KR900016607A - 요오 방향으로의 추력 벡터링 노즐 - Google Patents
요오 방향으로의 추력 벡터링 노즐 Download PDFInfo
- Publication number
- KR900016607A KR900016607A KR1019890018223A KR890018223A KR900016607A KR 900016607 A KR900016607 A KR 900016607A KR 1019890018223 A KR1019890018223 A KR 1019890018223A KR 890018223 A KR890018223 A KR 890018223A KR 900016607 A KR900016607 A KR 900016607A
- Authority
- KR
- South Korea
- Prior art keywords
- flap
- deflector
- nozzle
- diverging
- flaps
- 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
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
- F02K1/006—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
- F02K1/1292—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series hinged at their upstream ends on a substantially axially movable structure
-
- 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)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Supercharger (AREA)
- Exhaust Silencers (AREA)
- Control Of Turbines (AREA)
- Sampling And Sample Adjustment (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Percussion Or Vibration Massage (AREA)
- Multiple-Way Valves (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
내용 없음.
Description
본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음
제1도는 본 발명의 특성을 반영한 배기 노즐을 포함하는 개스 터빈 엔진의 측면선도,
제2도는 수렴 및 발산플랩과 디플렉터 플랩과 회전 작동기를 포함하는 2차원 수렴 발산 배기 노즐의 부분 사시도,
제3도는 제1도의 개스 터빈 엔진 배기 노즐의 단면도.
Claims (11)
- 디플렉터 플랩이 노즐의 흐름 표면상의 한 선에 관해 회전가능하도록 노즐에 힌지된 적어도 하나의 디플렉터플랩과, 상기 디플렉터 플랩을 배기 흐름 방향내로 한 각도에 배치시키기 위한 수단을 포함하는 것을 특징으로 하는 노즐의 배기 개스 흐름 방향 설정용 추력 벡터링 장치.
- 제1항에 있어서, 상호 대칭 관계로 배치된 두 개의 상기 디플렉터 플랩을 포함하는 것을 특징으로 하는 노즐의 배기 개스 흐름 방향 설정용 추력 벡터링 장치.
- 제2항에 있어서, 두 세트의 상기 디플렉터 플랩을 포함하는데, 한 세트는 다른 세트에 대해 대칭 관계로 배치되고, 각각의 세트는 상호 대칭 관계로 배치된 두 개의 상기 디플렉터 플랩을 포함하는 것을 특징으로 하는 노즐의 배기 개스 흐름 방향 설정용 추력 벡터링 장치.
- 제1항에 있어서, 상기 노즐의 대향 측면에 배치된 두 개의 상기 디플렉터 플랩을 포함하는 것을 특징으로 하는 노즐의 배기 개스 흐름 방향 설정용 추력 벡터링 장치.
- 상부 및 하부의 한 세트의 수렴 플랩과, 각각의 수렴 플랩에 피봇가능하게 연결된 한 세트의 상,하부 발산 플랩과, 상기 플랩의 외부에, 상기 플랩에 대체로 수직하게, 또한, 상기 플랩과 흐름 밀봉 및 미끄럼 결합 상태로 배치된 좌,우측벽과, 노즐의 흐름 표면상의 한 선에 관해 회전할 수 있도록 노즐에 힌지된 적어도 네 개의 디플렉터 플랩과, 상기 디플렉터 플랩의 흐름 편향 표면이 배기 흐름의 중심을 향하도록 상기 디플렉터 플랩을 상기 흐름내에 배치시키고, 또한, 상기 배기 흐름의 방향에 대해 예각으로 상기 디플렉터 플랩을 배치시키기 위한 배치수단을 포함하는 것을 특징으로 하는 2차원의 추력 벡터링 수렴, 발산 노즐.
- 수렴부와, 발산부와, 그 사이의 목부분과, 상기 발산부내에서 배기 흐름의 적어도 일부를 요오 방향으로 편향시키는 편향 수단을 포함하는 것을 특징으로 하는 2차원의 수렴 발산 노즐.
