FR1401425A - Dispositif de tuyère d'éjection pour avions à réaction - Google Patents

Dispositif de tuyère d'éjection pour avions à réaction

Info

Publication number
FR1401425A
FR1401425A FR972170A FR972170A FR1401425A FR 1401425 A FR1401425 A FR 1401425A FR 972170 A FR972170 A FR 972170A FR 972170 A FR972170 A FR 972170A FR 1401425 A FR1401425 A FR 1401425A
Authority
FR
France
Prior art keywords
jet
nozzle device
jet nozzle
jet jet
nozzle
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
FR972170A
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.)
Ateliers dAviation Louis Breguet SA
Original Assignee
Ateliers dAviation Louis Breguet 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 Ateliers dAviation Louis Breguet SA filed Critical Ateliers dAviation Louis Breguet SA
Priority to FR972170A priority Critical patent/FR1401425A/fr
Priority to GB11346/65A priority patent/GB1057265A/en
Priority to US443974A priority patent/US3333772A/en
Priority to DE19651476597 priority patent/DE1476597B1/de
Application granted granted Critical
Publication of FR1401425A publication Critical patent/FR1401425A/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
    • F02K1/36—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto having an ejector
    • 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
    • F02K1/42—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet the means being movable into an inoperative position

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Exhaust Silencers (AREA)
FR972170A 1964-04-24 1964-04-24 Dispositif de tuyère d'éjection pour avions à réaction Expired FR1401425A (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR972170A FR1401425A (fr) 1964-04-24 1964-04-24 Dispositif de tuyère d'éjection pour avions à réaction
GB11346/65A GB1057265A (en) 1964-04-24 1965-03-17 Discharge nozzle apparatus for jet aircraft
US443974A US3333772A (en) 1964-04-24 1965-03-30 Discharge nozzle apparatus for jet aircraft
DE19651476597 DE1476597B1 (de) 1964-04-24 1965-04-23 Austrittsduesenvorrichtung fuer Luftfahrzeuge mit Strahlantrieb

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR972170A FR1401425A (fr) 1964-04-24 1964-04-24 Dispositif de tuyère d'éjection pour avions à réaction

Publications (1)

Publication Number Publication Date
FR1401425A true FR1401425A (fr) 1965-06-04

Family

ID=8828586

Family Applications (1)

Application Number Title Priority Date Filing Date
FR972170A Expired FR1401425A (fr) 1964-04-24 1964-04-24 Dispositif de tuyère d'éjection pour avions à réaction

Country Status (4)

Country Link
US (1) US3333772A (fr)
DE (1) DE1476597B1 (fr)
FR (1) FR1401425A (fr)
GB (1) GB1057265A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2126922A1 (fr) * 1971-01-20 1972-10-13 Snecma

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3392529A (en) * 1965-07-23 1968-07-16 Rolls Royce Aircraft provided with a gas turbine vertical lift engine
FR1547756A (fr) * 1967-10-19 1968-11-29 Snecma Silencieux pour réacteurs aéronautiques
FR1588852A (fr) * 1968-07-31 1970-03-16
US3566989A (en) * 1969-12-01 1971-03-02 Rohr Corp Sound suppression nozzle structure for fan jet aircraft engine
US3667680A (en) * 1970-04-24 1972-06-06 Boeing Co Jet engine exhaust nozzle system
US3685293A (en) * 1970-05-13 1972-08-22 Herbert C Shipman Exhaust control for engines
US3726091A (en) * 1971-02-16 1973-04-10 Rohr Corp Sound suppressing apparatus
GB1473543A (en) * 1974-09-07 1977-05-11 Rolls Royce Gas turbine powerplants
US3990530A (en) * 1975-05-19 1976-11-09 United Technologies Corporation Noise suppressor for turbine type power plant
US4291782A (en) * 1979-10-30 1981-09-29 The Boeing Company Simplified method and apparatus for hot-shield jet noise suppression
US4501393A (en) * 1982-03-17 1985-02-26 The Boeing Company Internally ventilated noise suppressor with large plug nozzle
US5154052A (en) * 1990-05-07 1992-10-13 General Electric Company Exhaust assembly for a high speed civil transport aircraft engine
US5761899A (en) * 1995-05-11 1998-06-09 The Boeing Company Supersonic engine apparatus and method with ejector/suppressor
US5655360A (en) * 1995-05-31 1997-08-12 General Electric Company Thrust reverser with variable nozzle
US5884472A (en) * 1995-10-11 1999-03-23 Stage Iii Technologies, L.C. Alternating lobed mixer/ejector concept suppressor
US5761900A (en) * 1995-10-11 1998-06-09 Stage Iii Technologies, L.C. Two-stage mixer ejector suppressor
US5779150A (en) * 1996-10-01 1998-07-14 The Boeing Company Aircraft engine ejector nozzle
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
US5908159A (en) * 1997-02-24 1999-06-01 The Boeing Company Aircraft chute ejector nozzle
FR2890378B1 (fr) * 2005-09-08 2009-01-16 Airbus France Sas Capot de nacelle pour turboreacteur et nacelle comportant au moins un tel capot.
FR2929998B1 (fr) * 2008-04-14 2011-08-12 Aircelle Sa Nacelle de turboreacteur a double flux
FR3000994A1 (fr) * 2013-01-16 2014-07-18 Aircelle Sa Tuyere de nacelle a dispositifs de regulation de pression
US9863366B2 (en) * 2013-03-13 2018-01-09 Rolls-Royce North American Technologies Inc. Exhaust nozzle apparatus and method for multi stream aircraft engine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB834907A (en) * 1956-10-23 1960-05-11 Rolls Royce Improvements in or relating to jet propulsion nozzles
US3055174A (en) * 1957-01-14 1962-09-25 Boeing Co Retractable noise suppressor for jet engines
FR1164936A (fr) * 1957-01-21 1958-10-15 Bertin Et Cie Soc Silencieux pour conduits d'échappement et notamment pour tuyères de propulseurs àréaction
US3032981A (en) * 1957-02-11 1962-05-08 Boeing Co Noise suppressor and thrust reverser for jet engine nozzles
DE1094529B (de) * 1957-03-01 1960-12-08 Rolls Royce Strahltriebduese mit zwei einstellbaren Stellungen
DE1062988B (de) * 1957-03-12 1959-08-06 Rolls Royce Strahltriebduese
US2944624A (en) * 1957-08-07 1960-07-12 Rolls Royce Jet noise suppressor nozzle
GB895922A (en) * 1958-03-13 1962-05-09 Rolls Royce Improvements in or relating to aircraft gas-turbine jet propulsion engines
US3050937A (en) * 1958-06-09 1962-08-28 Boeing Co Reversible thrust jet engines and controls therefor
DE1100385B (de) * 1958-12-10 1961-02-23 Entwicklungsbau Pirna Veb Vorrichtung zur Laermbekaempfung des Abgasstrahles eines Strahltriebwerkes durch Zumischen von Frischluft und zur AEnderung der Ausstroemrichtung des Abgasstrahles mittels stellbarer Umlenkplatten
US3027714A (en) * 1959-06-11 1962-04-03 Canadair Ltd Combined thrust reversing and noise suppressing device for turbo-jet engines
US2987883A (en) * 1959-06-22 1961-06-13 Boeing Co Jet engine noise suppression nozzle with aerodynamic supplemental fluting

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2126922A1 (fr) * 1971-01-20 1972-10-13 Snecma

Also Published As

Publication number Publication date
GB1057265A (en) 1967-02-01
DE1476597B1 (de) 1970-10-15
US3333772A (en) 1967-08-01

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