FR91242E - Dispositif de tuyère d'éjection pour avions à réaction - Google Patents

Dispositif de tuyère d'éjection pour avions à réaction

Info

Publication number
FR91242E
FR91242E FR81810A FR81810A FR91242E FR 91242 E FR91242 E FR 91242E FR 81810 A FR81810 A FR 81810A FR 81810 A FR81810 A FR 81810A FR 91242 E FR91242 E FR 91242E
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
FR81810A
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
Priority to FR81810A priority Critical patent/FR91242E/fr
Priority to GB43431/67A priority patent/GB1170809A/en
Priority to US675552A priority patent/US3493178A/en
Priority to DE19671531377 priority patent/DE1531377A1/de
Application granted granted Critical
Publication of FR91242E publication Critical patent/FR91242E/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • 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
    • 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/563—Reversing jet main flow in specified direction, e.g. to obviate its reinjection

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Nozzles (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR81810A 1966-10-27 1966-10-27 Dispositif de tuyère d'éjection pour avions à réaction Expired FR91242E (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR81810A FR91242E (fr) 1966-10-27 1966-10-27 Dispositif de tuyère d'éjection pour avions à réaction
GB43431/67A GB1170809A (en) 1966-10-27 1967-09-25 Discharge Nozzle Apparatus for Jet Aircraft
US675552A US3493178A (en) 1966-10-27 1967-10-16 Ejection nozzle device for jet aircraft
DE19671531377 DE1531377A1 (de) 1966-10-27 1967-10-23 Duesenvorrichtung

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR81810A FR91242E (fr) 1966-10-27 1966-10-27 Dispositif de tuyère d'éjection pour avions à réaction

Publications (1)

Publication Number Publication Date
FR91242E true FR91242E (fr) 1968-05-03

Family

ID=8620057

Family Applications (1)

Application Number Title Priority Date Filing Date
FR81810A Expired FR91242E (fr) 1966-10-27 1966-10-27 Dispositif de tuyère d'éjection pour avions à réaction

Country Status (4)

Country Link
US (1) US3493178A (fr)
DE (1) DE1531377A1 (fr)
FR (1) FR91242E (fr)
GB (1) GB1170809A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2103536C1 (ru) * 1995-12-07 1998-01-27 Виктор Александрович Юрченко Устройство для реверсирования тяги реактивного двигателя
EP0822327A1 (fr) * 1996-08-01 1998-02-04 Hispano-Suiza Inverseur de poussée de turboréacteur à portes formant écopes

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4232516A (en) * 1977-10-05 1980-11-11 Rolls-Royce Limited Flow deflecting devices
WO1983003281A1 (fr) * 1982-03-17 1983-09-29 Klees, Garry, William Attenuateur de bruit ventile interieurement avec diffuseur a large tampon
US4502636A (en) * 1982-04-07 1985-03-05 Rolls-Royce Inc. Variable geometry ejector nozzle for turbomachines
US4807434A (en) * 1987-12-21 1989-02-28 The Boeing Company Thrust reverser for high bypass jet engines
US5761899A (en) * 1995-05-11 1998-06-09 The Boeing Company Supersonic engine apparatus and method with ejector/suppressor
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
US5842643A (en) * 1996-12-03 1998-12-01 General Electric Company Articulated exhaust nozzle fairing
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
US8713911B2 (en) * 2010-12-15 2014-05-06 Woodward Hrt, Inc. System and method for operating a thrust reverser for a turbofan propulsion system

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL67983C (fr) * 1945-03-22 1900-01-01
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
US3097484A (en) * 1960-06-13 1963-07-16 Thrust reversers for jet engines
US3347467A (en) * 1963-08-07 1967-10-17 Gen Electric Combination jet exhaust nozzle and thrust reverser

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2103536C1 (ru) * 1995-12-07 1998-01-27 Виктор Александрович Юрченко Устройство для реверсирования тяги реактивного двигателя
EP0822327A1 (fr) * 1996-08-01 1998-02-04 Hispano-Suiza Inverseur de poussée de turboréacteur à portes formant écopes
FR2752017A1 (fr) * 1996-08-01 1998-02-06 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes formant ecopes
WO1998005857A1 (fr) * 1996-08-01 1998-02-12 Hispano Suiza Inverseur de poussee de turboreacteur a portes formant ecopes
US5983625A (en) * 1996-08-01 1999-11-16 Societe Hispano-Suiza Pivoting door thrust reverser with deflecting passage within the door

Also Published As

Publication number Publication date
DE1531377A1 (de) 1971-03-25
US3493178A (en) 1970-02-03
GB1170809A (en) 1969-11-19

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