- 제6항에 있어서, 상기 목부분의 면적으로 변화시키는 수단을 포함하는 것을 특징으로 하는 2차원의 수렵 발산 벡터가능 노즐.
- 제7항에 있어서, 상기 발산부내에 상부 및 하부 발산 노즐 플랩을 포함하는데, 상기 편향 수단중의 적어도 하나는 상기 발산 노즐 플랩상에 장착된 것을 특징으로 하는 2차원의 수렴 발산 벡터가능 노즐.
- 제8항에 있어서, 상기 편향 수단은, 상기 발산 노즐 플랩의 표면상의 한 선에 관해 회전할 수 있도록 상기 발산 노즐 플랩의 하나에 힌지된 적어도 하나의 디플렉터 플랩과, 상기 디플레터 플랩을 상기 발산 노즐 플랩의 흐름 표면에 연한배기 흐름내의 흐름의 방향에 대해 한 각도로 배치하기 위한 배치 수단을 포함하는 것을 특징으로 하는 2차원의 수렴 발산 벡터가능 노즐.
- 제9항에 있어서, 상기 편향 수단은 상호 대칭 관계로 배치된 두 개의 디플렉터 플랩을 포함하는 것을 특징으로 하는 2차원의 수렴 발산 벡터가능 노즐.
- 제10항에 있어서, 상기 편향 수단은 두 세트의 상기 디플렉터 플랩을 포합하는데, 한 세트는 다른 세트에 대해 대칭 관계로 배치되고, 각각의 세트는 상호 대칭 관계로 배치된 두 개의 상기 디플렉터 플랩을 포함하는 것을 특징으로 하는 2차원의 수렴 발산 벡터가능 노즐.※ 참고사항 :최초출원 내용에 의하여 공개하는 것임.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/336,405 US4978071A (en) | 1989-04-11 | 1989-04-11 | Nozzle with thrust vectoring in the yaw direction |
US336405 | 1999-06-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
KR900016607A true KR900016607A (ko) | 1990-11-14 |
KR930003085B1 KR930003085B1 (ko) | 1993-04-17 |
Family
ID=23315944
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1019890018223A KR930003085B1 (ko) | 1989-04-11 | 1989-12-09 | 2차원 수렴 발산 노즐의 배기 흐름 방향 설정용 추력 벡터링 장치 |
Country Status (13)
Country | Link |
---|---|
US (1) | US4978071A (ko) |
JP (1) | JPH02275049A (ko) |
KR (1) | KR930003085B1 (ko) |
CN (1) | CN1046019A (ko) |
AU (1) | AU614450B2 (ko) |
CA (1) | CA2013931A1 (ko) |
CH (1) | CH680814A5 (ko) |
DE (1) | DE3940472C2 (ko) |
FR (1) | FR2645594A1 (ko) |
GB (1) | GB2230240B (ko) |
IT (1) | IT1237860B (ko) |
NO (1) | NO168882C (ko) |
SE (1) | SE466665B (ko) |
Families Citing this family (56)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5050803A (en) * | 1989-10-12 | 1991-09-24 | General Electric Company | Actuation system for positioning a vectoring exhaust nozzle |
US5031836A (en) * | 1990-07-10 | 1991-07-16 | United Technologies Corporation | Flexible fairing for airframe/nozzle interface |
US5261604A (en) * | 1992-05-11 | 1993-11-16 | General Electric Company | Yaw vectoring blade |
US5294055A (en) * | 1992-09-08 | 1994-03-15 | Mcdonnell Douglas Corporation | Rotatable arms for thrust vectoring and changing the area of a nozzle throat |
FR2706946B1 (fr) * | 1993-06-23 | 1995-07-28 | Soc Nat Detude Et De Construction De Moteurs Daviation Snecma | Tuyere d'echappement pseudo-bidimensionnelle |
US5442909A (en) * | 1994-05-13 | 1995-08-22 | General Electric Company | Control system for limiting the vector angle in an axisymmetric vectoring exhaust nozzle |
GB2366265B (en) * | 1995-05-30 | 2002-06-19 | Rolls Royce Plc | Vtol aircraft nozzle |
IL116668A (en) * | 1996-01-03 | 1998-12-06 | Univ Ramot | Apparatus and method for controlling the motion of a solid body or fluid stream |
ES2136528B1 (es) * | 1996-12-26 | 2000-05-01 | Sener Ing & Sist | Perfeccionamientos en toberas axisimetricas de geometria variable y orientacion del flujo destinadasa propulsores de turbina de gas |
