WO2007142551A1 - Moteur rotatif à combustion interne et son cycle de travail - Google Patents

Moteur rotatif à combustion interne et son cycle de travail Download PDF

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Publication number
WO2007142551A1
WO2007142551A1 PCT/RU2007/000232 RU2007000232W WO2007142551A1 WO 2007142551 A1 WO2007142551 A1 WO 2007142551A1 RU 2007000232 W RU2007000232 W RU 2007000232W WO 2007142551 A1 WO2007142551 A1 WO 2007142551A1
Authority
WO
WIPO (PCT)
Prior art keywords
compression
conversion
blade
chamber
internal combustion
Prior art date
Application number
PCT/RU2007/000232
Other languages
English (en)
Russian (ru)
Inventor
Anatoly Vladimirovich Karasyov
Original Assignee
Anatoly Vladimirovich Karasyov
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 Anatoly Vladimirovich Karasyov filed Critical Anatoly Vladimirovich Karasyov
Priority to EA200801273A priority Critical patent/EA012459B1/ru
Publication of WO2007142551A1 publication Critical patent/WO2007142551A1/fr

Links

Classifications

    • 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
    • F02B53/02—Methods of operating
    • 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
    • F01C1/3448—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 with axially movable vanes
    • 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

Definitions

  • the objective of the present invention is to increase the force acting on the blade, providing its reciprocating motion, while reducing pressure in the contact zone of the pusher and
  • the rotary internal combustion engine (Figs. 1-4) comprises a housing 1 with side covers 2, in which a disk 3 and an annular 4 structural units are placed with the possibility of mutual rotation.
  • the disk 3 and ring 4 structural units are highlighted with dashed contours, while the circuits themselves are conditional and the affiliation of a particular part to the corresponding structural unit 3 or 4 is defined below in the description.
  • the locking mechanism 22 (23) and the spacer 25 with which this mechanism is connected, and the combustion chamber 10 should be assigned to the device for moving the blades 8 (9) and to the combustion chamber 10, from the side opposite to the working chambers 17 (18) adjacent cylinder 38 (53) with a piston 39 (54) and a gas reservoir 40 (55), which are separated by an exhaust valve 42 (50), while the combustion chamber 10 and the gas reservoir 40 (55) are interconnected by an intake valve 41 (49).

Landscapes

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

Abstract

Dans le moteur rotatif à combustion interne de l'invention qui comprend des unités structurelles en forme de disque et en forme d'anneau, les unités étant disposées dans un boîtier (1) de manière à pouvoir faire des rotations l'une par rapport à l'autre, chaque chambre de combustion (10) située dans un disque (6) est entourée des deux côtés par des pales de compression et de conversion, prétensionnées par ressort, les pales étant disposées dans le logement du disque. Des dispositifs d'arrêt (22) disposés dans le boîtier (1) fixent les pales de conversion en position prédéterminée sur toute la longueur des chambres de compression et laissent libres les pales de compression qui, lors du mouvement dans une direction prédéterminée, compriment le mélange carburant /air dans des chambres de combustion correspondantes (10). Dans les chambres de conversion, montées en séquence dans le sens du mouvement, les dispositifs d'arrêt (22) disposés sur toute leur longueur fixent les pales de compression et laissent libres les pales de compression sur lesquelles fait pression le mélange allumé carburant / air.
PCT/RU2007/000232 2006-06-01 2007-05-04 Moteur rotatif à combustion interne et son cycle de travail WO2007142551A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EA200801273A EA012459B1 (ru) 2006-06-01 2007-05-04 Роторный двигатель внутреннего сгорания и его рабочий цикл

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2006120326/06A RU2307255C1 (ru) 2006-06-01 2006-06-01 Способ осуществления рабочего цикла роторного двигателя внутреннего сгорания и устройство для его реализации
RU2006120326 2006-06-01

Publications (1)

Publication Number Publication Date
WO2007142551A1 true WO2007142551A1 (fr) 2007-12-13

Family

ID=38801703

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2007/000232 WO2007142551A1 (fr) 2006-06-01 2007-05-04 Moteur rotatif à combustion interne et son cycle de travail

Country Status (3)

Country Link
EA (1) EA012459B1 (fr)
RU (1) RU2307255C1 (fr)
WO (1) WO2007142551A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009054746A1 (fr) * 2007-10-22 2009-04-30 Anatoly Vladimirovich Karasyov Moteur rotatif à combustion interne

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3942484A (en) * 1973-09-12 1976-03-09 Pile Delbert W Impeller type engine
GB2183732A (en) * 1985-12-06 1987-06-10 Charles Sejbl Sinusoidal pump/motor
US5429084A (en) * 1994-02-25 1995-07-04 Sky Technologies, Inc. Axial vane rotary device and sealing system therefor
RU2148721C1 (ru) * 1998-12-11 2000-05-10 Козлов Георгий Леонидович Роторный аксиальный двигатель

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3942484A (en) * 1973-09-12 1976-03-09 Pile Delbert W Impeller type engine
GB2183732A (en) * 1985-12-06 1987-06-10 Charles Sejbl Sinusoidal pump/motor
US5429084A (en) * 1994-02-25 1995-07-04 Sky Technologies, Inc. Axial vane rotary device and sealing system therefor
RU2148721C1 (ru) * 1998-12-11 2000-05-10 Козлов Георгий Леонидович Роторный аксиальный двигатель

Also Published As

Publication number Publication date
EA200801273A1 (ru) 2008-08-29
EA012459B1 (ru) 2009-10-30
RU2307255C1 (ru) 2007-09-27

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