FR1525355A - Silencieux débrayable pour avion à réaction - Google Patents

Silencieux débrayable pour avion à réaction

Info

Publication number
FR1525355A
FR1525355A FR101852A FR101852A FR1525355A FR 1525355 A FR1525355 A FR 1525355A FR 101852 A FR101852 A FR 101852A FR 101852 A FR101852 A FR 101852A FR 1525355 A FR1525355 A FR 1525355A
Authority
FR
France
Prior art keywords
disengageable
silencer
jet aircraft
aircraft
jet
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
FR101852A
Other languages
English (en)
French (fr)
Inventor
Georges Bruner
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.)
Breguet Aviation SA
Original Assignee
Breguet Aviation SA
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 Breguet Aviation SA filed Critical Breguet Aviation SA
Priority to FR101852A priority Critical patent/FR1525355A/fr
Priority to DE19681751079 priority patent/DE1751079A1/de
Priority to GB05257/68A priority patent/GB1218631A/en
Priority to BE713074D priority patent/BE713074A/xx
Priority to US718565A priority patent/US3550721A/en
Priority to NL6804667A priority patent/NL6804667A/xx
Application granted granted Critical
Publication of FR1525355A publication Critical patent/FR1525355A/fr
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
    • F02K1/38—Introducing air inside the jet
    • F02K1/383—Introducing 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)
FR101852A 1967-04-07 1967-04-07 Silencieux débrayable pour avion à réaction Expired FR1525355A (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR101852A FR1525355A (fr) 1967-04-07 1967-04-07 Silencieux débrayable pour avion à réaction
DE19681751079 DE1751079A1 (de) 1967-04-07 1968-03-29 Geraeuschdaempfungsvorrichtung
GB05257/68A GB1218631A (en) 1967-04-07 1968-03-29 Improved silencer assembly for jet engines
BE713074D BE713074A (OSRAM) 1967-04-07 1968-04-01
US718565A US3550721A (en) 1967-04-07 1968-04-03 Silencing assembly for jet engines
NL6804667A NL6804667A (OSRAM) 1967-04-07 1968-04-03

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
FR1525355A true FR1525355A (fr) 1968-05-17

Family

ID=8628358

Family Applications (1)

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

Country Status (6)

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

Cited By (4)

* 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
US3618700A (en) * 1970-06-15 1971-11-09 Boeing Co Retracted noise suppression system
US3647020A (en) * 1970-02-02 1972-03-07 Rohr Corp Jet propulsion apparatus and operating method
RU2182672C1 (ru) * 2001-01-15 2002-05-20 Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз" Выходное двухмерное сопло для воздушно-реактивного двигателя

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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

Cited By (4)

* 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
RU2182672C1 (ru) * 2001-01-15 2002-05-20 Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз" Выходное двухмерное сопло для воздушно-реактивного двигателя

Also Published As

Publication number Publication date
NL6804667A (OSRAM) 1968-10-08
GB1218631A (en) 1971-01-06
US3550721A (en) 1970-12-29
DE1751079A1 (de) 1975-06-19
BE713074A (OSRAM) 1968-08-16

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