FR2499158B1 - Dispositif de reduction de poussee residuelle pour turboreacteur - Google Patents

Dispositif de reduction de poussee residuelle pour turboreacteur

Info

Publication number
FR2499158B1
FR2499158B1 FR8102198A FR8102198A FR2499158B1 FR 2499158 B1 FR2499158 B1 FR 2499158B1 FR 8102198 A FR8102198 A FR 8102198A FR 8102198 A FR8102198 A FR 8102198A FR 2499158 B1 FR2499158 B1 FR 2499158B1
Authority
FR
France
Prior art keywords
turbo
jet
reducing device
drive reducing
residual drive
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
FR8102198A
Other languages
English (en)
Other versions
FR2499158A1 (fr
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR8102198A priority Critical patent/FR2499158B1/fr
Publication of FR2499158A1 publication Critical patent/FR2499158A1/fr
Application granted granted Critical
Publication of FR2499158B1 publication Critical patent/FR2499158B1/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
    • F02K1/06—Varying effective area of jet pipe or nozzle

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)
FR8102198A 1981-02-05 1981-02-05 Dispositif de reduction de poussee residuelle pour turboreacteur Expired FR2499158B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR8102198A FR2499158B1 (fr) 1981-02-05 1981-02-05 Dispositif de reduction de poussee residuelle pour turboreacteur

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8102198A FR2499158B1 (fr) 1981-02-05 1981-02-05 Dispositif de reduction de poussee residuelle pour turboreacteur

Publications (2)

Publication Number Publication Date
FR2499158A1 FR2499158A1 (fr) 1982-08-06
FR2499158B1 true FR2499158B1 (fr) 1985-10-18

Family

ID=9254857

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8102198A Expired FR2499158B1 (fr) 1981-02-05 1981-02-05 Dispositif de reduction de poussee residuelle pour turboreacteur

Country Status (1)

Country Link
FR (1) FR2499158B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8356483B2 (en) 2008-04-10 2013-01-22 United Technologies Corp Gas turbine engine systems involving variable nozzles with sliding doors

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB623108A (en) * 1944-07-29 1949-05-12 Westinghouse Electric Int Co Improvements in or relating to power plants
CA508034A (fr) * 1948-04-19 1954-12-07 Westinghouse Electric Corporation Appareil de turbine a gaz
GB1119608A (en) * 1966-10-27 1968-07-10 Rolls Royce Jet pipe with variable effective flow cross-sectional area for a gas turbine engine
FR1562941A (fr) * 1968-01-19 1969-04-11
FR2146109A1 (fr) * 1971-07-19 1973-03-02 Bruner Georges
GB1357370A (en) * 1971-09-24 1974-06-19 Rolls Royce Ducted fan gas turbine jet propulsion engine with thrust control means
GB1418905A (en) * 1972-05-09 1975-12-24 Rolls Royce Gas turbine engines

Also Published As

Publication number Publication date
FR2499158A1 (fr) 1982-08-06

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Legal Events

Date Code Title Description
ST Notification of lapse