GB764907A - Improvements in or relating to aircraft reaction propulsion units and installations - Google Patents

Improvements in or relating to aircraft reaction propulsion units and installations

Info

Publication number
GB764907A
GB764907A GB2986852A GB2986852A GB764907A GB 764907 A GB764907 A GB 764907A GB 2986852 A GB2986852 A GB 2986852A GB 2986852 A GB2986852 A GB 2986852A GB 764907 A GB764907 A GB 764907A
Authority
GB
United Kingdom
Prior art keywords
valve
jet
jet pipe
gases
flow
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
GB2986852A
Inventor
Albert George Elliott
Harry Pearson
Geoffrey Fawn
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
Priority to BE524592D priority Critical patent/BE524592A/xx
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB2986852A priority patent/GB764907A/en
Priority to FR1092654D priority patent/FR1092654A/en
Priority to CH320188D priority patent/CH320188A/en
Publication of GB764907A publication Critical patent/GB764907A/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

Abstract

764,907. Controlling jet-propelled aircraft. ROLLS-ROYCE, Ltd. Nov. 17, 1953 [Nov. 25. 1952], No. 29868/52. Class 4. [Also in Group XXVI] A jet propulsion plant is mounted in a wing nacelle 10 and the jet pipe 11 terminates at its rear end in a portion 12 movable axially by pneumatically-operated jacks 14 mounted within the nacelle 10 and having piston rods 15 connected to a fairing structure 16 secured externally of the portion 12. The piston rods 15 extend through tubular mounting struts 17 which support a series of axially-spaced annular dished-section guide vanes 18. A butterfly valve 19 is mounted within the portion 12 on a pivot 20 which carries a spring-loaded arm 22 connected to one end of a link rod 23. The other end of the link has a stop 25 which abuts a guide block 24 when the portion 12 is in the position shown to cause the valve 19 to close the rear end of the jet pipe and cause the gases to flow through the ducts exposed by the portion 12 when in its rearward position, the gases being deflected forwardly to provide a braking effect on the aircraft. When the jacks 14 are operated to move the portion 12 against the rear end of the pipe 11 the lateral ducts are blanked off and the valve 19 is opened to permit rearward flow of the gases. The valve 19 is mounted on an off-centre pivot so that the flow of gas holds it open. In a further embodiment, Figs. 3-6 (not shown), the jet pipe 11 extends rearwardly to a propelling nozzle and it is provided with diametrically opposed ports closed by slide valves, the ports being on the inner ends of forwardly inclined ducts which extend to further ports in the outer surface of the nacelle fairing opened and closed by hinged flaps operated by further jacks, vanes such as vanes 18 being used for deflection of the gases. The end of the jet pipe is provided with opposed hinged shutters to close the nozzle and in a still further embodiment, Fig. 7 (not shown), these shutters may be associated with a valve such as valve 19. Provision is made for a flow of cooling air around the jet pipe such air being passed through the slide valves and opposed hinged shutters, which are double skinned for this purpose, when jet deflection is not taking place.
GB2986852A 1952-11-25 1952-11-25 Improvements in or relating to aircraft reaction propulsion units and installations Expired GB764907A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BE524592D BE524592A (en) 1952-11-25
GB2986852A GB764907A (en) 1952-11-25 1952-11-25 Improvements in or relating to aircraft reaction propulsion units and installations
FR1092654D FR1092654A (en) 1952-11-25 1953-11-24 Improvements to aircraft jet propulsion units and installations
CH320188D CH320188A (en) 1952-11-25 1953-11-25 Recoil engine in an airplane

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
GB764907A true GB764907A (en) 1957-01-02

Family

ID=10298492

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2986852A Expired GB764907A (en) 1952-11-25 1952-11-25 Improvements in or relating to aircraft reaction 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 (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US3113428A (en) * 1957-03-13 1963-12-10 Rolls Royce Silenced jet propulsion nozzle with thrust reversing means
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
EP3081796A1 (en) * 2015-04-16 2016-10-19 Honeywell International Inc. Translating cowl thrust reverser with pivota blocker doors
US10563614B2 (en) 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system

Families Citing this family (20)

* 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 (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
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
FR1198179A (en) * 1958-06-05 1959-12-04 Snecma Improvements to jet deflectors
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
US3262269A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser
US3262268A (en) * 1965-06-07 1966-07-26 Gen Electric Thrust reverser

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
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
EP3081796A1 (en) * 2015-04-16 2016-10-19 Honeywell International Inc. Translating cowl thrust reverser with pivota blocker doors
US10563614B2 (en) 2016-08-17 2020-02-18 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system
US10859035B2 (en) 2016-08-17 2020-12-08 Honeywell International Inc. Composite translating cowl assembly for a thrust reverser system

Also Published As

Publication number Publication date
FR1092654A (en) 1955-04-26
BE524592A (en)
CH320188A (en) 1957-03-15

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