US6857600B1 (en) | 2002-04-26 | 2005-02-22 | General Electric Company | Infrared suppressing two dimensional vectorable single expansion ramp nozzle |
US6619915B1 (en) * | 2002-08-06 | 2003-09-16 | Power Systems Mfg, Llc | Thermally free aft frame for a transition duct |
US6948317B2 (en) * | 2003-10-31 | 2005-09-27 | General Electric Company | Methods and apparatus for flade engine nozzle |
US7188477B2 (en) * | 2004-04-21 | 2007-03-13 | United Technologies Corporation | High temperature dynamic seal for scramjet variable geometry |
US7055307B2 (en) * | 2004-08-31 | 2006-06-06 | General Electric Company | Vectorable nozzle with sideways pivotable ramp |
WO2006137869A2 (en) | 2004-09-17 | 2006-12-28 | Aurora Flight Sciences | System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft |
EP1796962A2 (en) * | 2004-09-17 | 2007-06-20 | Aurora Flight Sciences | Inbound transition control for a trail-sitting vertical take off and landing aircraft |
WO2007001369A2 (en) * | 2004-09-17 | 2007-01-04 | Aurora Flight Sciences | System and method for controlling engine rpm of a ducted fan aircraft |
WO2007001371A2 (en) | 2004-09-17 | 2007-01-04 | Aurora Flight Sciences | Vibration isolation engine mount system and method for ducted fan aircraft |
US7559191B2 (en) | 2004-09-17 | 2009-07-14 | Aurora Flight Sciences Corporation | Ducted spinner for engine cooling |
US7096662B2 (en) * | 2004-09-28 | 2006-08-29 | General Electric Company | Variable area throat exhaust nozzle with vectorable sideways shifting of exhaust flow |
US7481038B2 (en) * | 2004-10-28 | 2009-01-27 | United Technologies Corporation | Yaw vectoring for exhaust nozzle |
SE527787C2 (sv) * | 2004-11-05 | 2006-06-07 | Volvo Aero Corp | Utloppsanordning till en jetmotor och en jetmotor innefattande sådan utloppsanordning |
US7475548B2 (en) * | 2005-09-09 | 2009-01-13 | General Electric Company | Vectorable nozzle with pivotable triangular panels |
US7837141B2 (en) * | 2006-03-22 | 2010-11-23 | The Boeing Company | Reaction drive rotor/wing variable area nozzle |
US7368828B1 (en) * | 2006-03-29 | 2008-05-06 | Calhoon Scott W | Wind energy system |
FR2903454B1 (fr) * | 2006-07-05 | 2008-08-29 | Airbus France Sas | Nacelle de reacteur d'aeronef et aeronef comprenant une telle nacelle |
WO2008063154A2 (en) * | 2006-10-12 | 2008-05-29 | United Technologies Corporation | Fan variable area nozzle with adaptive structure |
US8020367B2 (en) * | 2007-03-16 | 2011-09-20 | General Electric Company | Nozzle with yaw vectoring vane |
US7726609B2 (en) * | 2007-03-16 | 2010-06-01 | The Boeing Company | High-performance low-noise aircraft exhaust systems and methods |
US7615894B1 (en) | 2007-05-15 | 2009-11-10 | Deal Clarence D | Electric motor with a permanent magnet carrier rotating a sprocket |
FR2929998B1 (fr) * | 2008-04-14 | 2011-08-12 | Aircelle Sa | Nacelle de turboreacteur a double flux |
