DE602007000660D1 - Anordnung zum Ausstoßen von Treibgasen in einem Luftfahrzeug, die einen Bogen bildet - Google Patents

Anordnung zum Ausstoßen von Treibgasen in einem Luftfahrzeug, die einen Bogen bildet

Info

Publication number
DE602007000660D1
DE602007000660D1 DE602007000660T DE602007000660T DE602007000660D1 DE 602007000660 D1 DE602007000660 D1 DE 602007000660D1 DE 602007000660 T DE602007000660 T DE 602007000660T DE 602007000660 T DE602007000660 T DE 602007000660T DE 602007000660 D1 DE602007000660 D1 DE 602007000660D1
Authority
DE
Germany
Prior art keywords
ejecting
aircraft
arc
arrangement
forms
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
DE602007000660T
Other languages
English (en)
Inventor
Thomas Daris
Alain Pierre Page
Jackie Raymond Julien Prouteau
Edgar Brunet
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 DE602007000660D1 publication Critical patent/DE602007000660D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangements 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
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • 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
    • F02K1/40—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
    • 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
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F02K1/825—Infrared radiation suppressors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Exhaust Silencers (AREA)
DE602007000660T 2006-04-28 2007-04-25 Anordnung zum Ausstoßen von Treibgasen in einem Luftfahrzeug, die einen Bogen bildet Active DE602007000660D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0651543A FR2900388B1 (fr) 2006-04-28 2006-04-28 Ensemble d'echappement des gaz de propulsion dans un aeronef formant un coude

Publications (1)

Publication Number Publication Date
DE602007000660D1 true DE602007000660D1 (de) 2009-04-23

Family

ID=37709708

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007000660T Active DE602007000660D1 (de) 2006-04-28 2007-04-25 Anordnung zum Ausstoßen von Treibgasen in einem Luftfahrzeug, die einen Bogen bildet

Country Status (7)

Country Link
US (1) US7784284B2 (de)
EP (1) EP1849983B1 (de)
CA (1) CA2585878C (de)
DE (1) DE602007000660D1 (de)
FR (1) FR2900388B1 (de)
IL (1) IL182789A0 (de)
RU (1) RU2443891C2 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8061145B2 (en) * 2005-09-27 2011-11-22 Volvo Aero Corporation Arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine
US8783605B2 (en) * 2010-12-28 2014-07-22 Rolls-Royce North American Technologies, Inc. Flight vehicle, propulsion system and thrust vectoring system
EP2719621A3 (de) * 2012-10-10 2017-10-25 Sikorsky Aircraft Corporation Nachabgassystem für Drehflügelflugzeug
CN102926888B (zh) * 2012-11-16 2014-10-22 中国航空工业集团公司西安飞机设计研究所 一种隐身排气系统
US9644497B2 (en) 2013-11-22 2017-05-09 Siemens Energy, Inc. Industrial gas turbine exhaust system with splined profile tail cone
US9540956B2 (en) 2013-11-22 2017-01-10 Siemens Energy, Inc. Industrial gas turbine exhaust system with modular struts and collars
US9587519B2 (en) 2013-11-22 2017-03-07 Siemens Energy, Inc. Modular industrial gas turbine exhaust system
US9512740B2 (en) 2013-11-22 2016-12-06 Siemens Energy, Inc. Industrial gas turbine exhaust system with area ruled exhaust path
US9598981B2 (en) 2013-11-22 2017-03-21 Siemens Energy, Inc. Industrial gas turbine exhaust system diffuser inlet lip
CN105114206B (zh) * 2015-09-18 2017-06-16 中国航空工业集团公司沈阳发动机设计研究所 一种可降低红外和雷达信号特征的喷管
CN106438103A (zh) * 2016-05-30 2017-02-22 西北工业大学 一种s弯收‑扩喷管结构
CN108087148A (zh) * 2017-12-11 2018-05-29 中国航发沈阳发动机研究所 一种红外隐身喷管及具有其的飞机
RU2716651C2 (ru) * 2018-03-30 2020-03-13 Артём Георгиевич Арутюнов Система сопел двухконтурного турбореактивного двигателя
CN109611238B (zh) * 2018-12-24 2020-04-24 南京航空航天大学 一种肋片强化换热红外抑制器及红外抑制方法
KR20210090501A (ko) * 2020-01-10 2021-07-20 한화에어로스페이스 주식회사 배기 덕트 및 이를 이용하는 배기 덕트 어셈블리와 비행체
CN114562379B (zh) * 2022-01-13 2023-05-05 中国航发沈阳发动机研究所 一种作动筒长距可调引气喷管
CN114776461B (zh) * 2022-03-25 2023-04-07 中国民用航空飞行学院 一种用于航空发动机的s弯喷管及其设计方法
CN115217670B (zh) * 2022-05-24 2024-04-26 中国民用航空飞行学院 一种三涵道超声速喷管构型的设计方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3210934A (en) * 1964-11-30 1965-10-12 Gen Motors Corp Jet engine exhaust
US3981448A (en) * 1970-04-23 1976-09-21 The Garrett Corporation Cooled infrared suppressor
US4215537A (en) * 1978-07-27 1980-08-05 Avco Corporation Apparatus for and method of suppressing infrared radiation emitted from gas turbine engine
GB2044359B (en) * 1979-03-16 1982-10-27 Rolls Royce Gas turbine engine air intakes
US4280587A (en) * 1979-05-08 1981-07-28 The Boeing Company Noise-suppressing jet engine nozzles and method
US5746047A (en) * 1982-07-08 1998-05-05 Gereral Electric Company Infrared suppressor
US4864819A (en) * 1985-06-03 1989-09-12 General Electric Company Exhaust system including protective arrangements
DE3909347A1 (de) * 1989-03-22 1990-09-27 Mtu Muenchen Gmbh Schubduese zur schubvektorsteuerung fuer mit strahltriebwerken ausgeruestete fluggeraete
RU2046202C1 (ru) * 1992-06-05 1995-10-20 Варюхин Александр Сергеевич Устройство для управления вектором тяги методом вдува рабочего тела в сверхзвуковую часть сопла
US5404713A (en) * 1993-10-04 1995-04-11 General Electric Company Spillage drag and infrared reducing flade engine
US6000635A (en) * 1995-10-02 1999-12-14 Lockheed Martin Corporation Exhaust nozzle for a turbojet engine
US5699662A (en) * 1996-05-28 1997-12-23 Lockheed Martin Corporation Infrared suppression exhaust duct system for a turboprop propulsion system for an aircraft
US6112513A (en) * 1997-08-05 2000-09-05 Lockheed Martin Corporation Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow
SE515379C2 (sv) * 1999-12-22 2001-07-23 Saab Ab Utloppsanordning för en jetmotor samt flygfarkost med en utloppsanordning

Also Published As

Publication number Publication date
EP1849983A1 (de) 2007-10-31
US7784284B2 (en) 2010-08-31
CA2585878C (fr) 2014-07-08
FR2900388A1 (fr) 2007-11-02
RU2443891C2 (ru) 2012-02-27
EP1849983B1 (de) 2009-03-11
US20070266712A1 (en) 2007-11-22
IL182789A0 (en) 2007-08-19
CA2585878A1 (fr) 2007-10-28
RU2007115878A (ru) 2008-11-10
FR2900388B1 (fr) 2009-01-16

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition