GB1323133A - Rotary engines fluid-operated motors and fluid pumps - Google Patents

Rotary engines fluid-operated motors and fluid pumps

Info

Publication number
GB1323133A
GB1323133A GB4293970A GB4293970A GB1323133A GB 1323133 A GB1323133 A GB 1323133A GB 4293970 A GB4293970 A GB 4293970A GB 4293970 A GB4293970 A GB 4293970A GB 1323133 A GB1323133 A GB 1323133A
Authority
GB
United Kingdom
Prior art keywords
chamber
vanes
rotor
rotor body
stator housing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB4293970A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Pfeiffer R A
Original Assignee
Pfeiffer R A
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Pfeiffer R A filed Critical Pfeiffer R A
Publication of GB1323133A publication Critical patent/GB1323133A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01CROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C1/00Rotary-piston machines or engines
    • F01C1/30Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members
    • F01C1/34Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members
    • F01C1/344Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member
    • F01C1/3448Rotary-piston machines or engines having the characteristics covered by two or more groups F01C1/02, F01C1/08, F01C1/22, F01C1/24 or having the characteristics covered by one of these groups together with some other type of movement between co-operating members having the movement defined in group F01C1/08 or F01C1/22 and relative reciprocation between the co-operating members with vanes reciprocating with respect to the inner member with axially movable vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B2053/005Wankel engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B75/00Other engines
    • F02B75/02Engines characterised by their cycles, e.g. six-stroke
    • F02B2075/022Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle
    • F02B2075/027Engines characterised by their cycles, e.g. six-stroke having less than six strokes per cycle four
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Rotary Pumps (AREA)
  • Transmission Devices (AREA)

Abstract

1323133 Rotary pumps; motors and engines R A PFEIFFER 8 Sept 1970 [8 Sept 1969] 42939/70 Heading F1F A rotary pump, motor or engine comprises a stator housing having end walls whose inner surfaces are in substantially constant axial separation from each other and cylindrical outer and inner walls to form an annular space divided into two separate chambers by a rotor concentrically rotatable within the stator housing, and a plurality of vanes equi-angularly spaced around the rotor to divide each chamber into a plurality of isolated compartments, wherein the rotor or vanes or both are axially displaceable with respect to the stator housing on rotation of the rotor to vary the volumes of the said compartment. In one embodiment described as a four-stroke I.C. engine, a stator housing 10, Figs.1, 2 and 3, comprises end walls 11, 12 having sinusoidal inner surfaces 13, 14 respectively and outer and inner cylindrical walls 18, 15 to form an annular space divided into separate chambers 28, 29 by a rotor body 25 keyed to a shaft 20 concentrically journalled in the stator housing. Vanes 31 to 36 equi-angularly spaced around the rotor body divide the chamber 28 into compartments 40 to 45 and the chamber 29 into compartments 46 to 51 so that as the rotor body rotates a gaseous fuel/air mixture sucked in through inlet passages 62, 63 is in sequence inducted, compressed, ignited and expanded in each compartment and finally exhausted through discharge passages 65, 66. In operation on a two-stroke cycle a gaseous fuel/air mixture inducted through an inlet passage 122, Fig.9, after compression in the first chamber is transferred through a tranfer passage 124 into the second chamber in which it is ignited and expanded and finally exhausted through a discharge passage 126. The outlet from the transfer passage 124 and the discharge passage 126 are disposed sufficiently close together to permit scavenging of the exhaust gases. In another embodiment, a gaseous fuel/air mixture is compressed in one chamber and transferred to the other chamber in which a four-stroke cycle is carried out. To prevent excessive wear on seals 39 between the vane tips and the outer cylindrical wall 18, lateral projections 52, 53 which co-operate with thrust bearings 54 are formed on the vanes. Instead of operating as an I.C. engine the machine may function as a pump with one chamber pumping a gaseous fluid and the other a liquid. In a further embodiment, the rotor body is divided by vanes 156 to 159, Figs.12, 13 diametrically opposite pairs of parts 171, 173 and 172, 174 with parts 171, 173 connected to an inner sleeve 186 splined to a shaft 150 and parts 172, 174 connected to an outer sleeve 189 splined to the inner sleeve. Radial projections 177 on each of the rotor body parts co-operate with a sinusoidal guideway 178 in the outer cylindrical wall 148 to reciprocate the rotor body parts between the end walls which may be either planar whence no reciprocation of the vanes occur or sinusoidal whence both rotor pads and vanes reciprocate. Another embodiment is described in which the rotor body parts are connected to a shaft which is obliquely disposed with respect to the axis of the stator housing. This shaft being connected to an axially directed shaft by level gearing. (For Figures see next page)
GB4293970A 1969-09-08 1970-09-08 Rotary engines fluid-operated motors and fluid pumps Expired GB1323133A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691945388 DE1945388A1 (en) 1969-09-08 1969-09-08 Rotary motor

Publications (1)

Publication Number Publication Date
GB1323133A true GB1323133A (en) 1973-07-11

Family

ID=5744871

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4293970A Expired GB1323133A (en) 1969-09-08 1970-09-08 Rotary engines fluid-operated motors and fluid pumps

Country Status (4)

Country Link
CA (1) CA940831A (en)
DE (1) DE1945388A1 (en)
FR (1) FR2061080A5 (en)
GB (1) GB1323133A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111022179A (en) * 2019-12-05 2020-04-17 曹玉玲 Sliding vane type engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111022179A (en) * 2019-12-05 2020-04-17 曹玉玲 Sliding vane type engine

Also Published As

Publication number Publication date
FR2061080A5 (en) 1971-06-18
DE1945388A1 (en) 1971-03-18
CA940831A (en) 1974-01-29

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees