for moving the piston in its eccentric cyclic path within the housing, and eccentric means rotatably mounted on the housing at a location which is spaced apart from the drive shaft, and having an eccentric portion coacting with the piston for preventing angular movement of the piston as it moves in its eccentric cyclic path within the housing with sealing means carried by the piston contacting a cylindrical inner wall of the housing to define therewith fluid pumping volumes for pumping fluid from an inlet to an outlet, wherein each of the sealing means carried by the piston comprises projections slidably received in arcuate slots in side walls of the S housing, each arcuate slot having a radius which is concentric with the cylindrical inner wall but is closer to the axis of the housing than that i inner wall, whereby limiteu arcuate movement of the sealing means is permitted relative to the housing as the piston moves in its eccentric movement and maintained in sealing engagement with the inner wall by the arcuate slots throughout said movement.

KLN/25361

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-I i I~(LU~1~I -3- Advantageously, the apparatus has a plurality of pairs of intake and exhaust valves mounted on the housing for controlling a flow of fluid Into and out of the chamber segments. Typically, a piston located within the chamber is mounted on a shaft rotatably mounted on the housing. The shaft is a first eccentric member that extends through a generally central bore in the piston whereby the rotation of the shaft will move the piston relative to the housing to affect thn pumping of the fluid through the chamber. Additional eccentric members may rotatably cooperate with the first eccentric member to limit th'e angular movement of the piston during the rotation of the shaft. A plurality of seal assemblies may be arranged around the piston to divide the chamber into chamber segments and locate the seal assemblies between each pair of the intake and exhaust valves.

The seal assemblies may have vane means associated with the housing to permit arcuate movement of the vane means and restrict radial movement with S 5 respect to the housing thereof during the orbial movement of the piston.

The seal assemblies may have pairs of blades or vanes located In generally radial slots in the piston. The slots may be circumferentially spaced around the piston. The circumferential space between adjacent seal assemblies can be equal or vary to provide selected working volumes for the chamber segments. Each blade may have engaging adjacent side surfaces and Souter ends. The outer ends have transverse grooves which accommodate seal S members. The seal members may be located in sliding and sealing engagement -ith the inner cylindrical wall of the housing and move along the arc o? the inner cylindrical wall. Beneficially, a cross bar attached to each blade has outer ends located in arcuate slots in the end plates of the housing. The arcuate slots cooperate with the outer ends of the cross bars to allow the blades to move relative to each other and have limited arcuate movement concentric with the arc of the inner cylindrical wall of the housing and restrict radial movement with respect to the housing thereof.

St 30 This ensures a uniform and constant sealing contact between the seal members and the inner cylindrical wall of the housing. The seal members i have relatively low sealing frictional engagement with the inner cylindrical wall of the housing and relatively low sliding speeds as compared to other constant displacement devices. The anchoring of the vanes on the housing minimizes the centrifugal force on the seal members and vanes thereby reducing sealing friction. This results in an effective seal having a long useful wear life.

KLN/25361

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LS U w 4 DESCRIPTION OF DRAWINGS A preferred form of the present invention will now be described by way of example with reference to the accompanying drawings, wherein: Fig. 1 is a side elevational view of the orbital gas compressor of the invention; Fig. 2 is a side view of the left side of Fig. 1; Fig. 3 is a side view of the right side of Fig. 1; Fig. 4 is an enlarged sectional view taken along the line 4-4 of Fig.

Fig. 5 is a sectional view taken along the line 5-5 of Fig. 4; Fig. 6 is a reduced scale sectional view taken along the line 6-6 of Fig. 4; Fig. 7 is an enlarged sectional view taken along tL V a. a Va.

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000 0400 oOtO 0000 0 0 *0 I 00 0 004 00 0 I 00* the line 7-7 of Figure 6; Figure 8 is a reduced s'cale sectional view taken along the line 8-8 of Figure 4; Figure 9 is an enlarged elevational view, partly sectioned, of a seal assembly as shown in Figure 6; Figure 1.0 is an enlarged sectional view taken along line 10-10 of Figure 91 Figure 11 is an enlarged sectional view taken along the line 11-11 of Figure 103 Figure 12 is an elevationa. view similar to Figure 9 of a modification of the seal assembly; Figure 13 is a sectional view taken along line 13--3.3 of Figure 12; Figure 14 is a sectional view taken along line 14-14 of Figure 121 Figure 15 is an enlarg'2!d sectional view taken along line 15-15 of Figure 12; and Figure 16 is a sectional view taken along line 16-16 of Figure DESCRIPTION OF PREFERRED EMBODIMENT Referring to Figures 1 to 4, there is shown the pumping apparatus of the invention indicated generally at operable to compress and pump gas, such as air, and deliver the compressed gas to a desired location. Apparatus 20 is operable to pump fluids including liquids, gases and fluid-like materials. The following description is directed to an apparatus for pumping air. Apparatus 20 efficiently 0~ 00 000 0 00 00 0~ 4000 0 1 00 02 41 0 0 01 I- 1~

