BR0108902A - Motor de carga direcionado - Google Patents
Motor de carga direcionadoInfo
- Publication number
- BR0108902A BR0108902A BR0108902-1A BR0108902A BR0108902A BR 0108902 A BR0108902 A BR 0108902A BR 0108902 A BR0108902 A BR 0108902A BR 0108902 A BR0108902 A BR 0108902A
- Authority
- BR
- Brazil
- Prior art keywords
- apex
- throat
- produces
- combustion chamber
- applications
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/292—Three-dimensional machined; miscellaneous tapered
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/712—Shape curved concave
-
- 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)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Portable Nailing Machines And Staplers (AREA)
Abstract
"MOTOR DE CARGA DIRECIONADO." A máquina de carga direcionada inclui uma câmara de combustão anular (3) formada pelo acoplamento dos alojamentos interno (1) e externo (2). A central através de um orifício no alojamento permite que os gases de exaustão saiam. O alojamento externo compreende um disco de contorno geralmente com uma cavidade de depressão interna cónica e através dos orifícios para a inserção do combustível e da ignição. A câmara de combustão é preferivelmente do formato cónico-afilado, mais largo na base, e diminui gradualmente na área da seção transversal quando esta alcança o ápice. Esta construção forma um ponto de base circular ou garganta para o ápice que produz uma zona de compressão primária. A zona de compressão secundária é criada no ápice se o alojamento externo, apenas além da garganta, produz os gases hipersónicos como geralmente opostos aos fluxos de exaustão que colidem e são forçados a sair através do orifício no alojamento interno. O motor de carga direcionado pode ser usado em uma variedade de aplicações, incluindo como um dispositivo de propulsão direto pulsado, como um acionador de turbina, ou em uma ampla cadeia de ferramentas e aplicações.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/517,130 US6430919B1 (en) | 2000-03-02 | 2000-03-02 | Shaped charged engine |
PCT/US2001/006617 WO2001065103A1 (en) | 2000-03-02 | 2001-03-02 | Shaped charge engine |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0108902A true BR0108902A (pt) | 2003-12-09 |
Family
ID=24058482
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0108902-1A BR0108902A (pt) | 2000-03-02 | 2001-03-02 | Motor de carga direcionado |
Country Status (11)
Country | Link |
---|---|
US (3) | US6430919B1 (pt) |
EP (1) | EP1264100A4 (pt) |
JP (1) | JP2004500515A (pt) |
KR (1) | KR20030025908A (pt) |
CN (1) | CN1522339A (pt) |
AU (1) | AU2001274804A1 (pt) |
BR (1) | BR0108902A (pt) |
CA (1) | CA2401759A1 (pt) |
EA (1) | EA004390B1 (pt) |
MX (1) | MXPA02008619A (pt) |
WO (1) | WO2001065103A1 (pt) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20080000215A1 (en) * | 2000-03-02 | 2008-01-03 | Duncan Ronnie J | Engine systems and methods |
US6874452B2 (en) | 2002-01-15 | 2005-04-05 | Joseph S. Adams | Resonant combustion chamber and recycler for linear motors |
JP4618612B2 (ja) * | 2004-03-29 | 2011-01-26 | 国立大学法人横浜国立大学 | パルスデトネーションエンジン着火方法及びその装置 |
US20090090110A1 (en) * | 2007-10-04 | 2009-04-09 | Honeywell International, Inc. | Faceted dome assemblies for gas turbine engine combustors |
GB2519155B (en) * | 2013-10-11 | 2016-10-12 | Reaction Engines Ltd | Engine |
CN104373247B (zh) * | 2014-09-26 | 2016-06-22 | 汤广武 | 内爆式推动器 |
IT202100001439A1 (it) * | 2021-01-26 | 2022-07-26 | Sidereus Space Dynamics S R L | Motore a razzo a doppia modalità di funzionamento e metodo di funzionamento di detto motore |
CN117869126A (zh) * | 2024-03-12 | 2024-04-12 | 西安航天动力研究所 | 一种火箭发动机燃烧室的直流式点火结构 |
Family Cites Families (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US864821A (en) * | 1905-05-22 | 1907-09-03 | Heinrich Zoelly | Explosive-turbine. |
US2810261A (en) * | 1952-10-15 | 1957-10-22 | Plessey Co Ltd | Combustion control system |
