CH339498A - Device for reversing the thrust of a jet engine of an airplane - Google Patents

Device for reversing the thrust of a jet engine of an airplane

Info

Publication number
CH339498A
CH339498A CH339498DA CH339498A CH 339498 A CH339498 A CH 339498A CH 339498D A CH339498D A CH 339498DA CH 339498 A CH339498 A CH 339498A
Authority
CH
Switzerland
Prior art keywords
airplane
reversing
thrust
jet engine
jet
Prior art date
Application number
Other languages
French (fr)
Inventor
Sinclair Rainbow Horace
Original Assignee
Armstrong Siddeley Motors Ltd
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 Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Publication of CH339498A publication Critical patent/CH339498A/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/023—Aircraft characterised by the type or position of power plant of rocket type, e.g. for assisting taking-off or braking
    • 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
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • F02K1/625—Reversing jet main flow by blocking the rearward discharge by means of flaps the aft end of the engine cowling being movable to uncover openings for the reversed flow
    • 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
    • F02K1/76—Control or regulation of thrust reversers
CH339498D 1956-04-27 1957-04-26 Device for reversing the thrust of a jet engine of an airplane CH339498A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB339498X 1956-04-27

Publications (1)

Publication Number Publication Date
CH339498A true CH339498A (en) 1959-06-30

Family

ID=10359469

Family Applications (1)

Application Number Title Priority Date Filing Date
CH339498D CH339498A (en) 1956-04-27 1957-04-26 Device for reversing the thrust of a jet engine of an airplane

Country Status (4)

Country Link
BE (1) BE557040A (en)
CH (1) CH339498A (en)
FR (1) FR1187684A (en)
GB (1) GB806038A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2156004A (en) * 1984-03-15 1985-10-02 Gen Electric Thrust modulation device for a gas turbine engine
FR2679605A1 (en) * 1991-07-24 1993-01-29 Snecma TURBOJET DRIVE INVERTER PROVIDED WITH A SAFETY DEVICE INTEGRATED WITH THE HYDRAULIC CONTROL SYSTEM.

Also Published As

Publication number Publication date
BE557040A (en)
GB806038A (en) 1958-12-17
FR1187684A (en) 1959-09-15

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