FR2277238B1 - - Google Patents

Info

Publication number
FR2277238B1
FR2277238B1 FR7423232A FR7423232A FR2277238B1 FR 2277238 B1 FR2277238 B1 FR 2277238B1 FR 7423232 A FR7423232 A FR 7423232A FR 7423232 A FR7423232 A FR 7423232A FR 2277238 B1 FR2277238 B1 FR 2277238B1
Authority
FR
France
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
FR7423232A
Other languages
French (fr)
Other versions
FR2277238A1 (en
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 FR7423232A priority Critical patent/FR2277238A1/en
Publication of FR2277238A1 publication Critical patent/FR2277238A1/en
Application granted granted Critical
Publication of FR2277238B1 publication Critical patent/FR2277238B1/fr
Granted 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
FR7423232A 1974-07-04 1974-07-04 Variable diameter exhaust duct for jet engine - has flaps fixed to ring linkage with radial linkage diagonals Granted FR2277238A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7423232A FR2277238A1 (en) 1974-07-04 1974-07-04 Variable diameter exhaust duct for jet engine - has flaps fixed to ring linkage with radial linkage diagonals

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7423232A FR2277238A1 (en) 1974-07-04 1974-07-04 Variable diameter exhaust duct for jet engine - has flaps fixed to ring linkage with radial linkage diagonals

Publications (2)

Publication Number Publication Date
FR2277238A1 FR2277238A1 (en) 1976-01-30
FR2277238B1 true FR2277238B1 (en) 1976-12-24

Family

ID=9140870

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7423232A Granted FR2277238A1 (en) 1974-07-04 1974-07-04 Variable diameter exhaust duct for jet engine - has flaps fixed to ring linkage with radial linkage diagonals

Country Status (1)

Country Link
FR (1) FR2277238A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2723145B1 (en) * 1981-11-24 1996-12-13 Snecma CONVERGENT-DIVERGENT NOZZLE, PARTICULARLY FOR A TURBOREACTOR
FR2732408A1 (en) * 1983-03-16 1996-10-04 Snecma Nozzles for gas turbine
US5176323A (en) * 1991-04-15 1993-01-05 General Electric Company Reduced weight nozzle actuation mechanism
RU2684362C1 (en) * 2018-02-13 2019-04-08 Государственный научный центр Российской Федерации-федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" Ram-jet adjustable split nozzle

Also Published As

Publication number Publication date
FR2277238A1 (en) 1976-01-30

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Legal Events

Date Code Title Description
ST Notification of lapse