US2951339A (en) * | 1959-03-31 | 1960-09-06 | United Aircraft Corp | Combustion chamber swirler |
DE1233207B (de) * | 1960-06-29 | 1967-01-26 | Klein Hans Christof | Vorrichtung zur periodischen Erzeugung von hochverdichtetem Arbeitsgas fuer Waermekraftmaschinen |
US3185871A (en) * | 1961-07-20 | 1965-05-25 | Jr Albert G Bodine | Alternating current magnetohydrodynamic generator |
US4034673A (en) | 1976-02-23 | 1977-07-12 | Calspan Corporation | Armor penetration shaped-charge projectile |
US4170110A (en) | 1976-07-19 | 1979-10-09 | Edward Radin | Combustion process |
US4074858A (en) | 1976-11-01 | 1978-02-21 | Institute Of Gas Technology | High pressure pulsed water jet apparatus and process |
US4510748A (en) | 1979-11-05 | 1985-04-16 | Adams Joseph S | Compression wave former |
JPS5853690A (ja) | 1981-09-25 | 1983-03-30 | Jidosha Kiki Co Ltd | ベ−ンポンプ |
US4938112A (en) | 1984-06-22 | 1990-07-03 | Washington Research Foundation | Apparatus and method for the acceleration of projectiles to hypervelocities |
EP0193029B1 (de) * | 1985-02-26 | 1988-11-17 | BBC Brown Boveri AG | Brennkammer für Gasturbinen |
FR2661454B1 (fr) | 1985-07-12 | 1994-02-11 | Onera | Perfectionnements apportes aux propulseurs de type statoreacteur. |
US4726184A (en) | 1985-09-09 | 1988-02-23 | Rockwell International Corporation | Rocket engine assembly |
FR2588372B1 (fr) | 1985-10-08 | 1989-07-13 | Thomson Brandt Armements | Dispositif de pilotage pour projectile guide au moyen de tuyeres laterales |
DE3603497C1 (de) | 1986-02-05 | 1993-01-07 | Rheinmetall Gmbh | Geschoss fuer eine Panzerabwehrwaffe zur Bekaempfung eines Panzers von oben |
US4724738A (en) | 1986-04-22 | 1988-02-16 | Johnson Family Enterprises | Space entry actuator launch system |
CH672366A5 (pt) * | 1986-12-09 | 1989-11-15 | Bbc Brown Boveri & Cie | |
GB8701578D0 (en) | 1987-01-24 | 1987-02-25 | Jaguar Cars | Supercharging i c engines |
JP2565988B2 (ja) | 1988-07-29 | 1996-12-18 | 株式会社東芝 | 連結式パルス燃焼装置 |
US5052176A (en) | 1988-09-28 | 1991-10-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Combination turbojet-ramjet-rocket propulsion system |
US5090891A (en) | 1989-06-26 | 1992-02-25 | Indugas, Inc. | Hybrid combustion device and system therefor |
FR2656382B1 (fr) | 1989-12-21 | 1994-07-08 | Europ Propulsion | Moteur a propulsion combinee a haute adaptabilite pour aeronef ou avion spatial. |
US5363766A (en) | 1990-02-08 | 1994-11-15 | The United States Of America As Represented By The Secretary Of The Army | Remjet powered, armor piercing, high explosive projectile |
US5194690A (en) | 1990-02-21 | 1993-03-16 | Teledyne Industries, Inc. | Shock compression jet gun |
US5111746A (en) | 1991-06-21 | 1992-05-12 | The United States Of America As Represented By The Secretary Of The Army | Multiple stage munition |
US5873240A (en) | 1993-04-14 | 1999-02-23 | Adroit Systems, Inc. | Pulsed detonation rocket engine |
US6003301A (en) | 1993-04-14 | 1999-12-21 | Adroit Systems, Inc. | Exhaust nozzle for multi-tube detonative engines |
US5901550A (en) | 1993-04-14 | 1999-05-11 | Adroit Systems, Inc. | Liquid fueled pulse detonation engine with controller and inlet and exit valves |
US5345758A (en) | 1993-04-14 | 1994-09-13 | Adroit Systems, Inc. | Rotary valve multiple combustor pulse detonation engine |
US5557926A (en) | 1994-06-24 | 1996-09-24 | Lockheed-Martin | Pulse detonation apparatus with inner and outer Spherical valves |
US5572864A (en) | 1994-09-16 | 1996-11-12 | Martin Marietta Corporation | Solid-fuel, liquid oxidizer hybrid rocket turbopump auxiliary engine |
FR2734025B1 (fr) * | 1995-05-11 | 1997-08-01 | Europ Propulsion | Moteur fusee a propergol liquide, a impulsions |
US6000214A (en) | 1996-07-08 | 1999-12-14 | Scragg; Robert L. | Detonation cycle gas turbine engine system having intermittent fuel and air delivery |
US5831155A (en) | 1996-12-02 | 1998-11-03 | Atlantic Research Corporation | Apparatus and method for simulating rocket-to-ramjet transition in a propulsion system |
