DE3066639D1 - Swivelling nozzle for jet propulsion - Google Patents

Swivelling nozzle for jet propulsion

Info

Publication number
DE3066639D1
DE3066639D1 DE8080401626T DE3066639T DE3066639D1 DE 3066639 D1 DE3066639 D1 DE 3066639D1 DE 8080401626 T DE8080401626 T DE 8080401626T DE 3066639 T DE3066639 T DE 3066639T DE 3066639 D1 DE3066639 D1 DE 3066639D1
Authority
DE
Germany
Prior art keywords
jet propulsion
swivelling
nozzle
swivelling nozzle
propulsion
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.)
Expired
Application number
DE8080401626T
Other languages
German (de)
English (en)
Inventor
Jean Georges Bouiller
Raymond Jean Maurice Joubert
Jacques Andre Jean Pous
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE3066639D1 publication Critical patent/DE3066639D1/de
Expired legal-status Critical Current

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
    • 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
    • F02K1/008—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 in any rearward direction

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Nozzles (AREA)
  • Quick-Acting Or Multi-Walled Pipe Joints (AREA)
DE8080401626T 1979-11-23 1980-11-13 Swivelling nozzle for jet propulsion Expired DE3066639D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7929208A FR2470253A1 (fr) 1979-11-23 1979-11-23 Tuyere orientable pour propulseur a reaction

Publications (1)

Publication Number Publication Date
DE3066639D1 true DE3066639D1 (en) 1984-03-22

Family

ID=9232145

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8080401626T Expired DE3066639D1 (en) 1979-11-23 1980-11-13 Swivelling nozzle for jet propulsion

Country Status (4)

Country Link
US (1) US4363445A (enExample)
EP (1) EP0029773B1 (enExample)
DE (1) DE3066639D1 (enExample)
FR (1) FR2470253A1 (enExample)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2501786A1 (fr) * 1981-03-13 1982-09-17 Snecma Dispositif de roulement et de guidage d'une tuyere orientable de propulseur a reaction
US4519543A (en) * 1982-04-07 1985-05-28 Rolls-Royce Inc. Vectorable nozzles for turbomachines
US4550877A (en) * 1982-08-03 1985-11-05 Rolls-Royce Inc. Streamlined nozzle for turbomachines
FR2569785B1 (fr) * 1984-09-06 1986-09-12 Snecma Disposit
US4836451A (en) * 1987-09-10 1989-06-06 United Technologies Corporation Yaw and pitch convergent-divergent thrust vectoring nozzle
FR2643947B1 (fr) * 1989-03-01 1991-05-17 Snecma Ensemble d'ejection de turboreacteur a tuyere axisymetrique a section variable et a poussee orientable
US4994660A (en) * 1989-04-11 1991-02-19 Hitachi, Ltd. Axisymmetric vectoring exhaust nozzle
US4978071A (en) * 1989-04-11 1990-12-18 General Electric Company Nozzle with thrust vectoring in the yaw direction
US4993641A (en) * 1989-10-26 1991-02-19 United Technologies Corporation Gas turbine spherical exhaust nozzle
US5076496A (en) * 1990-02-05 1991-12-31 General Electric Company Exhaust nozzle flap seal
US5082182A (en) * 1990-08-23 1992-01-21 United Technologies Corporation Thrust vectoring exhaust nozzle
US5261605A (en) * 1990-08-23 1993-11-16 United Technologies Corporation Axisymmetric nozzle with gimbled unison ring
US5150839A (en) * 1991-03-14 1992-09-29 General Electric Company Nozzle load management
ES2075782B1 (es) * 1992-02-20 1998-03-16 Sener Ing & Sist Tobera orientable de geometria variable para turbinas de gas.
ES2105928B1 (es) * 1993-09-21 1998-05-01 Sener Ing & Sist Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas.
FR2789122B1 (fr) 1999-01-29 2001-04-27 Snecma Systeme d'activation de tuyere orientable pour propulseur a reaction utilisant plusieurs ensembles elastiques repartis circonferentiellement
FR2789123B1 (fr) * 1999-01-29 2001-04-27 Snecma Systeme d'activation de tuyere orientable par anneau elastique pour propulseur a reaction
RU2162956C2 (ru) * 1999-04-06 2001-02-10 Открытое акционерное общество "Авиадвигатель" Поворотное осесимметричное сопло
RU2162955C2 (ru) * 1999-04-06 2001-02-10 Открытое акционерное общество "Авиадвигатель" Поворотное осесимметричное сопло
FR2792368B1 (fr) 1999-04-19 2001-05-25 Snecma Tuyere d'ejection de turboreacteur a systeme d'orientation du type cardan
FR2835288B1 (fr) * 2002-01-31 2006-04-28 Snecma Moteurs Systeme de refroidissement pour une tuyere de post-combustion de turbomachine
US20060150612A1 (en) * 2005-01-12 2006-07-13 Honeywell International Inc. Thrust vector control
FR2884874B1 (fr) * 2005-04-26 2007-06-15 Snecma Moteurs Sa Tuyere d'ejection orientable d'un moteur d'aeronef
US8931281B2 (en) 2010-06-07 2015-01-13 United Technologies Corporation External flap retaining mechanism
RU2696833C1 (ru) * 2018-04-26 2019-08-06 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Поворотное осесимметричное сопло турбореактивного двигателя
US10837402B2 (en) 2020-01-09 2020-11-17 Guanhao Wu Thrust vector nozzle
CN112761810B (zh) * 2021-01-15 2021-10-22 中国航发沈阳发动机研究所 一种航空发动机喷管及其扩张片拉杆结构
US11772809B2 (en) * 2021-11-27 2023-10-03 Airbus Defence and Space GmbH Fuselage for an aircraft with fuselage-integrated tailplane

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3094072A (en) * 1957-12-09 1963-06-18 Arthur R Parilla Aircraft, missiles, missile weapons systems, and space ships
US3182452A (en) * 1959-04-15 1965-05-11 Bendix Corp Movable thrust nozzle and sealing means therefor
US3090198A (en) * 1960-11-17 1963-05-21 Gen Motors Corp Swivel nozzle control
DE1192058B (de) * 1962-07-28 1965-04-29 Dornier Werke Gmbh Strahlumlenkeinrichtung aus mehreren hinter-einander angeordneten schwenkbaren Ringen
US3390899A (en) * 1965-03-15 1968-07-02 Lockheed Aircraft Corp Flexible joint means
US3696999A (en) * 1967-07-17 1972-10-10 Thlokol Chem Corp Movable thrust nozzle for rockets
US3504903A (en) * 1967-08-22 1970-04-07 Trw Inc Double acting laminated bearing flexible joint
US3860134A (en) * 1972-07-26 1975-01-14 Aerojet General Co Flexible nozzle for a thrust vector control system
DE2639474C2 (de) * 1976-09-02 1982-06-16 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkanordnung für eine Schubdüse
DE2719439C2 (de) * 1977-04-30 1984-01-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Schubdüse zur Vektorsteuerung
FR2408037A1 (fr) * 1977-11-07 1979-06-01 Aerospatiale Tuyere chaude

Also Published As

Publication number Publication date
EP0029773A1 (fr) 1981-06-03
FR2470253A1 (fr) 1981-05-29
US4363445A (en) 1982-12-14
FR2470253B1 (enExample) 1983-06-24
EP0029773B1 (fr) 1984-02-15

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Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee