GB889246A - Improvements relating to rotary engines - Google Patents

Improvements relating to rotary engines

Info

Publication number
GB889246A
GB889246A GB8676/59A GB867659A GB889246A GB 889246 A GB889246 A GB 889246A GB 8676/59 A GB8676/59 A GB 8676/59A GB 867659 A GB867659 A GB 867659A GB 889246 A GB889246 A GB 889246A
Authority
GB
United Kingdom
Prior art keywords
rotors
turbine
compressor
pockets
casings
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
GB8676/59A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB8676/59A priority Critical patent/GB889246A/en
Publication of GB889246A publication Critical patent/GB889246A/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
    • F01C3/00Rotary-piston machines or engines with non-parallel axes of movement of co-operating members
    • F01C3/06Rotary-piston machines or engines with non-parallel axes of movement of co-operating members the axes being arranged otherwise than at an angle of 90 degrees
    • F01C3/08Rotary-piston machines or engines with non-parallel axes of movement of co-operating members the axes being arranged otherwise than at an angle of 90 degrees of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing
    • F01C3/085Rotary-piston machines or engines with non-parallel axes of movement of co-operating members the axes being arranged otherwise than at an angle of 90 degrees of intermeshing-engagement type, i.e. with engagement of co-operating members similar to that of toothed gearing the axes of cooperating members being on the same plane
    • 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
    • F02B2730/00Internal-combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/05Internal-combustion engines with pistons rotating or oscillating with relation to the housing with pistons intermeshing as gear wheels; with helicoidal rotors
    • 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)
  • Supercharger (AREA)

Abstract

889,246. Rotary internal-combustion engines. HARDY, C. C. M. Oct. 12, 1960 [July 12, 1959], No. 8676/59. Class 110 (2). A rotary I.C. engine including a compressor, combustion chamber, and a turbine, comprises a compressor A having a pair of intermeshing screw-like conical rotors 1, 2 positioned in a conical casing 3, to define a plurality of pockets 17 of decreasing volume from the air intake end 9 to the compression chamber 19 and a turbine B having a pair of similar rotors 4, 5 defining with a conical casing 6 a plurality of pockets 18 of increasing volume from the combustion chamber to the outlet 10. Fuel injected into the combustion chamber 19 through injectors 20 mixes with the compressed air and the mixture ignited either by ignition means or by cornpression ignition rapidly expands to rotate the turbine which through a shaft 11 drives the compressor and a power take-off (not shown) to do useful work. A seal may be provided between the casings and the peripheries of the rotors by actual contact, by spring-loaded sealing strips located in rotor grooves or by roughening the peripheral surfaces of the rotors to cause a turbulent boundary layer of air or gas. With the latter method, since there is no mechanical friction between relatively moving parts, the engine can move at high speeds without danger of seizure, overheating or wear and lubrication between the parts is then unnecessary. Moreover manufacturing tolerances may be greater so that the casings and rotors may be manufactured from centrifugal castings or by means of mould powder metallurgy. Also, non- metallic materials such as ceramics or porous or semi-porous refractory materials may be used for these parts. The rotors may be axially adjustable by means of a differential screw and a centrally splined portion of the shaft 11. The casings may have water-cooled passages 21. Alternatively to provide gradually decreasing volume pockets 17 and gradually increasing volume pockets 18, the rotor shafts may be parallel and the pitch of the rotors varied along the lengths of the shafts, or the shafts may be parallel and tapered. A modified construction includes three intermeshing rotors both for the compressor and the turbine.
GB8676/59A 1959-07-12 1959-07-12 Improvements relating to rotary engines Expired GB889246A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8676/59A GB889246A (en) 1959-07-12 1959-07-12 Improvements relating to rotary engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8676/59A GB889246A (en) 1959-07-12 1959-07-12 Improvements relating to rotary engines

Publications (1)

Publication Number Publication Date
GB889246A true GB889246A (en) 1962-02-14

Family

ID=9857070

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8676/59A Expired GB889246A (en) 1959-07-12 1959-07-12 Improvements relating to rotary engines

Country Status (1)

Country Link
GB (1) GB889246A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4782802A (en) * 1987-01-20 1988-11-08 General Motors Corporation Positive displacement rotary mechanism
US4841930A (en) * 1987-01-20 1989-06-27 General Motors Corporation Positive displacement rotary mechanism
US4860705A (en) * 1987-01-20 1989-08-29 General Motors Corporation Positive displacement rotary mechanism
US4877385A (en) * 1987-01-20 1989-10-31 General Motors Corporation Positive displacement rotary mechanism
US6257195B1 (en) * 2000-02-14 2001-07-10 Arthur Vanmoor Internal combustion engine with substantially continuous fuel feed and power output
CZ304109B6 (en) * 2005-12-19 2013-10-30 Bríza@Zdenek Internal combustion engine
WO2017008037A1 (en) * 2015-07-08 2017-01-12 Freeman Bret Fixed displacement turbine engine

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4782802A (en) * 1987-01-20 1988-11-08 General Motors Corporation Positive displacement rotary mechanism
US4841930A (en) * 1987-01-20 1989-06-27 General Motors Corporation Positive displacement rotary mechanism
US4860705A (en) * 1987-01-20 1989-08-29 General Motors Corporation Positive displacement rotary mechanism
US4877385A (en) * 1987-01-20 1989-10-31 General Motors Corporation Positive displacement rotary mechanism
US6530365B2 (en) 1999-05-18 2003-03-11 Arthur Vanmoor Fluid displacement pump with backpressure stop
US6257195B1 (en) * 2000-02-14 2001-07-10 Arthur Vanmoor Internal combustion engine with substantially continuous fuel feed and power output
CZ304109B6 (en) * 2005-12-19 2013-10-30 Bríza@Zdenek Internal combustion engine
WO2017008037A1 (en) * 2015-07-08 2017-01-12 Freeman Bret Fixed displacement turbine engine
US10138731B2 (en) 2015-07-08 2018-11-27 Bret Freeman Fixed displacement turbine engine

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