GB1550633A - Thrust-vectoring gas turbine engine exhaust nozzles - Google Patents

Thrust-vectoring gas turbine engine exhaust nozzles

Info

Publication number
GB1550633A
GB1550633A GB3035476A GB3035476A GB1550633A GB 1550633 A GB1550633 A GB 1550633A GB 3035476 A GB3035476 A GB 3035476A GB 3035476 A GB3035476 A GB 3035476A GB 1550633 A GB1550633 A GB 1550633A
Authority
GB
United Kingdom
Prior art keywords
vectoring
thrust
gas turbine
turbine engine
engine exhaust
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
GB3035476A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Priority to GB3035476A priority Critical patent/GB1550633A/en
Publication of GB1550633A publication Critical patent/GB1550633A/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1215—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure, and the downstream series having its flaps hinged at their downstream ends on a fixed structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
    • 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
    • F02K1/002—Plants 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
    • F02K1/006—Plants 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 within one plane only
GB3035476A 1976-07-21 1976-07-21 Thrust-vectoring gas turbine engine exhaust nozzles Expired GB1550633A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3035476A GB1550633A (en) 1976-07-21 1976-07-21 Thrust-vectoring gas turbine engine exhaust nozzles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3035476A GB1550633A (en) 1976-07-21 1976-07-21 Thrust-vectoring gas turbine engine exhaust nozzles

Publications (1)

Publication Number Publication Date
GB1550633A true GB1550633A (en) 1979-08-15

Family

ID=10306331

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3035476A Expired GB1550633A (en) 1976-07-21 1976-07-21 Thrust-vectoring gas turbine engine exhaust nozzles

Country Status (1)

Country Link
GB (1) GB1550633A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2132279A (en) * 1982-12-27 1984-07-04 United Technologies Corp Cooled exhaust nozzle flaps
EP0118181A1 (en) * 1983-01-31 1984-09-12 Fuji Jukogyo Kabushiki Kaisha Device for increasing and deflecting thrust of jet-propulsion engine of V/STOL aircraft
US4660767A (en) * 1984-08-16 1987-04-28 Rolls-Royce Vectorable exhaust nozzle for gas turbine engines
WO1990008254A1 (en) * 1989-01-19 1990-07-26 Mtu Motoren- Und Turbinen Union München Gmbh Propelling nozzle
EP1348835A3 (en) * 2002-03-27 2005-08-17 United Technologies Corporation Valve assembly for gas turbine engine
CN112539117A (en) * 2020-11-12 2021-03-23 太原科技大学 High-temperature heat insulation mechanism of multidirectional swing rail control engine

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2132279A (en) * 1982-12-27 1984-07-04 United Technologies Corp Cooled exhaust nozzle flaps
EP0118181A1 (en) * 1983-01-31 1984-09-12 Fuji Jukogyo Kabushiki Kaisha Device for increasing and deflecting thrust of jet-propulsion engine of V/STOL aircraft
US4660767A (en) * 1984-08-16 1987-04-28 Rolls-Royce Vectorable exhaust nozzle for gas turbine engines
US5186390A (en) * 1989-01-16 1993-02-16 Mtu Motoren-Und Turbinen-Union Munchen Gmbh Propelling nozzle
WO1990008254A1 (en) * 1989-01-19 1990-07-26 Mtu Motoren- Und Turbinen Union München Gmbh Propelling nozzle
EP1348835A3 (en) * 2002-03-27 2005-08-17 United Technologies Corporation Valve assembly for gas turbine engine
CN112539117A (en) * 2020-11-12 2021-03-23 太原科技大学 High-temperature heat insulation mechanism of multidirectional swing rail control engine
CN112539117B (en) * 2020-11-12 2022-07-08 太原科技大学 High-temperature heat insulation mechanism of multidirectional swing rail control engine

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee