DE602006001431D1 - Schwenkbare Schubdüse eines Flugtriebwerkes - Google Patents

Schwenkbare Schubdüse eines Flugtriebwerkes

Info

Publication number
DE602006001431D1
DE602006001431D1 DE602006001431T DE602006001431T DE602006001431D1 DE 602006001431 D1 DE602006001431 D1 DE 602006001431D1 DE 602006001431 T DE602006001431 T DE 602006001431T DE 602006001431 T DE602006001431 T DE 602006001431T DE 602006001431 D1 DE602006001431 D1 DE 602006001431D1
Authority
DE
Germany
Prior art keywords
aircraft engine
exhaust nozzle
pivoting
pivoting exhaust
nozzle
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.)
Active
Application number
DE602006001431T
Other languages
English (en)
Inventor
Philippe Bouiller
Michel Franchet
Jean-Pierre Ruis
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
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602006001431D1 publication Critical patent/DE602006001431D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02K1/006—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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity
    • 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)
  • Transmission Devices (AREA)
  • Control Of Turbines (AREA)
DE602006001431T 2005-04-26 2006-04-03 Schwenkbare Schubdüse eines Flugtriebwerkes Active DE602006001431D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0504154A FR2884874B1 (fr) 2005-04-26 2005-04-26 Tuyere d'ejection orientable d'un moteur d'aeronef

Publications (1)

Publication Number Publication Date
DE602006001431D1 true DE602006001431D1 (de) 2008-07-24

Family

ID=35645645

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006001431T Active DE602006001431D1 (de) 2005-04-26 2006-04-03 Schwenkbare Schubdüse eines Flugtriebwerkes

Country Status (4)

Country Link
US (1) US7555894B2 (de)
EP (1) EP1717432B1 (de)
DE (1) DE602006001431D1 (de)
FR (1) FR2884874B1 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103867341B (zh) * 2012-12-14 2016-07-13 上海新力动力设备研究所 一种小型固体火箭发动机球窝摆动喷管空间矢量抗扭装置
RU2529283C1 (ru) * 2013-04-18 2014-09-27 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Осесимметричное сопло турбореактивного двигателя
WO2019014386A1 (en) * 2017-07-12 2019-01-17 Jetoptera, Inc. AUGMENTATION FAIRING IN CARDAN
RU2696833C1 (ru) * 2018-04-26 2019-08-06 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Поворотное осесимметричное сопло турбореактивного двигателя
CN111237083B (zh) * 2018-11-28 2022-01-11 海鹰航空通用装备有限责任公司 组合喷管结构及具有其的飞机
CN112555049A (zh) * 2020-12-03 2021-03-26 北方工业大学 一种微型涡轮喷气发动机的外套式矢量喷管结构

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3302885A (en) * 1962-06-22 1967-02-07 Lockheed Aircraft Corp Swinveled rocket motor nozzle
FR1460577A (fr) * 1965-06-14 1966-03-04 Snecma Perfectionnements à la liaison articulée des conduits, notamment à l'accrochage du canal d'éjection d'un propulseur à réaction
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
FR2776338B1 (fr) * 1998-03-23 2000-08-11 Snecma Protection contre les efforts de traction d'une butee flexible reliant une tuyere a un corps de propulseur
US6938408B2 (en) * 2001-04-26 2005-09-06 Propulsion Vectoring, L.P. Thrust vectoring and variable exhaust area for jet engine nozzle
US7216476B2 (en) * 2003-12-09 2007-05-15 The Boeing Company Two-axis thrust vectoring nozzle

Also Published As

Publication number Publication date
US7555894B2 (en) 2009-07-07
US20060236676A1 (en) 2006-10-26
FR2884874B1 (fr) 2007-06-15
EP1717432A1 (de) 2006-11-02
EP1717432B1 (de) 2008-06-11
FR2884874A1 (fr) 2006-10-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition