IT972637B - Turboreattore con ugello di sca rico regolabile convergente diver gente - Google Patents

Turboreattore con ugello di sca rico regolabile convergente diver gente

Info

Publication number
IT972637B
IT972637B IT3325272A IT3325272A IT972637B IT 972637 B IT972637 B IT 972637B IT 3325272 A IT3325272 A IT 3325272A IT 3325272 A IT3325272 A IT 3325272A IT 972637 B IT972637 B IT 972637B
Authority
IT
Italy
Prior art keywords
turboreactor
diver
people
exhaust nozzle
convergent exhaust
Prior art date
Application number
IT3325272A
Other languages
English (en)
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of IT972637B publication Critical patent/IT972637B/it

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)
IT3325272A 1971-12-20 1972-12-20 Turboreattore con ugello di sca rico regolabile convergente diver gente IT972637B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US20966571A 1971-12-20 1971-12-20

Publications (1)

Publication Number Publication Date
IT972637B true IT972637B (it) 1974-05-31

Family

ID=22779734

Family Applications (1)

Application Number Title Priority Date Filing Date
IT3325272A IT972637B (it) 1971-12-20 1972-12-20 Turboreattore con ugello di sca rico regolabile convergente diver gente

Country Status (8)

Country Link
JP (1) JPS5754614B2 (it)
AU (1) AU470247B2 (it)
CA (1) CA961652A (it)
DE (1) DE2254719C3 (it)
FR (1) FR2164594B1 (it)
GB (1) GB1372330A (it)
IT (1) IT972637B (it)
SE (1) SE374171B (it)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3979065A (en) * 1974-10-31 1976-09-07 United Technologies Corporation Cooling liner for an exhaust nozzle
US4375276A (en) * 1980-06-02 1983-03-01 General Electric Company Variable geometry exhaust nozzle
FR2724977B1 (fr) * 1980-12-30 1996-12-13 Snecma Tuyere convergente-divergente en particulier pour turboreacteur
CN115614179B (zh) * 2022-08-31 2024-04-05 中国航发四川燃气涡轮研究院 喉道面积的调节机构

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049875A (en) * 1952-08-15 1962-08-21 United Aircraft Corp Variable flap plug type nozzle
FR1215236A (fr) * 1958-11-12 1960-04-15 Snecma Tuyère réglable et propulseur à réaction équipé d'une telle tuyère
US3046730A (en) * 1960-09-21 1962-07-31 Marquardt Corp Variable area exit nozzle
US3454227A (en) * 1966-08-19 1969-07-08 United Aircraft Corp Free floating articulate ejector nozzle
FR2030532A5 (it) * 1969-07-03 1970-11-13 Snecma

Also Published As

Publication number Publication date
JPS5754614B2 (it) 1982-11-19
AU470247B2 (en) 1976-03-11
FR2164594A1 (it) 1973-08-03
AU4878772A (en) 1974-05-23
DE2254719B2 (de) 1981-06-25
JPS4869300A (it) 1973-09-20
CA961652A (en) 1975-01-28
DE2254719A1 (de) 1973-06-28
GB1372330A (en) 1974-10-30
SE374171B (it) 1975-02-24
DE2254719C3 (de) 1982-02-04
FR2164594B1 (it) 1977-04-08

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