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a a a a~ .s 6 C C Ste a at a e compresses the air with minimum of vibration and wear on its operative parts. The moving and sealing components of apparatus 20 have low sliding speeds and low sealing friction which improves the pumping and compression efficiency and wear life of the apparatus.

Apparatus 20 has an annular housing indicated generally at 21 secured to a supporting frame 22. Frame 22 is attached to fixed base 23 or similar support. Frame 22 has a generally horizontal plate 32 adapted to be secured to base 23. A pair of upright legs 33 and 34 secured to the top of plate 32 engage opposite portions of housing 21. As shown in Figure 1, a plurality of bolts 36 secure the upper ends of the legs 33 to housing 21. Log 34 is secured to housing 21 in a similar manner. Other types of frames ca~n be used to support the apparatus in its Working environment.

As shown in Figures 4, 6, and 7, housing 21 has a circular body 24 having an internal cylindrical wall 26.

End plates 27 and 28 are secured to opposite sides of body 24 with bolts 29 and 31. A cylindrical piston or orbitor, aD indicated generally at 37, is located in chamber 40. Piston 37 has an outer cylindrical surface 38 and a diameter smaller that the diameter of the cylindrical wall 26 of body 24. Surface 38 and cylindrical wall 26 are shown circular but need not be and are machined withi conventional machine '*ools. Pairs of arcuate segment side seals 39 and 41 carried by piston 37 adjacent surface 38 engage the inside surfaces of'end plates 27 and 28 to minimize the leakage of gas from compression chamber 40, Piston 37 is mounted on a i

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shaft 42. As shown in Figure 4, a first bearing 43 rotatably mounts one end of shaft 42 on end plate 27. A second bearing 44 rotatably mounts the opposite end of shaft 42 on end plate 28. The portion of shaft 42 between end plates 27 and 28 has an enlarged cylindrical eccentric :1 journal or hub 46. A bearing 47 surrounding hub 46 rotatably supports piston 37 on hub 46.

A pair of counter weights 48 and 49 are mounted on shaft 42 adjacent opposite sides of end plates 27 and 28 to balance shaft 42 and piston 37. Counter weight 49, as shown in Figure 5, has a generally semi-circular shape. A cap 51 located over shaft 42 is secured to counter weight 49 with a plurality of bolts 52, A key or spline is used to index counter weight 49 to shaft 42 to balance the system. Counter weight 48 is secured to shaft 42 in a similar manner. Referring to Figure 4, a disk 53 is located adjacent an end of shaft 42 and counter weight 49, A cylindrical tube 54 space plate 53 from end plate 27 providing a confined space for rotating counter weight 49.

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A plurality of bolts 56 extend through tube 54 securing plate 53 to end plate 27.

A generally flat annular member 57 is spaned laterally from end plate 27 with a ring 58. A plurality of bolts 59 secure member 57 and ring 58 to the outside of end plate 27. The space between annular member 57 and end plate 27 is an air inlet chamber having a mouth or opening 62. An annular air filter 63 surrounds opening 62. Filter 63 is a conventional ring filter having a filter element. A C C V C C

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ala 4 aaa aa a a a aa~ a aa a a at aaqa a at a tt circular cover 64 is mounted on theoutside of filter 63. A bolt 66 threaded into a nut 67 mounted on the center of disk 53 extends through a center hole in cover 64. A wing nut 68 on bolt 66 retains cover 64 and filter 63 in assembled relation with annular member 57.

A flywheel 69 is attached to shaft 42 with a cylindrical collar 72 located about a sleeve 73. Sleeve 73 is located in tight gripping engagement with shaft 42.

Collar 72 and sleeve 73 having engaging tapured surfaces. A 1c: nut 75 threaded on sleeve 73 in engagement with the outer end of collar 72 holds collar 72 on sleeve 73 and sleeve 73 on shaft 42. A plurality of bolts 74 3ecurfe flywheel 69 to collar 72. Ant external source of power (not shown), such as electric motor or internal combustion engine, is, coupled to shaft 42 to rotate flywheel 69 and shatt 42.

