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US2152564A - Rotary fluid motor - Google Patents

Rotary fluid motor
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Publication number
US2152564A
US2152564AUS160924AUS16092437AUS2152564AUS 2152564 AUS2152564 AUS 2152564AUS 160924 AUS160924 AUS 160924AUS 16092437 AUS16092437 AUS 16092437AUS 2152564 AUS2152564 AUS 2152564A
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Prior art keywords
abutment
cylinder
piston
housing
shaft
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US160924A
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Mart C Perkins
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March 28, 1939. M. c, PERKINS ROTARY FLUID MOTOR Filed Aug. 25, 1937 3 Sheets-Shes;
March 28, 1939. c PE I 2,152,564
ROTARY FLUID MOTOR Filed Aug. 25, 1937 3 Sheets-Sheet 2 March 28, 1939. c PERK|NS 2,152,564
ROTARY FLU ID MOTOR Fild Aug. 25, 1937 3 Sheets-Sheet 3 52 4 32 m 4 Z; r /0 3'5 /0 4w '""Zb 2 '";'7-
.3 a 44 3 42 4/ 46 E 44 Z9 Z4 45' 37 1% 5a 37 Z 95 E /z 3" v 51 (to: M; 5'
Patented Mar. 28, 1939 UNITED STATES PATENT OFFICE 2,152,564 ROTARY FLUID Moron Mart C. Perkins, Casper, Wyo.
Application August 25, 1937, Serial No. 160,924
2 Claims.
all within a unitary housing. Other objects and advantages of this invention will appear in the following description taken in connection with the accompanying drawings.
Figure 1 is a vertical cross section showing the arrangement of the cylinders and abutments. Figure 2 is a fragmentary end elevation of one end of the engine. Figure 2 is a fragmentary end elevation of the opposite end of the engine. Figure 3 is a vertical section taken substantially through the center of the engine. Figure 4 is a transverse cross section of the piston corresponding to a section on line 44 of Figure 1. Figure 5 is an enlarged View showing the piston in greater detail. Figure 6 is a view of the power fluid valve viewed on the line 66 of Figure 7. Figure 7 is an enlarged view substantially on the line 1-1 of Figure 1. Figure 8 is a detail of the lubricating system.
The engine comprises a housing In having a toroidal cylinder H in the inner circumference l2 of which is rotatably mounted a ring gear orrotor 13. The ring gear or rotor I3 carries upon its periphery a plurality of pistons or vanes 14. At spaced points about the cylinder are located rotary abutments l5 each of which is recessed as at It. The remainder of the periphery of each abutment is provided with a plurality of gear teeth I! which mesh with gear teeth l8 of the ring gear. In operation the ring gear rotates in a counterclockwise direction as viewed in Figure 1 carrying with it the pistons 14 which are forced around through the toroidal cylinder by the power fluid and which nest successively within or pass through the respective recesses [6 of each abutment during the rotation of the engine.
Steam, compressed air or some other power fluid is admitted to the power fluid inlet box Is by means of theinlet ports 20. Thedisc valve 2| rotates about itsshaft 22 to an appropriate point where the elongatedarcuate port 23 Places the steam box or power fluid supply means l9 in communication with theport 24, which in turn is in communication with thecylinder 25 in which the abutment rotates throughrecess 16 at the time the piston I4 is passing out of the recess I6. Steam or other power fluid enters the cylinder through the space provided by therecess 16 of the rotary abutment and continues to fill up the space in the cylinder limited by the abutment at one end and thetrailing face 26 of the piston [4 at the other end. The pitch circles of the gear teeth H on the abutment and I8 on the ring gear are so arranged that the pistons will successively engage the recess of each abutment. The continued movement of the abutment in a clockwise direction cuts oil the admission of steam and the expansion of the steam in the cylinder ll moves the piston l4 away from the abutment A toward the abutment B. When the piston clears theexhaust port 21, the expanded steam is re leased from the cylinder thereby allowing the piston to pass through the recess 5 of abutment B so that the cylinder will then receive a new supply of steam from the corresponding ports of abutment B and the piston will again be forced in a counterclockwise direction towards the abutment C during which the cycle of operation is repeated. This same action takes. place behind each piston and between each piston and abutment which it has just passed. In this manner a continuous series of power impulses are applied to the pistons which transmit the power in turn to the ring gear I3, which in turn transmits the power impulses toshaft 28 by means of akeyed driving connection 29. The number of teeth It on the ring gear is properly coordinated with the number of teeth on the periphery of the rotary abutment so that each piston will ride through the abutment recess as it passes the abutment. Theopposed faces 26 and 30 of each piston are arranged with a contour corresponding to a tooth curve so that an accurate intermeshing of the piston and the abutment recess will be obtained.
