GB1218631A - Improved silencer assembly for jet engines - Google Patents

Improved silencer assembly for jet engines

Info

Publication number
GB1218631A
GB1218631A GB05257/68A GB1525768A GB1218631A GB 1218631 A GB1218631 A GB 1218631A GB 05257/68 A GB05257/68 A GB 05257/68A GB 1525768 A GB1525768 A GB 1525768A GB 1218631 A GB1218631 A GB 1218631A
Authority
GB
United Kingdom
Prior art keywords
trough members
members
nozzle
ring member
trough
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
GB05257/68A
Other languages
English (en)
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
Publication of GB1218631A publication Critical patent/GB1218631A/en
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)
GB05257/68A 1967-04-07 1968-03-29 Improved silencer assembly for jet engines Expired GB1218631A (en)

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
GB1218631A true GB1218631A (en) 1971-01-06

Family

ID=8628358

Family Applications (1)

Application Number Title Priority Date Filing Date
GB05257/68A Expired GB1218631A (en) 1967-04-07 1968-03-29 Improved silencer assembly for jet engines

Country Status (6)

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

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
EP0841518B1 (en) * 1996-11-08 2003-02-05 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
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
BE713074A (enExample) 1968-08-16
NL6804667A (enExample) 1968-10-08
US3550721A (en) 1970-12-29
FR1525355A (fr) 1968-05-17
DE1751079A1 (de) 1975-06-19

Similar Documents

Publication Publication Date Title
GB1218631A (en) Improved silencer assembly for jet engines
US3409228A (en) Ejector nozzle
US3032977A (en) Correlated bypass inlet and outlet control for a supersonic reaction powerplant
GB1078421A (en) Nozzle having a silencer effect for jet propulsion engines
GB1092170A (en) Improvements in thrust reversers for jet propulsion powerplants
GB937829A (en) Deflector assembly defining convergent nozzles
GB1009776A (en) Supersonic jet propulsion nozzle
GB907288A (en) Fluid intake for supersonic flow
GB1147351A (en) Improvements in thrust reverser for jet propulsion engine
GB1100099A (en) Improvements in convergent-divergent jet exhaust nozzle for supersonic aircraft
GB933612A (en) Jet engine thrust reversers
GB750307A (en) Improvements relating to variable nozzles for gas-turbine jet propulsion engines
GB772363A (en) Improvements in or relating to jet propulsion nozzles
GB1338240A (en) Thrust reversing device
GB1019857A (en) Jet propulsion nozzle assembly
US2920446A (en) Shock positioning means
GB1166396A (en) Improvements in Power Plant with Thrust Reverser.
US2841955A (en) Directional control for jets
GB1278801A (en) Jet nozzle for a gas turbine engine
GB1114478A (en) Jet propulsion nozzle having a central bulbous body
GB1038854A (en) Nozzle assembly for a jet propulsion engine
ES301570A1 (es) Un motor de chorro para despegue vertical
GB1142660A (en) Improvements in combination jet exhaust nozzle and thrust reverser
GB895331A (en) Improvements in or relating to jet propulsion nozzles
GB859994A (en) Noise suppressor for jet propulsion engines