CH320188A - Rückstosstriebwerk in einem Flugzeug - Google Patents

Rückstosstriebwerk in einem Flugzeug

Info

Publication number
CH320188A
CH320188A CH320188DA CH320188A CH 320188 A CH320188 A CH 320188A CH 320188D A CH320188D A CH 320188DA CH 320188 A CH320188 A CH 320188A
Authority
CH
Switzerland
Prior art keywords
airplane
recoil engine
recoil
engine
Prior art date
Application number
Other languages
German (de)
English (en)
Inventor
George Elliott Albert
Pearson Harry
Fawn Geoffrey
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH320188A publication Critical patent/CH320188A/de

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
    • F02K1/62—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
    • F02K1/56—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Braking Arrangements (AREA)
  • Wind Motors (AREA)
CH320188D 1952-11-25 1953-11-25 Rückstosstriebwerk in einem Flugzeug CH320188A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2986852A GB764907A (en) 1952-11-25 1952-11-25 Improvements in or relating to aircraft reaction propulsion units and installations

Publications (1)

Publication Number Publication Date
CH320188A true CH320188A (de) 1957-03-15

Family

ID=10298492

Family Applications (1)

Application Number Title Priority Date Filing Date
CH320188D CH320188A (de) 1952-11-25 1953-11-25 Rückstosstriebwerk in einem Flugzeug

Country Status (4)

Country Link
BE (1) BE524592A (fr)
CH (1) CH320188A (fr)
FR (1) FR1092654A (fr)
GB (1) GB764907A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1287444B (de) * 1965-06-07 1969-01-16 Gen Electric Schubumkehrvorrichtung fuer ein Mantelstromstrahltriebwerk
DE1456037B1 (de) * 1965-06-07 1970-10-01 Gen Electric Schubumkehreinrichtung für ein Strahltriebwerk

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2929204A (en) * 1954-10-01 1960-03-22 Gen Electric Jet spoiler and reverser
US2950595A (en) * 1954-11-01 1960-08-30 Marquardt Corp Thrust reverser
US2933890A (en) * 1955-01-20 1960-04-26 Boeing Co Nozzle closing jet deflectors
US2847823A (en) * 1955-03-15 1958-08-19 Curtiss Wright Corp Reverse thrust nozzle construction
US2931171A (en) * 1955-04-19 1960-04-05 United Aircraft Corp Combination noise suppressor and thrust reverser
US2944395A (en) * 1955-06-06 1960-07-12 Doak Aircraft Co Inc Means and methods of neutralizing and converting thrust components
US2954668A (en) * 1956-03-12 1960-10-04 Rohr Aircraft Corp Brake for jet airplane
DE1054848B (de) * 1956-04-27 1959-04-09 Armstrong Siddeley Motors Ltd Vorrichtung zur Schubumkehr bei einem Strahltriebwerk eines Flugzeugs
US3002343A (en) * 1956-10-29 1961-10-03 Aerojet General Co Thrust-reversing mechanism for jet aircraft
US2996881A (en) * 1956-11-09 1961-08-22 Gen Motors Corp Jet thrust reversing and afterburner means
US3032981A (en) * 1957-02-11 1962-05-08 Boeing Co Noise suppressor and thrust reverser for jet engine nozzles
US3113428A (en) * 1957-03-13 1963-12-10 Rolls Royce Silenced jet propulsion nozzle with thrust reversing means
US3059426A (en) * 1957-03-22 1962-10-23 Marquardt Corp Thrust reverser utilizing aft end mechanical blockage
US2874538A (en) * 1957-03-22 1959-02-24 Marquardt Aircraft Company Thrust reverser for jet engine
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US2976681A (en) * 1957-09-17 1961-03-28 Boeing Co Clam shell thrust reversers with noise suppressors
FR1198179A (fr) * 1958-06-05 1959-12-04 Snecma Perfectionnements aux déviateurs de jet
US3050937A (en) * 1958-06-09 1962-08-28 Boeing Co Reversible thrust jet engines and controls therefor
US3027714A (en) * 1959-06-11 1962-04-03 Canadair Ltd Combined thrust reversing and noise suppressing device for turbo-jet engines
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
DE1187491B (de) * 1960-03-07 1965-02-18 Moteuers D Aviat Soc Nat D Etu Stroemungskanal mit ringfoermigem Querschnitt und seitlichen Strahlumlenkungsoeffnungen
US3500644A (en) * 1968-04-10 1970-03-17 Rohr Corp Thrust reverser
US3814324A (en) * 1972-06-19 1974-06-04 Gen Electric Propulsion nozzle and actuator system employed therein
US20160305370A1 (en) * 2015-04-16 2016-10-20 Honeywell International Inc. Translating cowl thrust reverser with door pivots aft of reverse flow path
US10563614B2 (en) 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1287444B (de) * 1965-06-07 1969-01-16 Gen Electric Schubumkehrvorrichtung fuer ein Mantelstromstrahltriebwerk
DE1456037B1 (de) * 1965-06-07 1970-10-01 Gen Electric Schubumkehreinrichtung für ein Strahltriebwerk

Also Published As

Publication number Publication date
FR1092654A (fr) 1955-04-26
BE524592A (fr)
GB764907A (en) 1957-01-02

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