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SE8904172D0 - Nozzle with thrust vectoring in the yaw direction - Google Patents

Nozzle with thrust vectoring in the yaw direction

Info

Publication number
SE8904172D0
SE8904172D0 SE8904172A SE8904172A SE8904172D0 SE 8904172 D0 SE8904172 D0 SE 8904172D0 SE 8904172 A SE8904172 A SE 8904172A SE 8904172 A SE8904172 A SE 8904172A SE 8904172 D0 SE8904172 D0 SE 8904172D0
Authority
SE
Sweden
Prior art keywords
thrust vectoring
nozzle
deflectors
yaw direction
dimensional
Prior art date
Application number
SE8904172A
Other languages
English (en)
Other versions
SE466665B (sv
SE8904172L (sv
Inventor
M K Mc Lean
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SE8904172D0 publication Critical patent/SE8904172D0/sv
Publication of SE8904172L publication Critical patent/SE8904172L/sv
Publication of SE466665B publication Critical patent/SE466665B/sv

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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
  • Multiple-Way Valves (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Sampling And Sample Adjustment (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
  • Percussion Or Vibration Massage (AREA)
SE8904172A 1989-04-11 1989-12-11 Munstycke med sidoriktad dragkraftinstaellning SE466665B (sv)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
SE8904172D0 true SE8904172D0 (sv) 1989-12-11
SE8904172L SE8904172L (sv) 1990-10-12
SE466665B SE466665B (sv) 1992-03-16

Family

ID=23315944

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8904172A SE466665B (sv) 1989-04-11 1989-12-11 Munstycke med sidoriktad dragkraftinstaellning

Country Status (12)

Country Link
US (1) US4978071A (sv)
JP (1) JPH02275049A (sv)
KR (1) KR930003085B1 (sv)
CN (1) CN1046019A (sv)
AU (1) AU614450B2 (sv)
CA (1) CA2013931A1 (sv)
CH (1) CH680814A5 (sv)
DE (1) DE3940472C2 (sv)
FR (1) FR2645594A1 (sv)
GB (1) GB2230240B (sv)
NO (1) NO168882C (sv)
SE (1) SE466665B (sv)

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US7055307B2 (en) * 2004-08-31 2006-06-06 General Electric Company Vectorable nozzle with sideways pivotable ramp
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
WO2007001373A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences Inbound transition control for a trail-sitting vertical take off and landing aircraft
US7441724B2 (en) 2004-09-17 2008-10-28 Aurora Flight Sciences Corporation System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft
WO2007001372A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences Ducted spinner for engine cooling
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US7481038B2 (en) * 2004-10-28 2009-01-27 United Technologies Corporation Yaw vectoring for exhaust nozzle
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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
EP2074321B1 (en) * 2006-10-12 2012-12-05 United Technologies Corporation Fan variable area nozzle with adaptive structure and method of varying a fan exit area of a gas turbine engine
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
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
US8127532B2 (en) * 2008-11-26 2012-03-06 The Boeing Company Pivoting fan nozzle nacelle
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
US11365016B2 (en) 2013-08-27 2022-06-21 The Regents Of The University Of Michigan Electrodeless plasma thruster
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
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
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
CN108026890A (zh) 2015-05-07 2018-05-11 纳特尔能源公司 液力涡轮
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
EP4026159A4 (en) 2019-09-04 2024-03-20 Phase Four, Inc. FUEL INJECTION SYSTEM FOR PLASMA PRODUCTION DEVICES AND THRUNES
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

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Also Published As

Publication number Publication date
SE466665B (sv) 1992-03-16
KR930003085B1 (ko) 1993-04-17
GB2230240B (en) 1992-12-16
JPH02275049A (ja) 1990-11-09
US4978071A (en) 1990-12-18
SE8904172L (sv) 1990-10-12
CA2013931A1 (en) 1990-10-11
GB8927712D0 (en) 1990-02-07
CH680814A5 (sv) 1992-11-13
KR900016607A (ko) 1990-11-14
NO894952D0 (no) 1989-12-08
NO168882C (no) 1992-04-15
FR2645594A1 (fr) 1990-10-12
AU614450B2 (en) 1991-08-29
NO894952L (no) 1990-10-12
DE3940472C2 (de) 1993-10-14
GB2230240A (en) 1990-10-17
AU4607289A (en) 1990-10-18
DE3940472A1 (de) 1990-10-18
CN1046019A (zh) 1990-10-10
NO168882B (no) 1992-01-06

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