FR1092654A - Improvements to aircraft jet propulsion units and installations - Google Patents

Improvements to aircraft jet propulsion units and installations

Info

Publication number
FR1092654A
FR1092654A FR1092654DA FR1092654A FR 1092654 A FR1092654 A FR 1092654A FR 1092654D A FR1092654D A FR 1092654DA FR 1092654 A FR1092654 A FR 1092654A
Authority
FR
France
Prior art keywords
installations
jet propulsion
propulsion units
aircraft jet
aircraft
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.)
Expired
Application number
Other languages
French (fr)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1092654A publication Critical patent/FR1092654A/en
Expired legal-status Critical Current

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
FR1092654D 1952-11-25 1953-11-24 Improvements to aircraft jet propulsion units and installations Expired FR1092654A (en)

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
FR1092654A true FR1092654A (en) 1955-04-26

Family

ID=10298492

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1092654D Expired FR1092654A (en) 1952-11-25 1953-11-24 Improvements to aircraft jet propulsion units and installations

Country Status (4)

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

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2847823A (en) * 1955-03-15 1958-08-19 Curtiss Wright Corp Reverse thrust nozzle construction
US2874538A (en) * 1957-03-22 1959-02-24 Marquardt Aircraft Company Thrust reverser for jet engine
DE1054848B (en) * 1956-04-27 1959-04-09 Armstrong Siddeley Motors Ltd Device for thrust reversal in a jet engine of an aircraft
US2931171A (en) * 1955-04-19 1960-04-05 United Aircraft Corp Combination noise suppressor and thrust reverser
US2933890A (en) * 1955-01-20 1960-04-26 Boeing Co Nozzle closing jet deflectors
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
US2996881A (en) * 1956-11-09 1961-08-22 Gen Motors Corp Jet thrust reversing and afterburner means
US3002343A (en) * 1956-10-29 1961-10-03 Aerojet General Co Thrust-reversing mechanism for jet aircraft
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US3027714A (en) * 1959-06-11 1962-04-03 Canadair Ltd Combined thrust reversing and noise suppressing device for turbo-jet engines
US3032981A (en) * 1957-02-11 1962-05-08 Boeing Co Noise suppressor and thrust reverser for jet engine nozzles
US3036431A (en) * 1959-09-08 1962-05-29 Boeing Co Thrust reverser for jet engines
US3041829A (en) * 1958-06-05 1962-07-03 Snecma Improvements to jet deflecting devices, particularly for discharge nozzles of propulsion units
US3059426A (en) * 1957-03-22 1962-10-23 Marquardt Corp Thrust reverser utilizing aft end mechanical blockage
DE1187491B (en) * 1960-03-07 1965-02-18 Moteuers D Aviat Soc Nat D Etu Flow channel with ring-shaped cross-section and lateral beam deflection openings

Families Citing this family (11)

* 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
US3113428A (en) * 1957-03-13 1963-12-10 Rolls Royce Silenced jet propulsion nozzle with thrust reversing means
US2976681A (en) * 1957-09-17 1961-03-28 Boeing Co Clam shell thrust reversers with noise suppressors
US3050937A (en) * 1958-06-09 1962-08-28 Boeing Co Reversible thrust jet engines and controls therefor
US3262269A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3262268A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
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 (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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 (en) * 1956-04-27 1959-04-09 Armstrong Siddeley Motors Ltd Device for thrust reversal in a jet engine of an aircraft
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
US2874538A (en) * 1957-03-22 1959-02-24 Marquardt Aircraft Company Thrust reverser for jet engine
US3059426A (en) * 1957-03-22 1962-10-23 Marquardt Corp Thrust reverser utilizing aft end mechanical blockage
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US3041829A (en) * 1958-06-05 1962-07-03 Snecma Improvements to jet deflecting devices, particularly for discharge nozzles of propulsion units
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 (en) * 1960-03-07 1965-02-18 Moteuers D Aviat Soc Nat D Etu Flow channel with ring-shaped cross-section and lateral beam deflection openings

Also Published As

Publication number Publication date
CH320188A (en) 1957-03-15
GB764907A (en) 1957-01-02
BE524592A (en)

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