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FR2402077A1 - Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz - Google Patents

Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz

Info

Publication number
FR2402077A1
FR2402077A1 FR7619687A FR7619687A FR2402077A1 FR 2402077 A1 FR2402077 A1 FR 2402077A1 FR 7619687 A FR7619687 A FR 7619687A FR 7619687 A FR7619687 A FR 7619687A FR 2402077 A1 FR2402077 A1 FR 2402077A1
Authority
FR
France
Prior art keywords
maneuverable
gas turbine
turbine engine
ejection device
flaps
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
FR7619687A
Other languages
English (en)
Other versions
FR2402077B1 (fr
Inventor
Robert Gerald Beavers
Kermit Franklin Byrd
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2402077A1 publication Critical patent/FR2402077A1/fr
Application granted granted Critical
Publication of FR2402077B1 publication Critical patent/FR2402077B1/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Exhaust Silencers (AREA)
  • Toys (AREA)

Abstract

Dispositif de complexité réduite, ayant un profil aérodynamique permettant son installation dans une aile d'avion. Il comprend une première paroi 72 définissant partiellement un chemin d'écoulement 42 du courant de gaz éjectés, un dispositif déflecteur 80 comportant un premier volet articulé 82, un deuxième volet articulé 84 et un dispositif 94 couplé aux premier et deuxième volets afin d'obtenir un mouvement synchronisé de ces volets, une deuxième paroi 108 comprenant un troisième volet 114 à position variable et un dispositif d'actionnement 118 couplé aux deuxième et troisième volets. Application aux avions de combat.
FR7619687A 1975-06-30 1976-06-29 Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz Granted FR2402077A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/591,879 US3986687A (en) 1975-06-30 1975-06-30 Aircraft propulsion system with flight maneuverable exhaust nozzle

Publications (2)

Publication Number Publication Date
FR2402077A1 true FR2402077A1 (fr) 1979-03-30
FR2402077B1 FR2402077B1 (fr) 1983-07-01

Family

ID=24368335

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7619687A Granted FR2402077A1 (fr) 1975-06-30 1976-06-29 Dispositif d'ejection manoeuvrable en vol pour un moteur a turbine a gaz

Country Status (7)

Country Link
US (1) US3986687A (fr)
JP (1) JPS6056255B2 (fr)
CA (1) CA1050773A (fr)
DE (1) DE2628808A1 (fr)
FR (1) FR2402077A1 (fr)
GB (2) GB1546108A (fr)
IT (1) IT1062477B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101327844A (zh) * 2007-06-20 2008-12-24 通用电气公司 用于推进系统的推力发生器

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2924742C2 (de) * 1979-06-20 1983-12-08 Dornier Gmbh, 7990 Friedrichshafen Großflugzeug, insbesondere in Schulterdeckerbauart
US4280660A (en) * 1979-08-17 1981-07-28 General Electric Company Vectorable nozzle
GB2247048B (en) * 1981-06-27 1992-05-13 Rolls Royce Variable area nozzles for turbomachines
FR2734323A1 (fr) * 1985-04-17 1996-11-22 Snecma Perfectionnement aux tuyeres bidimensionnelles comportant en particulier un deviateur de jet
GB2194597B (en) * 1986-08-29 1990-07-25 Rolls Royce Plc A variable area exhaust nozzle for a gas turbine engine
US4813607A (en) * 1987-10-02 1989-03-21 Allied-Signal Inc. Variable-area thrust vectoring and reversing asymmetric aircraft exhaust nozzle
US5042745A (en) * 1989-09-18 1991-08-27 Grumann Aerospace Corporation Tilt ramp swept edge nozzle
US5050803A (en) * 1989-10-12 1991-09-24 General Electric Company Actuation system for positioning a vectoring exhaust nozzle
US5407133A (en) * 1989-12-26 1995-04-18 United Technologies Corporation Cooled thin metal liner
US6918244B2 (en) * 2001-08-17 2005-07-19 John Eugene Dickau Vertical takeoff and landing aircraft propulsion systems
US6857600B1 (en) 2002-04-26 2005-02-22 General Electric Company Infrared suppressing two dimensional vectorable single expansion ramp nozzle
US7395657B2 (en) * 2003-10-20 2008-07-08 General Electric Company Flade gas turbine engine with fixed geometry inlet
US20070018034A1 (en) * 2005-07-12 2007-01-25 Dickau John E Thrust vectoring
JP5406251B2 (ja) * 2011-08-10 2014-02-05 網矢 ハル子 分散噴射型エンジン
US9915228B2 (en) 2013-08-16 2018-03-13 United Technologies Corporation Air with integral spring for a gas turbine engine exhaust drive
US10378451B2 (en) 2013-09-13 2019-08-13 United Technologies Corporation Large displacement high temperature seal
CN104875887B (zh) * 2015-06-23 2017-06-16 中国航空工业集团公司西安飞机设计研究所 一种垂直提升组件以及具有其的扇翼飞行器
CN107923247B (zh) 2015-08-12 2020-12-25 通用电气公司 用于涡轮发动机的扩散器和其形成方法
US9889924B2 (en) * 2015-08-24 2018-02-13 The Boeing Company Multi-directional control using upper surface blowing systems
US11084605B2 (en) * 2016-02-05 2021-08-10 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Device and system for controlling missiles and kill vehicles operated with gel-like fuels
RU2674232C1 (ru) * 2017-10-05 2018-12-05 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Плоское сопло турбореактивного авиационного двигателя
US10718264B2 (en) * 2018-03-16 2020-07-21 The Boeing Company Inlet diffusers for jet engines, jet engines, jet aircraft, and methods for diffusing incoming air of jet engines
CN112963854B (zh) * 2020-07-30 2021-12-21 山东大学 一种均温效果的烟道分配器
CN112963853B (zh) * 2020-07-30 2021-12-21 山东大学 一种设置烟道分配器的锅炉系统
CN114000958B (zh) * 2021-10-29 2022-11-08 厦门大学 基于双拨片型滑块原理的tbcc尾喷管调节机构设计方法