End plate 27 has an air inlet pasoage 76 leading to an air inlet valve assembly indicated generally at 77.

Valve assembly 77 is a one way valve operable to allow air to flow into the chamber 40 as indicated by the arrows in 20 response to the orbital movement of piston 37. Valve assembly 77 includes a cup-shaped sleeve 83 located in a bore 79 in body 24. Body 24 has an. internal inwardly directed lip 81 engageable with a valving member 82.

Valving member 82 is mounted on the open end of sleeve 83 located within bore 79, Sleeve 83 has a chamber 84 open to hold the valve assembly in assembled relation with body 24.

A plurality of bolts 87 secure cover 86 to body 24. Bolts 87 can be removed allowing cover 86 as well as the entire ii C, tC *14 t Ct *1 C

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Apparatus 20 has an exhaust valve assembly indicated generally at 88 operable to allow compressed air to flow into an outlet passage 89 which leads to an annular manifold 91. Manifold 91 has a gas outlet connection 92 adapted to be connected to a gas receiver such as a tank, gas line or the like. A plurality of bolts 93 secure manifold 91 to the outside of end plate 28.

Valve assembly 88 has a cup-shaped sleeve 99 lo.cated within a radial bore 96 in body 24. Body 24 has an inwardly directed annular lip 97 supporting a valving member 98. The valving member 98 is movably mounted in sleeve 99 positioned within bore 96. Sleeve 99 has a chamber 101 which accommodates valving member 98 and is open to outlet passage 89. A cover 102 fits over sleeve 99. A plurality of bolts 103 attach cover 102 to body 24. Bolts 103 can be removed so that cover 102 as well as the valve assembly can be withdrawn from body 24 for servicing and replacement.

Apparatus 20 has five pair of inlet and exhaust valve assemblies mounted in body 24. Inlet valve asoembly 77 and exhaust valve assembly 88 are commercial one-way valves, such as reed, plate or disk valves.

Referring to Figure 6, piston 37 is operatively associated with a pair of eccentric members 104 and 106 which control the orbital movement of piston 37 during rotation of shaft 42. As shown in Figure 7, eccentric 104 is located within a bore 107. Roller bearings 108 located I A- 7 ii ri 11

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1 -9 q in bore 107 rotatably mount eccentric 104 in piston 37. oil.

seals 109 surround opposite ends of eccentric 104 adjacent opposite ends of bearings 108. Eccentric 104 has a pair of outwardly directed shafts 110 and 113 rotatably mounter] on end plates 28 and 27, Shaft 110 fits into a bore 111, Roller bearings 112 support shaft 110 in bore 111. Shaft 113 fits into a bore 114 and is rotatably mounted therein wuith roller bearings 116. The axis of rotation of shafts 110 and 113 is laterally offset from the axis of eccentric 104. Piston 37 has a lubricating oil passage 117 connecting the mid-section of bore 107 and the mid-section of the central passage accommodating the bearing 47. Returning to Figure 6, eccentric 106 is identical1 in structure to eccentric 104. Eccentric 106 is angularly spaced about degrees from eccentric 104. Eccentric 106 has oppositely directed stub shafts 113 that rotatably mount eccentric 106 o on end plates 27 and 28. Eccentrics 104 and 106 control the orbital movement of piston 37 as indicated by arrow 119 such that no angular displacement with respect to housing 21 occurs on the piston.

Piston 37 has a bore 121 located midway between the bores for the eccentrics 104 and 106. A cylindrical counter weight 122 is located in bore 121 to compensate for the mass of eccentrics 104 and 106 thereby balancing piston 37. Ae shown in Figure 7, a plurality of snap rings 123 and 124 retain weight 122 in bore 121.

A plurality of seal assemblies indicated generally at 126, 127, 128, 129 and 130 are circumferentially spaced 1i~ ii about orbitor 37, Seal assemblies 126 130 divide chamber 40 into separate compression chamber segments or working volumes. Each chamber segment is an air pumping volume. As shown in Figure 6, apparatus 20 has five pumping volumes located between the adjacent seal assemblies. The number of pumping volumes can vary. Intake and exhaust valve assemblies are in communication with each pumping volume to control the flow of air into and out of the pumping volume.

