FR2297326A1 - Perfectionnements aux tuyeres a geometrie variable pour propulseurs a reaction - Google Patents

Perfectionnements aux tuyeres a geometrie variable pour propulseurs a reaction

Info

Publication number
FR2297326A1
FR2297326A1 FR7501206A FR7501206A FR2297326A1 FR 2297326 A1 FR2297326 A1 FR 2297326A1 FR 7501206 A FR7501206 A FR 7501206A FR 7501206 A FR7501206 A FR 7501206A FR 2297326 A1 FR2297326 A1 FR 2297326A1
Authority
FR
France
Prior art keywords
actuators
jet pipe
downstream end
guide rollers
aircraft engine
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.)
Granted
Application number
FR7501206A
Other languages
English (en)
French (fr)
Other versions
FR2297326B1 (OSRAM
Inventor
Theophile Francois Le Maout
Georges Mazeaud
Roger Alfred Jul Vandenbroucke
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 FR7501206A priority Critical patent/FR2297326A1/fr
Publication of FR2297326A1 publication Critical patent/FR2297326A1/fr
Application granted granted Critical
Publication of FR2297326B1 publication Critical patent/FR2297326B1/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/12Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Catching Or Destruction (AREA)
FR7501206A 1975-01-09 1975-01-09 Perfectionnements aux tuyeres a geometrie variable pour propulseurs a reaction Granted FR2297326A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7501206A FR2297326A1 (fr) 1975-01-09 1975-01-09 Perfectionnements aux tuyeres a geometrie variable pour propulseurs a reaction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7501206A FR2297326A1 (fr) 1975-01-09 1975-01-09 Perfectionnements aux tuyeres a geometrie variable pour propulseurs a reaction

Publications (2)

Publication Number Publication Date
FR2297326A1 true FR2297326A1 (fr) 1976-08-06
FR2297326B1 FR2297326B1 (OSRAM) 1977-07-15

Family

ID=9149859

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7501206A Granted FR2297326A1 (fr) 1975-01-09 1975-01-09 Perfectionnements aux tuyeres a geometrie variable pour propulseurs a reaction

Country Status (1)

Country Link
FR (1) FR2297326A1 (OSRAM)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2653176A1 (fr) * 1989-10-12 1991-04-19 Gen Electric Dispositif d'actionnement pour la mise en place d'une tuyere d'echappement pouvant etre vectorisee.

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2653176A1 (fr) * 1989-10-12 1991-04-19 Gen Electric Dispositif d'actionnement pour la mise en place d'une tuyere d'echappement pouvant etre vectorisee.

Also Published As

Publication number Publication date
FR2297326B1 (OSRAM) 1977-07-15

Similar Documents

Publication Publication Date Title
GB1456280A (en) Variable area exhaust nozzle assemblies
GB881513A (en) Improvements relating to turbo-jet propulsion units in aircraft
GB871265A (en) Improvements relating to variable-area jet nozzles of turbojet engines
GB1009777A (en) Supersonic jet propulsion nozzle
GB1533986A (en) Nozzles for gas turbine engines
GB1100099A (en) Improvements in convergent-divergent jet exhaust nozzle for supersonic aircraft
GB1019857A (en) Jet propulsion nozzle assembly
BR8004978A (pt) Conjunto de bocais para tear com injecao a jato
GB1435946A (en) Efflux conduits for aircraft jet propulsion engines
GB1073278A (en) Improvements in or relating to propulsion nozzles
US2657575A (en) Asymmetric adjustable supersonic nozzle
FR2297326A1 (fr) Perfectionnements aux tuyeres a geometrie variable pour propulseurs a reaction
US3564934A (en) Link mechanism
FR2344720A2 (fr) Perfectionnement aux tuyeres de turbomachines
GB1387160A (en) Exhaust nozzles for jet propulsion engines for supersonic aircraft or vehicles
GB865881A (en) Means for actuating a variable area jet propulsion nozzle
GB1435567A (en) Vertical take-off and landing aircraft
GB951130A (en) Improvements relating to jet engines
GB1183893A (en) Nozzles having Silencing Means
GB1038854A (en) Nozzle assembly for a jet propulsion engine
GB895331A (en) Improvements in or relating to jet propulsion nozzles
GB1303875A (OSRAM)
GB871274A (en) Variable-shape jet propulsion nozzle
GB984955A (en) Nozzle for a jet engine
FR2257789A1 (en) Propulsive unit for missile - has jet and rocket with coaxial discharges axially displaced from each other

Legal Events

Date Code Title Description
ST Notification of lapse