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479487A (en) * 1946-01-28 1949-08-16 Goembel William Philip Jet propelled airplane with wing discharge slot
US2802333A (en) * 1951-12-28 1957-08-13 Lockheed Aircraft Corp Variable area and direction changing propulsive nozzle
CH326061A (de) * 1953-04-08 1957-11-30 Power Jets Res & Dev Ltd Antriebseinrichtung an einem Flugzeug
FR1166520A (fr) * 1956-11-20 1958-11-12 Continental Aviat & Eng Corp Brûleur-veilleuse pour réacteurs
US2880575A (en) * 1952-11-28 1959-04-07 Curtiss Wright Corp Combined variable area nozzle and aerodynamic brake
GB859713A (en) * 1958-05-03 1961-01-25 Rolls Royce Improvements in or relating to combustion systems for gas turbine engines
US2978204A (en) * 1955-09-28 1961-04-04 Power Jets Res & Dev Ltd Aircraft flying control systems
GB889540A (en) * 1959-07-24 1962-02-14 Harald Eugen Markus Improvements in or relating to jet propelled aircraft
FR1307026A (fr) * 1960-11-28 1962-10-19 Rolls Royce Perfectionnements aux dispositifs de tuyère de propulsion à réaction pour aérodynes
FR1329959A (fr) * 1962-07-27 1963-06-14 Rolls Royce Moteurs à réaction à tuyère convergente-divergente
US3095695A (en) * 1959-11-23 1963-07-02 Gen Motors Corp Convergent-divergent jet nozzle
US3148848A (en) * 1957-08-13 1964-09-15 Nathan C Price Wingless supersonic aircraft
GB1060051A (en) * 1965-01-11 1967-02-22 Rolls Royce Improvements in or relating to gas turbine engines
FR2228156A1 (fr) * 1973-05-02 1974-11-29 Rolls Royce

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2420323A (en) * 1943-07-21 1947-05-13 Westinghouse Electric Corp Wing-mounted jet-propulsion system with controllable discharge outlet
GB951130A (en) * 1961-07-28 1964-03-04 Rolls Royce Improvements relating to jet engines
US3658279A (en) * 1970-04-21 1972-04-25 Lockheed Aircraft Corp Integrated propulsion system

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2479487A (en) * 1946-01-28 1949-08-16 Goembel William Philip Jet propelled airplane with wing discharge slot
US2802333A (en) * 1951-12-28 1957-08-13 Lockheed Aircraft Corp Variable area and direction changing propulsive nozzle
US2880575A (en) * 1952-11-28 1959-04-07 Curtiss Wright Corp Combined variable area nozzle and aerodynamic brake
CH326061A (de) * 1953-04-08 1957-11-30 Power Jets Res & Dev Ltd Antriebseinrichtung an einem Flugzeug
US2978204A (en) * 1955-09-28 1961-04-04 Power Jets Res & Dev Ltd Aircraft flying control systems
FR1166520A (fr) * 1956-11-20 1958-11-12 Continental Aviat & Eng Corp Brûleur-veilleuse pour réacteurs
US3148848A (en) * 1957-08-13 1964-09-15 Nathan C Price Wingless supersonic aircraft
GB859713A (en) * 1958-05-03 1961-01-25 Rolls Royce Improvements in or relating to combustion systems for gas turbine engines
GB889540A (en) * 1959-07-24 1962-02-14 Harald Eugen Markus Improvements in or relating to jet propelled aircraft
US3095695A (en) * 1959-11-23 1963-07-02 Gen Motors Corp Convergent-divergent jet nozzle
FR1307026A (fr) * 1960-11-28 1962-10-19 Rolls Royce Perfectionnements aux dispositifs de tuyère de propulsion à réaction pour aérodynes
FR1329959A (fr) * 1962-07-27 1963-06-14 Rolls Royce Moteurs à réaction à tuyère convergente-divergente
GB1060051A (en) * 1965-01-11 1967-02-22 Rolls Royce Improvements in or relating to gas turbine engines
FR2228156A1 (fr) * 1973-05-02 1974-11-29 Rolls Royce

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101327844A (zh) * 2007-06-20 2008-12-24 通用电气公司 用于推进系统的推力发生器
CN101327844B (zh) * 2007-06-20 2014-03-05 通用电气公司 用于推进系统的推力发生器

Also Published As

Publication number Publication date
FR2402077B1 (fr) 1983-07-01
DE2628808A1 (de) 1977-01-27
US3986687A (en) 1976-10-19
DE2628808C2 (fr) 1987-10-22
GB1546109A (en) 1979-05-16
IT1062477B (it) 1984-10-10
JPS527598A (en) 1977-01-20
CA1050773A (fr) 1979-03-20
GB1546108A (en) 1979-05-16
JPS6056255B2 (ja) 1985-12-09

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Legal Events

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