US7582982B1 (en) | 2008-08-27 | 2009-09-01 | Deal Clarence D | Omni Directional wind generator |
US8127532B2 (en) * | 2008-11-26 | 2012-03-06 | The Boeing Company | Pivoting fan nozzle nacelle |
US8959889B2 (en) | 2008-11-26 | 2015-02-24 | The Boeing Company | Method of varying a fan duct nozzle throat area of a gas turbine engine |
CN101985903B (zh) * | 2010-09-03 | 2014-03-05 | 清华大学 | 两段式发动机推力转向机构 |
KR101159648B1 (ko) * | 2011-07-29 | 2012-06-25 | 삼성탈레스 주식회사 | 제트엔진이 탑재된 미사일 기만기 |
CN102434315B (zh) * | 2011-11-28 | 2014-05-28 | 南京航空航天大学 | 旁路式双喉道无源矢量喷管 |
US9435292B2 (en) | 2012-02-23 | 2016-09-06 | United Technologies Corporation | Turbine engine with thrust vectoring exhaust nozzle |
EP2813696B1 (de) * | 2013-06-12 | 2015-12-02 | MTU Aero Engines GmbH | Schubumlenkvorrichtung sowie Flugtriebwerk |
WO2015031447A1 (en) * | 2013-08-27 | 2015-03-05 | The Regents Of The University Of Michigan | Converging/diverging magnetic nozzle |
AU2014312406A1 (en) | 2013-08-27 | 2016-03-17 | The Regents Of The University Of Michigan | Electrodeless plasma thruster |
CN103423023A (zh) * | 2013-09-04 | 2013-12-04 | 西北工业大学 | 一种脉冲爆震发动机二元收敛扩张喷管 |
CN103437911B (zh) * | 2013-09-04 | 2015-11-18 | 北京航空航天大学 | 带隔板流体控制二元矢量喷管及其矢量推力产生和控制方法 |
JP6361404B2 (ja) * | 2014-09-17 | 2018-07-25 | 三菱重工業株式会社 | 推力偏向装置、および、推力偏向装置を備える飛しょう体 |
CA2984914A1 (en) * | 2015-05-07 | 2016-11-10 | Natel Energy, Inc. | Hydraulic turbine |
US9964069B2 (en) | 2015-06-29 | 2018-05-08 | United Technologies Corporation | Exhaust nozzle control for a gas turbine engine |
CN104975983B (zh) * | 2015-07-09 | 2017-12-12 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种二元收敛喷管 |
CN104948344B (zh) * | 2015-07-09 | 2017-11-03 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种二元收敛喷管 |
CN107161330A (zh) * | 2017-05-27 | 2017-09-15 | 四川建筑职业技术学院 | 一种可变异型结构的变距多旋翼无人机 |
RU2674232C1 (ru) * | 2017-10-05 | 2018-12-05 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Плоское сопло турбореактивного авиационного двигателя |
CN109878702A (zh) * | 2017-12-06 | 2019-06-14 | 林瑤章 | 推力向量控制器 |
RU2771587C1 (ru) * | 2021-07-20 | 2022-05-06 | Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") | Регулируемое сопло турбореактивного двигателя |
CN113788139B (zh) * | 2021-10-26 | 2024-05-24 | 上海磐拓航空科技服务有限公司 | 一种多功能气动舵面精准控制飞行器轨迹的方法 |
CN114109647B (zh) * | 2021-11-12 | 2023-02-28 | 中国航发沈阳发动机研究所 | 一种可调喷管外罩机构 |
US11767806B1 (en) | 2022-03-07 | 2023-09-26 | Rohr, Inc. | Variable area nozzle assembly |
WO2024151226A1 (en) * | 2023-01-09 | 2024-07-18 | Kanal Mehmet Engin | Thrust vectoring system |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2839891A (en) * | 1953-11-27 | 1958-06-24 | Boeing Co | Thrust reversers for jet engines |
DE1225503B (de) * | 1964-11-26 | 1966-09-22 | Dornier Werke Gmbh | Verschlusseinrichtung fuer den Boden eines Hubtriebwerksschachtes |
