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 (en0)

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 (en0) 1968-08-16

Family

ID=8628358

Family Applications (1)

Application Number Title Priority Date Filing Date
BE713074D BE713074A (en0) 1967-04-07 1968-04-01

Country Status (6)

Country Link
US (1) US3550721A (en0)
BE (1) BE713074A (en0)
DE (1) DE1751079A1 (en0)
FR (1) FR1525355A (en0)
GB (1) GB1218631A (en0)
NL (1) NL6804667A (en0)

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
US5884843A (en) * 1996-11-04 1999-03-23 The Boeing Company Engine noise suppression ejector nozzle
US5941065A (en) * 1996-11-04 1999-08-24 The Boeing Company Stowable mixer ejection nozzle
US6010329A (en) * 1996-11-08 2000-01-04 Shrinkfast Corporation Heat gun with high performance jet pump and quick change attachments
US6227846B1 (en) 1996-11-08 2001-05-08 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
WO2014197030A2 (en) * 2013-03-12 2014-12-11 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
NL6804667A (en0) 1968-10-08
GB1218631A (en) 1971-01-06
FR1525355A (fr) 1968-05-17
US3550721A (en) 1970-12-29
DE1751079A1 (de) 1975-06-19

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