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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
-
- 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
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient 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.
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) |
Families Citing this family (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
Family Cites Families (16)
| 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 |
-
1995
- 1995-07-17 HU HU9502145A patent/HU213242B/hu not_active IP Right Cessation
-
1996
- 1996-07-17 RU RU98102924/06A patent/RU2165537C2/ru active
- 1996-07-17 KR KR1019980700401A patent/KR19990029097A/ko not_active Withdrawn
- 1996-07-17 WO PCT/HU1996/000039 patent/WO1997004226A1/en not_active Ceased
- 1996-07-17 BR BR9609560-1A patent/BR9609560A/pt not_active Application Discontinuation
- 1996-07-17 AU AU63671/96A patent/AU694886B2/en not_active Ceased
- 1996-07-17 US US09/000,332 patent/US6035630A/en not_active Expired - Fee Related
- 1996-07-17 CN CN96196798A patent/CN1196108A/zh active Pending
- 1996-07-17 EP EP96923005A patent/EP0839268A1/en not_active Withdrawn
- 1996-07-17 JP JP9506465A patent/JPH11509293A/ja active Pending
- 1996-07-17 CA CA002227167A patent/CA2227167C/en not_active Expired - Fee Related
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 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| BR9609560A (pt) | Motor giratório de combustão interna e método para operar o motor giratório de combustão interna. | |
| US20050000205A1 (en) | Pulsed combustion engine | |
| US6886325B2 (en) | Pulsed combustion engine | |
| RU99111740A (ru) | Охлаждающее устройство профильной части лопатки газотурбинного двигателя | |
| HUP9904124A2 (hu) | Teljesítménygenerátor és eljárás teljesítmény generálására | |
| US5996336A (en) | Jet engine having radial turbine blades and flow-directing turbine manifolds | |
| US6901738B2 (en) | Pulsed combustion turbine engine | |
| EP1471243A2 (en) | Rotating pulse detonation system for a gas turbine engine | |
| GB1533176A (en) | Gas turbine engine | |
| RU98102924A (ru) | Роторный двигатель внутреннего сгорания | |
| KR890006962A (ko) | 가변용량 배기터빈 과급기 | |
| US4843813A (en) | Compact turbocompressor unit | |
| JP5357151B2 (ja) | ロータリ内燃エンジン | |
| US4003672A (en) | Internal combustion engine having coaxially mounted compressor, combustion chamber, and turbine | |
| RU97121781A (ru) | Уплотнительное устройство газотурбинного двигателя | |
| EP1343950B1 (en) | System to feed cooling air into a gas turbine rotor | |
| EP0493004B1 (en) | Gas generator for a gas turbine | |
| RU2088775C1 (ru) | Газороторный двигатель | |
| US4757682A (en) | Axial flow turbine | |
| EP1435440B1 (en) | Pulsed combustion engine | |
| GB2017222A (en) | Gas Turbine Unit | |
| RU2109969C1 (ru) | Компрессорно-роторно-турбинный двигатель внутреннего сгорания | |
| EP0625629A1 (en) | Turbine | |
| GB2302914A (en) | Mounting exhaust-driven turbochargers on a support housing | |
| RU2014477C1 (ru) | Реактивная турбина |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FF | Decision: intention to grant | ||
| FA11 | Dismissal: dismissal - article 38, par. 2 of industrial property law |