FR1372176A - Oscillating Discharge Cone Nozzle for Gas Turbine Jet Engine - Google Patents

Oscillating Discharge Cone Nozzle for Gas Turbine Jet Engine

Info

Publication number
FR1372176A
FR1372176A FR949987A FR949987A FR1372176A FR 1372176 A FR1372176 A FR 1372176A FR 949987 A FR949987 A FR 949987A FR 949987 A FR949987 A FR 949987A FR 1372176 A FR1372176 A FR 1372176A
Authority
FR
France
Prior art keywords
gas turbine
jet engine
cone nozzle
discharge cone
turbine jet
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
FR949987A
Other languages
French (fr)
Inventor
James Oswald Mortlock
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 FR1372176A publication Critical patent/FR1372176A/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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041Aircraft 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
    • B64C29/0058Aircraft 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 vertical jet
    • 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
    • F02K1/78Other construction of jet pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR949987A 1962-10-08 1963-10-08 Oscillating Discharge Cone Nozzle for Gas Turbine Jet Engine Expired FR1372176A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3807762A GB948571A (en) 1962-10-08 1962-10-08 Gas turbine jet propulsion engine

Publications (1)

Publication Number Publication Date
FR1372176A true FR1372176A (en) 1964-09-11

Family

ID=10401015

Family Applications (1)

Application Number Title Priority Date Filing Date
FR949987A Expired FR1372176A (en) 1962-10-08 1963-10-08 Oscillating Discharge Cone Nozzle for Gas Turbine Jet Engine

Country Status (3)

Country Link
DE (1) DE1223626B (en)
FR (1) FR1372176A (en)
GB (1) GB948571A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4841726A (en) * 1985-11-19 1989-06-27 Mtu-Munchen Gmbh Gas turbine jet engine of multi-shaft double-flow construction

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3429509A (en) * 1967-05-31 1969-02-25 United Aircraft Corp Cooling scheme for a three bearing swivel nozzle
GB2379483A (en) * 2001-09-08 2003-03-12 Rolls Royce Plc Augmented gas turbine propulsion system
GB0504272D0 (en) 2005-03-02 2005-04-06 Rolls Royce Plc A turbine engine and a method of operating a turbine engine
US10563613B2 (en) * 2015-08-31 2020-02-18 Rolls-Royce North American Technologies Inc. Coanda device for a round exhaust nozzle

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2630673A (en) * 1950-09-27 1953-03-10 Gen Electric Cooling means for variable area nozzles
GB724004A (en) * 1952-04-29 1955-02-16 Rolls Royce Improvements in or relating to fuel supply arrangements for gas-turbine engines
FR1279495A (en) * 1960-11-10 1961-12-22 Snecma Jet deflection device for jet aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4841726A (en) * 1985-11-19 1989-06-27 Mtu-Munchen Gmbh Gas turbine jet engine of multi-shaft double-flow construction

Also Published As

Publication number Publication date
GB948571A (en) 1964-02-05
DE1223626B (en) 1966-08-25

Similar Documents

Publication Publication Date Title
FR1489735A (en) Safety device for supplying gas turbine engines
FR1097287A (en) Variable area nozzle enhancements for gas turbine jet engines
FR1018980A (en) Exhaust gas discharge section control device for jet engine
FR1372176A (en) Oscillating Discharge Cone Nozzle for Gas Turbine Jet Engine
CH401590A (en) Silent exhaust nozzle for jet thruster
FR1241897A (en) Device for removing moisture from a surface, applicable in particular to the air intake channel of a gas turbojet
FR1479351A (en) Jet Ejector Exhaust Nozzle
FR1247562A (en) Jet Nozzles for Jet Engines
FR1488151A (en) Gas turbine engine equipped with pneumatic starting device
FR1234975A (en) Exhaust cone for the exhaust nozzle of a gas turbine engine
FR1491861A (en) Supersonic Exhaust Converging-Diverging Nozzle for Jet Engine
FR1281740A (en) Expansion cone for the nozzle of a rocket engine
FR1192234A (en) Exhaust thrust reverser for jet engines
FR1439930A (en) Gas generator for jet engine
FR1006128A (en) Fuel and combustion device for gas turbines and turbo-reactors
FR1307016A (en) Starter nozzle for gas turbine
FR1496107A (en) Variable section intake guide ring for gas turbines
FR1494511A (en) Diverging-converging exhaust nozzle for jet engines
FR1368570A (en) Support of the downstream end of the combustion chamber of a gas turbo-engine
FR1420095A (en) Hand starter for gas turbine
FR1066674A (en) Improvement in starting a gas turbine vehicle
FR1367076A (en) Gas exhaust nozzle for turbo-reactors
FR1358266A (en) Drive mechanism of auxiliary devices for gas turbine engine
FR1441182A (en) Supersonic air inlet for gas turbine engine
FR1319068A (en) Combustion chamber of a gas turbo-engine