The housing is preferably made in the form of opposed segments 3| and 32 providing the cylinder space for the rotary abutment and a segmental portion of the toroidal cylinder for the pistons. These portions of the housing are bolted together by appropriate securing means 33 and to that side portion of the housing in which the rotary abutment is mounted is secured bymeans 34 the power fluid supply means l9. For the purpose of simplifying and improving the engine thesteam valve 2| and the abutment I5 are keyed to ashaft 22 at thepoints 35 and 36 respectively. In this manner the steam valve cooperates with the abutment to provide for the necessary inlet of the power medium. To operate theabutments oil grooves 65, 66 and 81.
tions forming anannular slot 42 in which is positioned a piston ring 43. The piston is assembled with the piston pin 44 projecting through theside walls 45 of the piston but terminating interiorly of the ring as at 46 in Figure 4, the pin passing through the opening 41 of the arm 31' giving the driving connection to the ring gear.
When the elements have all been assembled, they are appropriately secured together by means of arivet 48.
In an engine of this type it is obviously necessary to provide appropriate lubrication and this is accomplished by a system now to be described. The entire housing of the engine is mounted upon supports 49 and the central portion of the housing is sealed by end members 58 and 5|. These members provide appropriate bearingportions 52 and 53 for the shaft and are in turn reinforced by a series of radial ribs 54 and 55. These members also enclose the ring gear within the housing. On the left end member 5| an annular flange 56 together with the sealing member 5'! provides an,
oil reservoir and an appropriate housing for the reciprocating lubricating pump 58. The bottom of this housing contains a body of lubricant 59 which is taken into the pump 58 by means of its inlet 60 and forced into the bearing system by the tube 6|. This latter tube is in communication with an annular oil groove 62 and shaft and by means of radial passages 63 is placed in communication with anaxially extending oil passage 84. The latter communicates with the various The oil groove 66 has further communication with an oil passage 61 passing through one or more of thespokes 68 of the ring gear and is placed in communication with the friction surfaces between the abutment and the housing at thepoint 1|. This alsosupplies lubricant to the intermeshing gear teeth in the neighborhood of thepoint 12. Lubrication for the bearings, rotary abutment and steam valve is provided by means of a series oftubes 13 carrying oil from the oil channel 61 to the center of theshaft 22. The latter shaft contains a central bore which is in communication with thebearings 15 and 16. It will be readily appreciated that the pump 58 maintains a continuous supply of lubricant as a result of the rotation ofshaft 28. This is accomplished by the cam 71 which is. keyed to theshaft 28 by means of thekey 18 which is either a direct connection from a cam wheel or which may be a connection by means of a collar which in turn carries the cam. The rotation of the cam TI forces the plunger in a radial direction against the opposition of the spring 8| and accomplishes the necessary operation of the pump 58.
The supply of oil in the system may be maintained by occasionally replenishing it through port .82. Loss of oil along the shaft is avoided bypackings 83 secured in place by the packing rings 84. Theplate 50 is secured to the housing by a series ofbolts 85 and the plate 5| is secured to the housing by a. series ofbolts 86. Thecover member 57 is secured in place to seal the reservoir by a series ofbolts 81.
The abutments may be provided with counterbalance means such as bore holes if necessary to smooth out the rotary motion. To make the operation of the engine moreeflicient bleed lines 88 to 9|. are placed about a portion of the periphery of the abutment so that any power fluid.
trapped in the pocket l6 can escape and be useful' on the piston. This cannot occur by thetooth groove 92. The gear member I3 is provided with laterally projectingcylindrical shoulders 94 on opposite sides thereof which rotatably engage in a cylindrical bore 95-and the teeth l8 of the gear l3 engage in anannular slot 93 provided on the inner side of the cylinder Although a preferred embodiment of this inventionv has been shown and described, variations coming within the true spirit and scope of the invention are to be determined by the appended claims.
What I. claim is:
1. A rotary engine comprising a housing having a ring-shaped cylinder therein provided with an annular slot on the inner side thereof, a shaft disposed axially of said: cylinder, a gear secured to said shaft Within said housing having the teeth thereof engaging within said annular slot, a plurality of circumferentially spaced apart pistons secured to said gear and engaging within said cylinder, said housing having a plurality of circumferentially spaced apart abutment chambers communicating with saidcylinder, anabutment shaft journalled through. each chamber, an annular abutment in, each chamber fixed to an abutment. shaft and projecting interiorly of said cylinder, each abutment having a peripheral recess to receive a piston, a valve. chamber extending laterallyof andv communicating with each abutment chamber, a rotary inlet valvein each valve. chamber fixed toan abutment shaft, gear teeth carried by each abutment engaging said first gear, said cylinder having .anexhaust port between each abutment chamber.
2. Arotary engine comprising a housing having a ring-shaped cylinder therein provided with r an annular slot on. the inner sidethereof, a shaft disposed, axially of said cylinder, a gear secured to said shaft within said housing engaging in the slot thereof, laterally projecting cylindrical shoulders carried by said gear, a plurality of circumferentiallyspaced apart pistons secured to said gear and engaging within saidcylinder, said housing having a plurality of circumferentially spaced apart abutmentv chamber-sv communicating with said cylinder, an abutment shaft journalled through each chamber, anannular abutment in each chamber fixed tov an abutment shaft and projecting interiorlyof said cylinder, each abutment having a peripheral recess to receive a piston, a valve chamber extending laterally of and communicating with each abutment chamber, a rotary inletvalve in each valve chamber fixed to an abutment shaft, gear teeth carried by each abutment engaging said first gear, said cylinder having an exhaust port between each abutment chamber.
MART C. PERKINS.
US160924A1937-08-251937-08-25Rotary fluid motorExpired - LifetimeUS2152564A (en)

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
EP0023529A3 (en)*1979-08-071981-05-20Ernst HenkelRotary piston machine of the external axis type
WO1998012419A3 (en)*1996-09-191998-05-28Arthur VanmoorRadial vane rotary internal combustion engine
US6003486A (en)*1995-09-191999-12-21Moerkerken; Arthur VanRadial vane rotary internal combustion engine
US20040231635A1 (en)*2003-05-192004-11-25Gehman Grant G.Rotary engine
US20040261757A1 (en)*2003-06-302004-12-30Nathan Avraham MordehayVariable-volume rotary kinematic machine
US20080251047A1 (en)*2005-08-032008-10-16Bowley Ryan TToroidal engine method and apparatus
USRE41373E1 (en)*2003-05-192010-06-15Gehman Grant GRotary engine
US20140056745A1 (en)*2012-08-232014-02-27Mallen Research Limited PartnershipFixed-vane positive displacement rotary devices
US20170002730A1 (en)*2014-01-282017-01-05Imre NagyCombustion engine without compression and method
US9638035B2 (en)2011-11-172017-05-02Tripile E Power Ltd.Rotary engine and process
US9664048B2 (en)2012-08-232017-05-30Mallen Research Limited PartnershipPositive displacement rotary devices with uniform tolerances
US9664047B2 (en)2012-08-232017-05-30Mallen Research Limited PartnershipPositive displacement rotary devices with uniquely configured voids
US11066986B2 (en)*2018-03-132021-07-20Aleksei Mihailovich ORELInternal combustion engine
WO2024142064A1 (en)*2022-12-292024-07-04Coool.Energy LtdRotary compressor and expander

Cited By (21)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
EP0023529A3 (en)*1979-08-071981-05-20Ernst HenkelRotary piston machine of the external axis type
US6003486A (en)*1995-09-191999-12-21Moerkerken; Arthur VanRadial vane rotary internal combustion engine
US6550443B1 (en)1995-09-192003-04-22Arthur VanmoorRadial vane rotary internal combustion engine
WO1998012419A3 (en)*1996-09-191998-05-28Arthur VanmoorRadial vane rotary internal combustion engine
US20040231635A1 (en)*2003-05-192004-11-25Gehman Grant G.Rotary engine
US6935300B2 (en)*2003-05-192005-08-30Grant G. GehmanRotary engine
USRE41373E1 (en)*2003-05-192010-06-15Gehman Grant GRotary engine
US20040261757A1 (en)*2003-06-302004-12-30Nathan Avraham MordehayVariable-volume rotary kinematic machine
US20080251047A1 (en)*2005-08-032008-10-16Bowley Ryan TToroidal engine method and apparatus
US7621255B2 (en)*2005-08-032009-11-24E3P Technologies, Inc.Toroidal engine method and apparatus
US9638035B2 (en)2011-11-172017-05-02Tripile E Power Ltd.Rotary engine and process
US20140056745A1 (en)*2012-08-232014-02-27Mallen Research Limited PartnershipFixed-vane positive displacement rotary devices
US8956134B2 (en)*2012-08-232015-02-17Mallen Research LimitedFixed-vane positive displacement rotary devices
US9664048B2 (en)2012-08-232017-05-30Mallen Research Limited PartnershipPositive displacement rotary devices with uniform tolerances
US9664047B2 (en)2012-08-232017-05-30Mallen Research Limited PartnershipPositive displacement rotary devices with uniquely configured voids
US10138730B2 (en)2012-08-232018-11-27Mallen Research Limited PartnershipPositive displacement rotary devices with uniform tolerances
US11111788B2 (en)2012-08-232021-09-07Mallen Research Limited PartnershipPositive displacement rotary devices
US20170002730A1 (en)*2014-01-282017-01-05Imre NagyCombustion engine without compression and method
US10047668B2 (en)*2014-01-282018-08-14Imre NagyCombustion engine without compression and method
US11066986B2 (en)*2018-03-132021-07-20Aleksei Mihailovich ORELInternal combustion engine
WO2024142064A1 (en)*2022-12-292024-07-04Coool.Energy LtdRotary compressor and expander

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