US3442455A (en) * | 1967-07-07 | 1969-05-06 | Gen Motors Corp | Jet deflecting nozzle |
US3640469A (en) * | 1967-07-14 | 1972-02-08 | Gen Motors Corp | Constant-area vectoring nozzle |
US3666044A (en) * | 1971-04-13 | 1972-05-30 | Claud R Killian | Jet engine sound suppressor |
US3874620A (en) * | 1973-03-09 | 1975-04-01 | Boeing Co | Reversing apparatus for a jet engine |
US3981451A (en) * | 1975-11-17 | 1976-09-21 | Rohr Industries, Inc. | Fan cascade thrust reverser |
DE2719439C2 (de) * | 1977-04-30 | 1984-01-19 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Schwenkbare Schubdüse zur Vektorsteuerung |
US4128208A (en) * | 1977-07-11 | 1978-12-05 | General Electric Company | Exhaust nozzle flap seal arrangement |
US4176792A (en) * | 1977-07-11 | 1979-12-04 | General Electric Company | Variable area exhaust nozzle |
US4245787A (en) * | 1978-12-01 | 1981-01-20 | General Electric Company | Variable area nozzle system |
US4280660A (en) * | 1979-08-17 | 1981-07-28 | General Electric Company | Vectorable nozzle |
FR2470253A1 (fr) * | 1979-11-23 | 1981-05-29 | Snecma | Tuyere orientable pour propulseur a reaction |
US4375276A (en) * | 1980-06-02 | 1983-03-01 | General Electric Company | Variable geometry exhaust nozzle |
GB2155552B (en) * | 1981-02-24 | 1986-02-26 | Rolls Royce | Adjustable jet propulsion nozzle |
FR2501786A1 (fr) * | 1981-03-13 | 1982-09-17 | Snecma | Dispositif de roulement et de guidage d'une tuyere orientable de propulseur a reaction |
US4456178A (en) * | 1982-12-27 | 1984-06-26 | United Technologies Corporation | Exhaust nozzle assembly with dual unison ring structure |
US4575006A (en) * | 1983-06-13 | 1986-03-11 | United Technologies Corporation | Nozzle flap edge seal |
DE3327385C2 (de) * | 1983-07-29 | 1985-11-14 | Dornier Gmbh, 7990 Friedrichshafen | Strahlaustrittsdüse für Gasturbinenstrahltriebwerke |
FR2608680B1 (fr) * | 1986-12-17 | 1989-03-17 | Snecma | Tuyere bidimensionnelle reglable, notamment pour reacteur d'avion |
US4848664A (en) * | 1987-12-07 | 1989-07-18 | United Technologies Corporation | Yaw thrust vectoring exhaust nozzle |
-
1989
- 1989-04-11 US US07/336,405 patent/US4978071A/en not_active Expired - Fee Related
- 1989-12-04 IT IT02260789A patent/IT1237860B/it active IP Right Grant
- 1989-12-06 FR FR8916131A patent/FR2645594A1/fr not_active Withdrawn
- 1989-12-07 GB GB8927712A patent/GB2230240B/en not_active Expired - Fee Related
- 1989-12-07 DE DE3940472A patent/DE3940472C2/de not_active Expired - Fee Related
- 1989-12-08 NO NO894952A patent/NO168882C/no unknown
- 1989-12-08 AU AU46072/89A patent/AU614450B2/en not_active Ceased
- 1989-12-08 JP JP1317955A patent/JPH02275049A/ja active Pending
- 1989-12-09 KR KR1019890018223A patent/KR930003085B1/ko not_active IP Right Cessation
- 1989-12-09 CN CN89109241A patent/CN1046019A/zh active Pending
- 1989-12-11 SE SE8904172A patent/SE466665B/sv not_active IP Right Cessation
