GB568367A - An improved motor, prime mover or pump - Google Patents

An improved motor, prime mover or pump

Info

Publication number
GB568367A
GB568367A GB1224143A GB1224143A GB568367A GB 568367 A GB568367 A GB 568367A GB 1224143 A GB1224143 A GB 1224143A GB 1224143 A GB1224143 A GB 1224143A GB 568367 A GB568367 A GB 568367A
Authority
GB
United Kingdom
Prior art keywords
chambers
abutment
valves
engine
gases
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
GB1224143A
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.)
Phillips & Powis Aircraft Ltd
Original Assignee
Phillips & Powis Aircraft Ltd
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 Phillips & Powis Aircraft Ltd filed Critical Phillips & Powis Aircraft Ltd
Priority to GB1224143A priority Critical patent/GB568367A/en
Publication of GB568367A publication Critical patent/GB568367A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
    • F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
    • F01C11/002—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle
    • F01C11/004—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of similar working principle and of complementary function, e.g. internal combustion engine with supercharger
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

568,367. Rotary internal-combustion engines. MILES AIRCRAFT, Ltd. (formerly PHILLIPS & POWIS AIRCRAFT, Ltd.), and HEAL, L. C. July 27, 1943, No. 12241. [Class 110 (ii)] The engine may have a single working- chamber 2 with an abutment 7 pressing on the periphery of an eccentric rotor 5, but preferably has two chambers 2, 2a, with a common abutment 7. The rotors are 180‹ out of phase, and geared together for opposite rotation. Inlet and outlet ports 8, 9, are provided, and valves 20, 20a, control fluid flow. Rings, 12 supported on bearings may surround the rotors. The engine may use spark-ignition or compression-ignition. A small clearance may be allowed between a rotor and its cylinder bore. A doubleacting piston 13 is acted upon alternately by gases fired in firing chambers 14, 14a, to supply fuel gas under pressure to the opposite chambers. The semi-rotary sleeve valves control the admission of compressed gas to the firing chambers, and the admission of the gases after firing, to the working-chambers. The fired gases act upon the end of a rod 17 to actuate the piston 13. Gas is admitted by valves 19, 19a, into the cylinder 15. Intercooling may be used between the compression and engine stages. The ends of the abutment may be shaped to improve the sealing effect and may embody roller bearings. The bores of the valves 20, 20a, may be scavenged. The Provisional Specification states that the ends of the abutment may comprise graphite impregnated strips 5, and the inlet valve may be subject to barometric control.
GB1224143A 1943-07-27 1943-07-27 An improved motor, prime mover or pump Expired GB568367A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1224143A GB568367A (en) 1943-07-27 1943-07-27 An improved motor, prime mover or pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1224143A GB568367A (en) 1943-07-27 1943-07-27 An improved motor, prime mover or pump

Publications (1)

Publication Number Publication Date
GB568367A true GB568367A (en) 1945-03-30

Family

ID=10000977

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1224143A Expired GB568367A (en) 1943-07-27 1943-07-27 An improved motor, prime mover or pump

Country Status (1)

Country Link
GB (1) GB568367A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4886024A (en) * 1986-06-24 1989-12-12 Meredith Harold M Rotary piston engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4886024A (en) * 1986-06-24 1989-12-12 Meredith Harold M Rotary piston engine

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