GB755019A - Improvements in or relating to jet-propelled aircraft - Google Patents

Improvements in or relating to jet-propelled aircraft

Info

Publication number
GB755019A
GB755019A GB25019/53A GB2501953A GB755019A GB 755019 A GB755019 A GB 755019A GB 25019/53 A GB25019/53 A GB 25019/53A GB 2501953 A GB2501953 A GB 2501953A GB 755019 A GB755019 A GB 755019A
Authority
GB
United Kingdom
Prior art keywords
jet pipe
sept
casing
jet
joint
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
GB25019/53A
Inventor
Frederick William Walto Morley
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
Priority to GB25019/53A priority Critical patent/GB755019A/en
Publication of GB755019A publication Critical patent/GB755019A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/004Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/38Jet flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Nozzles (AREA)

Abstract

755,019. Jet propulsion plant. ROLLSROYCE, Ltd. Sept. 9, 1954 [Sept. 9, 1953], No. 25019/53. Class 110(3) [Also in Group XXXIII] An aircraft jet pipe having a directionally adjustable nozzle comprises a forward fixed part 11 and an adjustable rear part 9 connected by a joint which is in a plane at an angle to' a plane normal to the axis of the part 11. The forward part has an outer casing 12 spaced from an inner jet pipe 14 to which it is connected by tangential straps 26 which permit relative radial movement and a sliding joint 27 which permits relative axial movement. The rear part is similarly constructed with corresponding parts 13, 15, 28 and 29, and rotary gas-seals 19 and 24 are provided between the co-operating casing and jet pipe elements respectively. Part of the sealing structure for the casing carries a toothed ring 20 engaged by a pinion 21 driven by an electric motor 22, whereby the nozzle part 9 may be deflected from the position shown in which it is aligned with the forward part 11.
GB25019/53A 1953-09-09 1953-09-09 Improvements in or relating to jet-propelled aircraft Expired GB755019A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB25019/53A GB755019A (en) 1953-09-09 1953-09-09 Improvements in or relating to jet-propelled aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB25019/53A GB755019A (en) 1953-09-09 1953-09-09 Improvements in or relating to jet-propelled aircraft

Publications (1)

Publication Number Publication Date
GB755019A true GB755019A (en) 1956-08-15

Family

ID=10220907

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25019/53A Expired GB755019A (en) 1953-09-09 1953-09-09 Improvements in or relating to jet-propelled aircraft

Country Status (1)

Country Link
GB (1) GB755019A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2879014A (en) * 1957-07-02 1959-03-24 Bell Aircraft Corp Jet propelled airplane with jet diverter
US2986877A (en) * 1957-03-07 1961-06-06 Paul C Emmons Rotatable afterburners for jet aircraft
US3180087A (en) * 1960-10-21 1965-04-27 Bristol Siddeley Engines Ltd Jet propulsion engines
US3200586A (en) * 1961-06-05 1965-08-17 Kelsey Hayes Co Nozzle adjusting mechanism
US3206929A (en) * 1961-01-12 1965-09-21 Bristol Siddeley Engines Ltd Aircraft jet propulsion nozzles
US3260049A (en) * 1963-05-09 1966-07-12 Boeing Co Variable vectoring nozzle for jet propulsion engines
GB2282353A (en) * 1993-10-04 1995-04-05 Peter William Bishop Vectored thrust flight control
EP3181455A1 (en) * 2015-12-16 2017-06-21 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sections

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2986877A (en) * 1957-03-07 1961-06-06 Paul C Emmons Rotatable afterburners for jet aircraft
US2879014A (en) * 1957-07-02 1959-03-24 Bell Aircraft Corp Jet propelled airplane with jet diverter
US3180087A (en) * 1960-10-21 1965-04-27 Bristol Siddeley Engines Ltd Jet propulsion engines
US3206929A (en) * 1961-01-12 1965-09-21 Bristol Siddeley Engines Ltd Aircraft jet propulsion nozzles
US3200586A (en) * 1961-06-05 1965-08-17 Kelsey Hayes Co Nozzle adjusting mechanism
US3260049A (en) * 1963-05-09 1966-07-12 Boeing Co Variable vectoring nozzle for jet propulsion engines
GB2282353A (en) * 1993-10-04 1995-04-05 Peter William Bishop Vectored thrust flight control
GB2282353B (en) * 1993-10-04 1997-09-24 Peter William Bishop Flight control systems for aircraft
EP3181455A1 (en) * 2015-12-16 2017-06-21 AIRBUS HELICOPTERS DEUTSCHLAND GmbH An aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sections
CN106882392A (en) * 2015-12-16 2017-06-23 空客直升机德国有限公司 The aircraft of the exhaust of hot air part with the discharge section being pivotally mounted on including two
CN106882392B (en) * 2015-12-16 2019-09-03 空客直升机德国有限公司 Aircraft with the exhaust of hot air part for including two discharge sections being pivotally mounted on
US10527000B2 (en) 2015-12-16 2020-01-07 Airbus Helicopters Deutschland GmbH Aircraft with a hot air exhaust that comprises two pivotally mounted exhaust sections

Similar Documents

Publication Publication Date Title
GB881513A (en) Improvements relating to turbo-jet propulsion units in aircraft
GB1104764A (en) Improvements in thrust reverters for jet propulsion powerplants
GB582978A (en) Improvements in gas turbines
GB755019A (en) Improvements in or relating to jet-propelled aircraft
GB960106A (en) Jet propulsion engines with orientable jet nozzles
GB1139005A (en) Improvements in or relating to gas turbine by-pass engines
GB907741A (en) Improvements relating to rockets
GB586571A (en) Improvements in fluid jet nozzles, more particularly for internal combustion power acting wholly or in part by jet propulsion
GB1073458A (en) Improvements relating to by-pass ducted for gas-turbine aircraft engines
GB1375868A (en)
GB961001A (en) Improvements in propulsion units having a plurality of reaction propulsion nozzles
GB1140472A (en) Articulated structure especially for jet propulsion nozzle
GB1030521A (en) Mounting arrangement for gas turbine engines in aircraft
GB1357370A (en) Ducted fan gas turbine jet propulsion engine with thrust control means
GB1071075A (en) Improvements in aircraft
GB1003584A (en) Improvements in or relating to jet propulsion engines
GB1132157A (en) Improvements in movable nozzles for directing the thrust of jet-propelled aircraft
GB1324558A (en) Jet propulsion unit having a propellant gas jet deflector
GB1062839A (en) Improvements relating to thrust reversers
GB886201A (en) Jet noise silencer for an aircraft
GB888943A (en) Improvements in or relating to fan units
GB1024206A (en) Gas turbine engine with swivelling jet propulsion nozzle
GB770025A (en) Device for steering aircraft, rockets and the like, having a jet propelling nozzle
COMPAGNON A study of engine variable geometry systems for an advanced high subsonic long range commercial aircraft(Characteristics of variable geometry high Mach inlet concepts to reduce jet engine noise on subsonic, long range commercial aircraft)
GB1049688A (en) Improvements relating to aircraft provided with jet engines