IT994347B - Combinazione di un ugello variabile a valve di bloccaggio ed a spinta reversibile - Google Patents

Combinazione di un ugello variabile a valve di bloccaggio ed a spinta reversibile

Info

Publication number
IT994347B
IT994347B IT52792/73A IT5279273A IT994347B IT 994347 B IT994347 B IT 994347B IT 52792/73 A IT52792/73 A IT 52792/73A IT 5279273 A IT5279273 A IT 5279273A IT 994347 B IT994347 B IT 994347B
Authority
IT
Italy
Prior art keywords
combination
variable nozzle
locking valve
reversible thrust
reversible
Prior art date
Application number
IT52792/73A
Other languages
English (en)
Original Assignee
Boeing Co
Aeritalia Spa
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 Boeing Co, Aeritalia Spa filed Critical Boeing Co
Application granted granted Critical
Publication of IT994347B publication Critical patent/IT994347B/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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Exhaust Silencers (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
IT52792/73A 1972-12-26 1973-09-27 Combinazione di un ugello variabile a valve di bloccaggio ed a spinta reversibile IT994347B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US31790872A 1972-12-26 1972-12-26

Publications (1)

Publication Number Publication Date
IT994347B true IT994347B (it) 1975-10-20

Family

ID=23235777

Family Applications (1)

Application Number Title Priority Date Filing Date
IT52792/73A IT994347B (it) 1972-12-26 1973-09-27 Combinazione di un ugello variabile a valve di bloccaggio ed a spinta reversibile

Country Status (6)

Country Link
US (1) US3791586A (it)
JP (1) JPS5419930B2 (it)
DE (1) DE2360442C3 (it)
FR (1) FR2211595B1 (it)
GB (1) GB1448245A (it)
IT (1) IT994347B (it)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3877663A (en) * 1973-11-19 1975-04-15 Aeritalia Spa Translating splitter variable area nozzle and reverser
US3893640A (en) * 1973-11-27 1975-07-08 Gen Electric Sound suppressing nacelle arrangement
US3863867A (en) * 1973-12-26 1975-02-04 Boeing Co Thrust control apparatus for a jet propulsion engine and actuating mechanism therefor
US3915415A (en) * 1974-03-21 1975-10-28 Rohr Industries Inc Overwing thrust reverser
US3981463A (en) * 1974-03-21 1976-09-21 Rohr Industries, Inc. Overwing thrust reverser
US3997134A (en) * 1975-03-27 1976-12-14 The Boeing Company Fuselage tail jet engine thrust reverser
USRE31591E (en) * 1975-03-27 1984-05-29 The Boeing Company Fuselage tail jet engine thrust reverser and method
US4183478A (en) * 1977-11-25 1980-01-15 The Boeing Company Jet thrust reverser
FR2494775B1 (fr) * 1980-11-27 1985-07-05 Astech Dispositif pour la commande d'un inverseur de poussee pour moteur a reaction
US4579039A (en) * 1983-12-12 1986-04-01 Sundstrand Corporation Power drive unit
DE102008022289B4 (de) * 2008-04-25 2010-07-29 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugkörper
WO2020245513A1 (fr) * 2019-06-07 2020-12-10 Zipair Groupe de poussée pour dispositif de propulsion et dispositif de propulsion associe

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB820059A (en) * 1956-07-30 1959-09-16 Bristol Aero Engines Ltd Improvements in or relating to jet propulsion nozzles
US3080711A (en) * 1960-01-06 1963-03-12 James F Connors Penshape exhaust nozzle for supersonic engine
US3667680A (en) * 1970-04-24 1972-06-06 Boeing Co Jet engine exhaust nozzle system

Also Published As

Publication number Publication date
US3791586A (en) 1974-02-12
DE2360442A1 (de) 1974-07-11
GB1448245A (en) 1976-09-02
FR2211595A1 (it) 1974-07-19
JPS5419930B2 (it) 1979-07-19
DE2360442C3 (de) 1978-09-28
JPS49100799A (it) 1974-09-24
DE2360442B2 (de) 1978-02-02
FR2211595B1 (it) 1976-06-25

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