US5890459A (en) | 1997-09-12 | 1999-04-06 | Southwest Research Institute | System and method for a dual fuel, direct injection combustion engine |
-
2000
- 2000-03-02 US US09/517,130 patent/US6430919B1/en not_active Expired - Fee Related
-
2001
- 2001-03-02 AU AU2001274804A patent/AU2001274804A1/en not_active Abandoned
- 2001-03-02 BR BR0108902-1A patent/BR0108902A/pt not_active IP Right Cessation
- 2001-03-02 EP EP01941451A patent/EP1264100A4/en not_active Withdrawn
- 2001-03-02 KR KR1020027011503A patent/KR20030025908A/ko not_active Application Discontinuation
- 2001-03-02 MX MXPA02008619A patent/MXPA02008619A/es unknown
- 2001-03-02 CN CNA018089151A patent/CN1522339A/zh active Pending
- 2001-03-02 JP JP2001563775A patent/JP2004500515A/ja active Pending
- 2001-03-02 WO PCT/US2001/006617 patent/WO2001065103A1/en not_active Application Discontinuation
- 2001-03-02 CA CA002401759A patent/CA2401759A1/en not_active Abandoned
- 2001-03-02 EA EA200200936A patent/EA004390B1/ru not_active IP Right Cessation
-
2002
- 2002-06-14 US US10/172,406 patent/US6658838B2/en not_active Expired - Fee Related
-
2003
- 2003-10-15 US US10/687,452 patent/US20040134184A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US6430919B1 (en) | 2002-08-13 |
US20040134184A1 (en) | 2004-07-15 |
MXPA02008619A (es) | 2004-09-06 |
CN1522339A (zh) | 2004-08-18 |
KR20030025908A (ko) | 2003-03-29 |
CA2401759A1 (en) | 2001-09-07 |
JP2004500515A (ja) | 2004-01-08 |
EP1264100A1 (en) | 2002-12-11 |
WO2001065103A1 (en) | 2001-09-07 |
AU2001274804A1 (en) | 2001-09-12 |
EA200200936A1 (ru) | 2003-02-27 |
EA004390B1 (ru) | 2004-04-29 |
EP1264100A4 (en) | 2003-09-10 |
US20030046920A1 (en) | 2003-03-13 |
US6658838B2 (en) | 2003-12-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR0108902A (pt) | Motor de carga direcionado | |
BR0308671A (pt) | sistema anti-detonação de distribuição de combustìvel | |
CR6537A (es) | Disposicion mejorada para la combustion de combustible en masa | |
WO2000025067A8 (en) | Fuel air mixer for a radial dome in a gas turbine engine combustor | |
WO2005042924A3 (en) | Centrifugal supercharger | |
TW200519287A (en) | Combustion chamber structure in an internal combustion engine | |
AR027468A1 (es) | CONJUNTO QUEMADOR DE BAJO RUIDO Y BAJAS EMISIONES DE NOx Y METODO PARA REDUCIR EL CONTENIDO DE NOx DEL GAS DE COMBUSTION DE UN HORNO | |
BR0106672A (pt) | Sistema de injeção de combustìvel e processo para a injeção | |
BRPI0510876A (pt) | sistema de aperto de velas de ignição para caldeiras e/ou similares | |
BR0110229A (pt) | Queimador de biomassa | |
EP1574783A4 (en) | COMBUSTION CHAMBER FOR ANIMAL AND VEGETABLE OILS | |
ES2162407T3 (es) | Motor de combustion interna de encendido por chispa que tiene una camara de combustion provisto de tres valvulas y una bujia de encendido central. | |
ATE475803T1 (de) | Einspritzventil | |
BR0107067A (pt) | Biela do motor de combustão interna | |
JP2009068354A (ja) | エンジンの直接噴射式燃焼室 | |
KR950029541A (ko) | 실린더 헤드의 연소실 구조 | |
ES2174539T3 (es) | Palanca de accionamiento de valvula. | |
DK1474636T3 (da) | Brænder til indvendig forbrænding, navnlig til trækning af mineralfibre | |
PT963517E (pt) | Dispositivo de distribuicao de carburante para a alimentacao dos cilindros de um motor de combustao interna | |
ES2046796T3 (es) | Procedimiento para el funcionamiento de un motor de combustion interna. | |
BR0205965A (pt) | Estrutura para passagem de óleo lubrificante em motor de combustão interna | |
RU2002122027A (ru) | Запальная горелка с калильным зажиганием | |
KR200174524Y1 (ko) | 다기공 목탄 | |
KR100405883B1 (ko) | 부연소실 엔진에서 매연 저감을 위한 피스톤 구조 | |
KR200384500Y1 (ko) | 솔레노이드 밸브의 파일롯트부 피스톤 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: application dismissed [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 5A, 6A E 7A ANUIDADES. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: REFERENTE AO DESPACHO PUBLICADO NA RPI 1963 DE 19.08.2008. |