Seal assemblies 126 130 are identical in structure. They have limited circumferential movement relative to inner wall 26 of body 24 and restricted radial movement relative to body 24. The seal assemblies 126 130 are in sliding sealing engagement with the inner cylindrical.

wall 26 of body 24. This engagement is coutinuous and substantially constant. The following de-ocription is limited to seal assembly 129. Referring to Figure 9, seal assembly 129 has a pair of generally flat vanes or blades 131 and 132 located within a radial slot 133 in piston 37.

The side walls of the slot accommodate transverse seal members 134, 135, 136 and 137, First seal strips 138 interconnect seal members 134 and 135, Second seal strips 139 interconnect seal members 136 and 137. Vane 131, as shown in Figure 10, has two generally triangular members 131A and 131B. The members 131A and 131B have engaging diagonal surfaces which allow the members to move in opposite outward directions. The outer side edge of member 131A engages plate 27. The outer side edge of member 131B engages plate 28. Vane 131 has a slot 141 across the width I7 1 I 6; ~c 0095 5551 cc .9 9* 2 69$ 59 9$ 994- 99 9 4,5- 5- 95- O 5- 5-5- 5-5-5-c 5- 5cc 5- 5-5- 5- 1 C -11

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of the outer end thereof accommodating a seal 142. Seal 142 can be made of ceramic material. An eliptical spring 143 located in the base of slot 141 biases the rounded outer end 144 of seal 142 into engagemeiit with inner wall 26 of body 24. The outer end oE vane 131 has a chamfer 146. The chamfer 146 allows vane 131 to have limited angular movement or tilt without. engaging the inner wall 26 of body 24. Vane 132 is located in side surface engagement with vane 131.

Vane 132 has a slot 147 across the width of the outer end thereof accommodating a seal member 148. A 8pring 149 in the base of groove 147 bia.s:es the outer end 151 of seal member 148 into sealing engagement with inner wall 26 of housing 21. Vane 132 has a chamfered outer end 152 which allows the vane limited angular movement or tilt which allows the vanes to move without contactiug the inner wall 26 of body 24. Vane 131 is attached with a bolt or pin 145 to a cross bar 153. A bolt 154 socures pin 145 to the mid-section of bolt 154. Pin 145 extends through a hole in olade me~~i~r 131B and is anchored' to mermber 131A. A 2Q compression spring 140 disposed about pin 145 engages vane member 1318 and cross bar 153. Spring 140 biases members 131A and 13113 toward each other and maintains members 131A and 131B in engagement with end plates 27 and 28. Other means can be used to secure cross bar 53 to vane 131. Cross bar 153 and vane 131 can be a one-piece member. Bar 153 has a first end 156 located in an arcuate slot 157 in the end plate 28. The opposite end 158 of bar 153 is located in an arcuate slot 159 in end plate 27. Needle bearings rotatably St C S it C 44 -12mount ends 156 and 158 in s)lotr; 157 arid 1539, As shown in Figure 8, end plate 27 has a plurality of arcuate slots 159, 159A, 159B, 159C, and 159D circumfere~ntially arranged about shaft 42 for the ends of the cross bars of the seal assemblies. The radius length of each of thle slots 157 arid 159 is the same as the radius of inner wall 26 of body 24.

In other words, the arcuate curve or cam track of slots 157 and 159 is the same as the arcuate curve of inner wall 26 of body 24. This relationship ensures restricted radial movement of vanes 131 and 132 relative to inner wal. 26 of body 24 during orbital movement of piston 37, The arcuate slots 157 and i59 allow seal assembly 129 limited movement during orbital movement of piston 37. In a like manner, a transverse bar 161 is secured to the inner end of blade 132.

ere, Bar 161 has opposite ends located in the slots 157 and 159, Ct Bar 161 carries the gas load arid small centrifugal load associated with seal assembly 129.

V In use, apparatus 20 is operated by driving shaft 42 with an external power source, such as an ulectric motor or it an internal combustion engine. Rotation of shaft 42 causes the primary eccentric 46 to rotate about the axis ot shaft 42, This causes pis-ton 37 to have orbital motion in the amount determined by distance between the axis of rotation ft C of shaft 42 in the axis of the eccentric 46. The secondary eccentrics 104 and 106 limit the angular movement of piston 37 causing the peripheral segments of outer surface 38 of piston 37 to sequentially move toward and away from the inner cylindrical wall 26 of the body 24. This results in a 1~ 1 Tj-2 pumping action causing the air to flow through each chamber segment. The air is drawn intc a chamber segment through inlet valve assembly 77 as shown by the arrows in Figure 4.