- 1989-12-11 CH CH4433/89A patent/CH680814A5/de not_active IP Right Cessation
-
1990
- 1990-04-05 CA CA002013931A patent/CA2013931A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
GB2230240A (en) | 1990-10-17 |
NO168882C (no) | 1992-04-15 |
SE466665B (sv) | 1992-03-16 |
GB2230240B (en) | 1992-12-16 |
DE3940472A1 (de) | 1990-10-18 |
CH680814A5 (ko) | 1992-11-13 |
NO894952D0 (no) | 1989-12-08 |
FR2645594A1 (fr) | 1990-10-12 |
IT1237860B (it) | 1993-06-18 |
AU614450B2 (en) | 1991-08-29 |
KR930003085B1 (ko) | 1993-04-17 |
SE8904172L (sv) | 1990-10-12 |
US4978071A (en) | 1990-12-18 |
DE3940472C2 (de) | 1993-10-14 |
IT8922607A0 (it) | 1989-12-04 |
NO168882B (no) | 1992-01-06 |
CN1046019A (zh) | 1990-10-10 |
JPH02275049A (ja) | 1990-11-09 |
SE8904172D0 (sv) | 1989-12-11 |
NO894952L (no) | 1990-10-12 |
CA2013931A1 (en) | 1990-10-11 |
AU4607289A (en) | 1990-10-18 |
GB8927712D0 (en) | 1990-02-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
KR900016607A (ko) | 요오 방향으로의 추력 벡터링 노즐 | |
KR900016606A (ko) | 축대칭 벡터링 배기 노즐 | |
US4778109A (en) | Adjustable two dimensional nozzle for aircraft jet engines | |
US5687907A (en) | Yaw and pitch thrust vectoring nozzle | |
US6000635A (en) | Exhaust nozzle for a turbojet engine | |
SE8005644L (sv) | Stalror med riktbar vektor | |
US3973731A (en) | Flap-type two-dimensional nozzle | |
ES2010586A6 (es) | Tobera de empuje vectorial para desvio y cabeceo convergente-divergente. | |
US5690280A (en) | Multifunction exhaust system for gas turbine engines | |
CA2034381A1 (en) | Exhaust nozzle flap seal | |
US5833139A (en) | Single variable flap exhaust nozzle | |
US6910328B1 (en) | Vectorable variable area nozzle | |
US3142153A (en) | Solid propellant rocket thrust vectoring system | |
IL104301A (en) | Thrust reverser integrating a variable exhaust area nozzle | |
US5215256A (en) | Flap hinge arrangement for a convergent/divergent nozzle | |
DE69205791D1 (de) | Schubumkehrvorrichtung mit verbesserter Umlenkung der Gasstrahlen. | |
GB1325370A (en) | Propulsion nozzle assemblies for aircraft jet propulsion engines | |
US5437412A (en) | Variable geometry jet engine exhaust nozzle | |
GB1435946A (en) | Efflux conduits for aircraft jet propulsion engines | |
EP0442899A4 (en) | Vane-type thrust vectoring nozzle | |
US4993641A (en) | Gas turbine spherical exhaust nozzle | |
GB1332278A (en) | Variable area and reversing jet propulsion nozzles | |
US3592389A (en) | Flap linkage | |
JPH03100359A (ja) | 排気ノズルヒンジ | |
US7967219B1 (en) | Thrust nozzle for a gas turbine engine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
A201 | Request for examination | ||
E902 | Notification of reason for refusal | ||
G160 | Decision to publish patent application | ||
E701 | Decision to grant or registration of patent right | ||
GRNT | Written decision to grant | ||
LAPS | Lapse due to unpaid annual fee |