GB381727A - Rotary engine or pump - Google Patents

Rotary engine or pump

Info

Publication number
GB381727A
GB381727A GB28910/31A GB2891031A GB381727A GB 381727 A GB381727 A GB 381727A GB 28910/31 A GB28910/31 A GB 28910/31A GB 2891031 A GB2891031 A GB 2891031A GB 381727 A GB381727 A GB 381727A
Authority
GB
United Kingdom
Prior art keywords
vanes
rotor
bars
working chamber
point
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
GB28910/31A
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 GB28910/31A priority Critical patent/GB381727A/en
Publication of GB381727A publication Critical patent/GB381727A/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
    • F01C1/00—Rotary-piston machines or engines
    • F01C1/30—Rotary-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
    • F01C1/34—Rotary-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
    • F01C1/344—Rotary-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
    • F01C1/3446—Rotary-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 the inner and outer member being in contact along more than one line or surface
    • 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
    • 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
    • F02B2730/00—Internal-combustion engines with pistons rotating or oscillating with relation to the housing
    • F02B2730/01—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber
    • F02B2730/012—Internal-combustion engines with pistons rotating or oscillating with relation to the housing with one or more pistons in the form of a disk or rotor rotating with relation to the housing; with annular working chamber with vanes sliding in the piston
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Details And Applications Of Rotary Liquid Pumps (AREA)

Abstract

381,727. Rotary engines. HAPKINS, D. N., 109, South Carondelet Street, Los Angeles, U.S.A. Oct. 17, 1931, No. 28910. [Class 110 (ii).] In an internal-combustion engine of the type illustrated two abutments 39, 40 are formed in the casing liner 60, and during the suction stroke alternate vanes 271 are held in the retracted position so that the amount of fuel contained in 90‹ of the working chamber is compressed into the combustion chamber 56 and one of the pockets 55 scooped out of the rotor R. The vanes 27, 27<1> have guide-pins 27c surrounded by compression springs 29, and legs 27b which in the vanes 27<1> are fitted with rollers 47 which co-operate with cam tracks 50 extending over the arc of 180‹ covering the suction stroke. L-shaped packing-bars 33 fit in two slots in each vane, one of each bearing against a side wall of the working chamber. Sinusoidal springs 34 are fitted under the bars 33. The inlet port 41 extends to a point 41a midway between the abutment 40 and the midsuction stroke point 42. The engine is lubricated by means of a hollow shaft having radial holes communicating with holes 26 in the rotor. The number of vanes may vary.
GB28910/31A 1931-10-17 1931-10-17 Rotary engine or pump Expired GB381727A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB28910/31A GB381727A (en) 1931-10-17 1931-10-17 Rotary engine or pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB28910/31A GB381727A (en) 1931-10-17 1931-10-17 Rotary engine or pump

Publications (1)

Publication Number Publication Date
GB381727A true GB381727A (en) 1932-10-13

Family

ID=10283157

Family Applications (1)

Application Number Title Priority Date Filing Date
GB28910/31A Expired GB381727A (en) 1931-10-17 1931-10-17 Rotary engine or pump

Country Status (1)

Country Link
GB (1) GB381727A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2731683A1 (en) * 1976-07-14 1978-01-19 Kunieda GAS SEAL

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2731683A1 (en) * 1976-07-14 1978-01-19 Kunieda GAS SEAL

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