Piston 37, when moved toward the cylindrical inner wall 26 forces the air in the chamber segment out through the exhaust valve associated with the chamber. The air flows through the outlet passages 89 89D into manifold 91. The compressed air in manifold 91 flows through the gas outlet 92 to a receiver such as a tank or air line.

Seal assemblies 126 130 are in constant and generally uniform sealing engagement with the inner cylindrical wall 26. The seal assemblies divide chamber into separate pumping chamber segments. Each chamber segment is open to an intake Valve assembly and an exhaust valve-assembly', The seals 142 and 140 are maintained in :1 sliding frictional contact with the inner wall 26 and have K limited circumferential movement relative thereto. Vanes 131 and 132 are movably mounted on the end plates 127 and 128 through the cooperating means of the arcuate slots 157 and 159 and the ends of cross bars 153 and 161. Al~l of the seal assemblies are located in circumferentially spaced' generally radial slots in piston 37 so that the piston moves relative to the seal assemblies. This minimizes the centrifugal force on the seal assemblies thereby reducing the variations in the sealing loads on the vanes. The seal I assemblies have low sliding speeds and low sealing friction.

This improves the pumping and compression efficiency as well as the wear life of the seal assemblies.

A4 _I i i Referring to Figures 12 to 16, there is shown a modification of the seal assembly, indicated generally at 200 for use with piston 37 located in chamber 40. A plurality of seal assemblies 200 are circumferentially spaced around the piston in lieu of seal assemblies 126 130 shown in Figure 6. The following description is directed to a single seal assembly 200 as the remaining seal assemblies have the same structure and function.

Seal assembly 200 mounted on piston 37 is located in \c continuous sliding sealing engagement with the inner surface .26 of body 24. Piston 37 has a radial slot 202 slidably aaccommodating a generally flat blade or vane 201 having opposite flat sides 201A and 201B. A cross bar 203, shown as a cylindrical rod, extends transversely through the inner end of blade 201. Rollers 204 and 206 are mounted on the ends of bar 203. Side plates 27 and 28 of housing 21 have arcuate slots 157 and 159 providing tracks or cam surfaces for rollers 204 and 206. The arcuate length and shape of slot 159 is shown in Figure 12. Slot 157 has the same arcuate length and shape. The slots 157 and 159 are concentric with the inside cylindrical surface 26 of body a 9 24. Arcuate slots 157 and 159 positively position seal assembly 200 during orbital movement of piston 37 and i maintain seal assembly 200 in continuous sealing contact with inner surface 26 of body 24.

SThe outer end of blade 201 has a continuous transverse groove 207 accommodating generally flat seal members 208 and 211. Seal members 208 and 211 may be 1 RAZ r: c" ceramic material. Members 208 and 211, as shown in Figure 13, have inclined engaging surfaces and generally flat ends whereby the seal members 208 and 211 can move laterally relative to each other to provide end seals that engage the inside surfaces of end plates 27 and 28, Seal member 208 has an inside end shoulder 209 facing an inside end shoulder 212 on seal member 211. A bow spring 216 located in groove 207 in engagement with shoulders 209 and 212 biases seal members 209 and 211 into continuous engagement with O circumferential inner surface 26 of body 24. As shown in Figure 12, the outer end 214 of blade 201 is chamfered such (Ott that it does not contact inner surface 26 of body 24.

Blade 201 is slidably mounted on two pairs of bearing seals 217, 218, and 219, 220. Seals 217 220 each I have a semi-circular cross section and are mounted in a semi-circular groove in piston 37. The flat sides of seals j 217 220 are in sliding engagement with the opposite sides S 201A and 201B of the generally flat blade 201. As shown in broken lines in Figure 13, seals 219 and 220 extend the entire width of blade 201. Seals 217 and 218 also extend i i across the width of blade 201. A pair of bar seals 221 and cc C 222 are located outwardly of seals 218 and 220. Bar seals J, {221 and 222 bear against the opposite sides 201A and 201B of JJ blade 201 so as to minimize the leakage of gas into slot 202. Seal 221 is a flat member located in a groove 228 and cylinders 229 and 230. Cylinders 229 and 230 are located in holes 232 and 233 in opposite sides of piston 37. Cylinder 229 and piston 37 has a groove 228 accommodating bar seal 221 and wave spring 221A. A bar seal .222 and wave spring 222A are located in a groove 233 in piston 37 and cylinder 234. Springs 221A and 222A bias seals 221 and 222 into engagement with opposite sides of blade 201. Cylinders 234 and 236 are located in holes 232 and 237 in piston 37. Each cylinder 234 and 236 has slot accommodating ends of bar seals 221 and 222. Seals 217 222 allow piston 37 to move relative to blade 201 and permit limited tilting o~f blade 201 in slot 202. This enhances seal life and ensures ~O sealing engagement of seal members 208 and 211 on surface 26 of body 24.

