BE713074A - - Google Patents

Info

Publication number
BE713074A
BE713074A BE713074DA BE713074A BE 713074 A BE713074 A BE 713074A BE 713074D A BE713074D A BE 713074DA BE 713074 A BE713074 A BE 713074A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE713074A publication Critical patent/BE713074A/xx

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • F02K1/383Introducing air inside the jet with retractable elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
BE713074D 1967-04-07 1968-04-01 BE713074A (en:Method)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR101852A FR1525355A (fr) 1967-04-07 1967-04-07 Silencieux débrayable pour avion à réaction

Publications (1)

Publication Number Publication Date
BE713074A true BE713074A (en:Method) 1968-08-16

Family

ID=8628358

Family Applications (1)

Application Number Title Priority Date Filing Date
BE713074D BE713074A (en:Method) 1967-04-07 1968-04-01

Country Status (6)

Country Link
US (1) US3550721A (en:Method)
BE (1) BE713074A (en:Method)
DE (1) DE1751079A1 (en:Method)
FR (1) FR1525355A (en:Method)
GB (1) GB1218631A (en:Method)
NL (1) NL6804667A (en:Method)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3579993A (en) * 1969-08-04 1971-05-25 Rohr Corp Sound suppression system
US3647020A (en) * 1970-02-02 1972-03-07 Rohr Corp Jet propulsion apparatus and operating method
US3618700A (en) * 1970-06-15 1971-11-09 Boeing Co Retracted noise suppression system
US3695387A (en) * 1970-09-08 1972-10-03 Rohr Corp Sound suppression system for fan jet engines
US3815360A (en) * 1971-04-16 1974-06-11 Rohr Industries Inc Combined infrared and sound suppressor for aircraft jet engine
US3830431A (en) * 1973-03-23 1974-08-20 Nasa Abating exhaust noises in jet engines
US4196585A (en) * 1976-10-04 1980-04-08 Chuiko Viktor M Ejector-type engine thrust augmentor
US5910094A (en) * 1996-09-10 1999-06-08 The Boeing Company Aircraft labyrinth fire seal
US5771681A (en) * 1996-09-17 1998-06-30 The Boeing Company Aircraft turbofan engine mixing apparatus
US5779150A (en) * 1996-10-01 1998-07-14 The Boeing Company Aircraft engine ejector nozzle
US5794434A (en) * 1996-10-09 1998-08-18 The Boeing Company Aircraft thrust reverser system with linearly translating inner and outer doors
US5941065A (en) * 1996-11-04 1999-08-24 The Boeing Company Stowable mixer ejection nozzle
US5884843A (en) * 1996-11-04 1999-03-23 The Boeing Company Engine noise suppression ejector nozzle
US6227846B1 (en) 1996-11-08 2001-05-08 Shrinkfast Corporation Heat gun with high performance jet pump and quick change attachments
EP0841518B1 (en) * 1996-11-08 2003-02-05 Shrinkfast Corporation Heat gun with high performance jet pump and quick change attachments
US5908159A (en) * 1997-02-24 1999-06-01 The Boeing Company Aircraft chute ejector nozzle
US5826794A (en) * 1997-02-28 1998-10-27 The Boeing Company Aircraft scoop ejector nozzle
RU2182672C1 (ru) * 2001-01-15 2002-05-20 Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз" Выходное двухмерное сопло для воздушно-реактивного двигателя
FR2896274B1 (fr) * 2006-01-13 2008-04-18 Snecma Sa Melangeur de flux a section variable pour turboreacteur double flux d'avion supersonique
FR2911922B1 (fr) * 2007-01-26 2009-04-24 Snecma Sa Melangeur de flux a section variable pour turboreacteur a double flux d'avion supersonique
US20160017815A1 (en) * 2013-03-12 2016-01-21 United Technologies Corporation Expanding shell flow control device
FR3011038B1 (fr) * 2013-09-23 2015-10-23 Snecma Capot primaire a volets se chevauchant pour tuyere a flux confluents de turbomachine
US10566097B2 (en) 2017-03-27 2020-02-18 Ge-Hitachi Nuclear Energy Americas Llc Intermixing feedwater sparger nozzles and methods for using the same in nuclear reactors

Also Published As

Publication number Publication date
US3550721A (en) 1970-12-29
DE1751079A1 (de) 1975-06-19
NL6804667A (en:Method) 1968-10-08
FR1525355A (fr) 1968-05-17
GB1218631A (en) 1971-01-06

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