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BR9609560A - Motor giratório de combustão interna e método para operar o motor giratório de combustão interna. - Google Patents

Motor giratório de combustão interna e método para operar o motor giratório de combustão interna.

Info

Publication number
BR9609560A
BR9609560A BR9609560-1A BR9609560A BR9609560A BR 9609560 A BR9609560 A BR 9609560A BR 9609560 A BR9609560 A BR 9609560A BR 9609560 A BR9609560 A BR 9609560A
Authority
BR
Brazil
Prior art keywords
rotor
combustion
stator
internal combustion
expansion
Prior art date
Application number
BR9609560-1A
Other languages
English (en)
Inventor
Soos Sandor
Original Assignee
Soos Sandor Hungaro
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 Soos Sandor Hungaro filed Critical Soos Sandor Hungaro
Publication of BR9609560A publication Critical patent/BR9609560A/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • 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
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Valve Device For Special Equipments (AREA)
  • Pulleys (AREA)

Abstract

"MOTOR GIRATóRIO DE COMBUSTãO INTERNA E MéTODO PARA OPERAR O MOTOR GIRATóRIO DE COMBUSTãO INTERNA", dito motor compreendendo um estator (1) e um rotor (2) que estão dispostos de modo que a circunferência interna do estator (1), pelo menos em certos setores circunferentes predeterminados, circunda vedavelmente o rotor (2). O estator (1) é dotado de pelo menos duas câmaras de combustão. Cada câmara de combustão tem um abertura de saída de descarga tangencialmente na direção do rotor (2) e pelo menos uma entrada de combustível (15) através da qual oxigênio e ar e combustível, em quantidade predeterminadas, de modo a formar uma mistura de combustível, podem ser injetadas na câmara de combustão em predeterminados intervalos. O rotor (2) tem segmentos de anel externos (23) conectados a um eixo principal (21) por uma pluralidade de raios (22). Os segmentos de anel (23) são ditados de um interior de artéria (4) através do qual uma corrente contínua de ar ambiente passa através do rotor (2) na direção axial durante operação, e uma pluralidade de canais de expansão, adaptados para receber um jato de gás de gases de combustão sob alta pressão descarregado das câmaras de combustão através das saídas de descarga, quando as entradas dos canais de expansão estiverem temporária e sequencialmente defronte às saídas de descarga durante o movimento giratório relativo do rotor (2) em relação ao estator (1). O rotor (2) consiste de pelo menos dois segmentos de rotos adjacentes (20). Os canais de expansão em cada um dos segmentos do rotor fora (20) formam pelo menos um grupo de canais de expansão de artéria capaz de girar continuamente o rotor (2), convertendo a energia dos gases de combustão em toque de acionamento exercido na forma de impulsos tangenciais no segmento de anel (23). Cada canal de expansão provê uma conexão direta para os gases de combustão a partir das saídas de descarga das câmaras de combustão na direção do interior (4) do segmento do rotor (20), em intervalos quando as entradas periféricas dos canais de expansão estiverem defronte às saídas de descarga das câmaras de combustão.
BR9609560-1A 1995-07-17 1996-07-17 Motor giratório de combustão interna e método para operar o motor giratório de combustão interna. BR9609560A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
HU9502145A HU213242B (en) 1995-07-17 1995-07-17 Adiabatic, tangetial driving hydrogen engine
PCT/HU1996/000039 WO1997004226A1 (en) 1995-07-17 1996-07-17 Internal combustion rotary engine

Publications (1)

Publication Number Publication Date
BR9609560A true BR9609560A (pt) 1999-12-14

Family

ID=10987049

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9609560-1A BR9609560A (pt) 1995-07-17 1996-07-17 Motor giratório de combustão interna e método para operar o motor giratório de combustão interna.

Country Status (11)

Country Link
US (1) US6035630A (pt)
EP (1) EP0839268A1 (pt)
JP (1) JPH11509293A (pt)
KR (1) KR19990029097A (pt)
CN (1) CN1196108A (pt)
AU (1) AU694886B2 (pt)
BR (1) BR9609560A (pt)
CA (1) CA2227167C (pt)
HU (1) HU213242B (pt)
RU (1) RU2165537C2 (pt)
WO (1) WO1997004226A1 (pt)