Get& A pair of end seals 223 and 226 are located adjacent opposite ends of blade 201. Bow springs 224 and 2i7, shown IC in Figures 13 and 14, bias end srals 223 and 227 into engagement with side plates 27 and 28, as shown in Figure 13. End seals 223 and 226 each have a generally

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CC se semi-circular cross section and are located in semi-circular VVC grooves whereby blade 201 can have limited movement relative V to piston 37 during the orbital movement of piston 37. As O)Z shown in Figure 12, the outer end of seal member 226 has a slot 239 accommodating the end of seal member 211. Seal member 223 has a similar slot (not shown) accommodating the end of seal member 208, This provides continuous side seals for blade 201 engageable with the inside surfaces of end plates 27 and 28.

While there as been shown and described the preferred embodiment of the apparatus for pumping fluids and seal assemblies of the invention, it is understood that X I R-17- I I I changes in the structures materials, and parts may be made by those skilled in the art without departing from the invention. The invention is defined by the following claims, *0e~ 0Q40 at 1 ttt a tat t aa.~ ta a t *1 aat~ t t C Ct C Cr C C C

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Claims (11)

1. An orbital piston pump in which an orbital piston is movable in an eccentric cyclic path within a housing by means of a first eccentric member comprising a rotary drive shaft having an eccentric portion coacting with the piston for moving the piston in its eccentric cyclic path within the housing, and eccentric means rotatably mounted on the housing at a location which is spaced apart from the drive shaft, and having an eccentric portion coacting with the piston for preventing angular movement of the piston as it moves in its eccentric cyclic path within the housing with sealing means carried by the piston contacting a cylindrical inner So* o wall of the housing to define therewith fluid pumping volumes for pumping fluid from an inlet to an outlet, wherein each of the sealing means carried e*9e o 0 by the piston comprises projections slidably received in arcuate slots in o side walls of the housing, each arcuate slot having a radius which is concentric with the cylindrical inner wall but is closer to the axis of the o housing than that inner wall, whereby limited arcuate movement of the sealing means is permitted relative to the housing as the piston moves in its eccentric cyclic path, with the sealing means being restrained against Pradial movement and maintained in sealing engagement with the inner wall by the arcuate slots throughout said movement.

2. A pump according to claim 1, wherein the piston is provided with at least one counterweight to balance it as it moves in it eccentric cyclic path.

3. A pump according to claim 2, wherein the counterweight is received in a transverse bore though the piston on the opposite side of the piston. to the eccentric means.

4. A pump according to any preceding claim, wherein each of the sealing means comprises a blade carrying a seal member at its radially outer end.

A pump according to claim 4, wherein each seal member is biased outwardly from a groove in an end wall of the blade into sliding sealing engagement with the cylindrical inner wall of the housing.

6. A pump according to claim 4 or claim 5, wherein each blade is diagonally divided and is provided with means biasing the blade in the direction of the cylindrical inner wall of the housing and the two divided -pa-ts thereof against the opposite side walls of the housing.

7. A pump according to any of claims 4 to 6, wherein each of the sealing means comprises a pair of identical blades in side-to-side sliding contact, the projections of which are received in the same arcuate slots in the side walls of the housing.

8. A pump according to claim 4 or claim 5, wherein additional scal members are carried by the piston and sealingly engage opposite sides of the blades.

9. A pump according to claim 8, wherein the additional seal members include sealing members slidingly received in grooves in the piston and biased outwardly from the said grooves into sealing contact with the iopposite sides of the blades. S

10. A pump according to any of the preceding claims wherein the eccentric means comprises second and third eccentric members each rotatably mounted on the housing at mutually circumferentially spaced locations which t are radially spaced from the drive shaft, and each having an eccentric I t t portion coacting with the piston for preventing angular movement of the piston as it moves in its eccentric cyclic path within the housing.

11. An orbital piston pump substantially as hereinbefore described with reference to the accompanying drawings. t DATED this TWENTY-NINTH day of AUGUST 1990 Hansen Engine Corporation Patent Attorneys for the Applicant SSPRUSON FERGUSON I A1 KLN/25361 :s] '^1