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CN1124404C (zh) * 1999-09-03 2003-10-15 张胜利 反动式发动机
KR100334356B1 (ko) * 1999-11-30 2002-04-25 맹혁재 고압유체를 이용한 밀폐형 회전임펠러식 엔진
KR100365908B1 (ko) * 2000-05-18 2002-12-31 권병규 터빈엔진
US6606973B2 (en) 2001-05-23 2003-08-19 Cordell R. Moe Rotary engine
US6467450B1 (en) 2001-06-12 2002-10-22 Paguer, Inc. Radial combustion motor
RU2281408C2 (ru) * 2002-09-05 2006-08-10 Владимир Спартакович Самар Двухроторный двигатель внутреннего сгорания
RU2278287C2 (ru) * 2004-01-05 2006-06-20 Владимир Спартакович Самар Двухроторный двигатель внутреннего сгорания
US20060207546A1 (en) * 2005-03-18 2006-09-21 Bechtel Paul Y Engine system
CA2672396A1 (en) * 2005-12-13 2007-06-21 Richard Alan Haase Water combustion technology - the haase cycle
US7963096B2 (en) * 2006-11-02 2011-06-21 Vanholstyn Alex Reflective pulse rotary engine
RU2365763C1 (ru) * 2008-03-07 2009-08-27 Андрей Алексеевич Кровяков Вихревая турбина внутреннего сгорания
US20100251992A1 (en) * 2009-04-06 2010-10-07 Davis Frank S Radial pulsed rotary internal combustion engine
US20120024403A1 (en) * 2010-07-30 2012-02-02 Hamilton Sundstrand Corporation Inorganic coke resistant coatings to prevent aircraft fuel system fouling
US9970294B2 (en) * 2012-07-09 2018-05-15 Isaac Erik Anderson Shockwave rotor detonation (omni-engine, ubiquitous X engine) multipurpose engine
US8839599B1 (en) * 2013-10-07 2014-09-23 Juan Pedro Mesa, Jr. Axial combustion engine
CN104564423A (zh) * 2013-10-21 2015-04-29 王秋林 径流式冲压发动机
WO2015122971A1 (en) * 2013-12-31 2015-08-20 Bracalente Angelo Internal combustion rotary engine
CN106014616A (zh) * 2015-01-18 2016-10-12 吴小平 季差绝热式转子内燃机技术及所制造的内燃机
CN112360415B (zh) * 2020-11-10 2021-11-19 中国科学院武汉岩土力学研究所 一种旋转式压力脉冲转换器以及水力压裂注液装置
CN113006934B (zh) * 2021-03-12 2022-08-02 北京工业大学 一种点燃式柴油转子机及其控制方法

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Publication number Priority date Publication date Assignee Title
US1388371A (en) * 1921-08-23 Xatherine m
US547414A (en) * 1895-10-08 Gas-engine
US820838A (en) * 1905-03-25 1906-05-15 Wandel & Co Metalltuch Fabrick Means for operating picker-drums.
FR422371A (fr) * 1910-11-10 1911-03-20 Jean Jacques Heilmann Turbine à explosions à action directe
FR425945A (fr) * 1911-02-11 1911-06-23 Dauxin Soc Turbine à explosions
US1174439A (en) * 1914-03-03 1916-03-07 O D Jones Gas-turbine.
US1200133A (en) * 1915-06-17 1916-10-03 Eugene A Pharr Polyimpulse gas-engine.
CH121627A (de) * 1926-02-08 1927-07-16 V Keller Charles Explosionsturbine.
US2320391A (en) * 1938-09-06 1943-06-01 George H Wakefield Explosion turbine motor
FR1156955A (fr) * 1956-07-17 1958-05-23 Moteur rotatif à explosion sans embiellage
US3956888A (en) * 1975-01-07 1976-05-18 Thomas Sanfran Miyada Coaxial rotary engine
CA1042672A (en) * 1977-12-07 1978-11-21 Ignacy Wanat Internal combustion elastic fluid generator and turbine combination
DE2757236C3 (de) * 1977-12-22 1982-02-25 Dr.Ing.H.C. F. Porsche Ag, 7000 Stuttgart Antriebsaggregat, insbesondere für Kraftfahrzeuge
US4365472A (en) * 1980-06-25 1982-12-28 Saburo Ogata Turbine-type internal-combustion engine
GB2169967A (en) * 1985-01-22 1986-07-23 Piers Anthony Benedict Lee Radial flow gas turbine engines
DE3826533A1 (de) * 1988-08-04 1989-04-20 Helmut Dipl Ing Samulowitz Rotierende verbrennungskraftmaschine

Also Published As

Publication number Publication date
CA2227167A1 (en) 1997-02-06
WO1997004226A1 (en) 1997-02-06
EP0839268A1 (en) 1998-05-06
MX9800502A (es) 1998-08-30
US6035630A (en) 2000-03-14
CN1196108A (zh) 1998-10-14
AU694886B2 (en) 1998-07-30
KR19990029097A (ko) 1999-04-15
HU213242B (en) 1997-05-28
RU2165537C2 (ru) 2001-04-20
AU6367196A (en) 1997-02-18
HU9502145D0 (en) 1995-09-28
JPH11509293A (ja) 1999-08-17
CA2227167C (en) 2001-10-02

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Legal Events

Date Code Title Description
FF Decision: intention to grant
FA11 Dismissal: dismissal - article 38, par. 2 of industrial property law