FR2569232B1 - Tuyere d'echappement orientable pour turbomachine a gaz - Google Patents

Tuyere d'echappement orientable pour turbomachine a gaz

Info

Publication number
FR2569232B1
FR2569232B1 FR858512372A FR8512372A FR2569232B1 FR 2569232 B1 FR2569232 B1 FR 2569232B1 FR 858512372 A FR858512372 A FR 858512372A FR 8512372 A FR8512372 A FR 8512372A FR 2569232 B1 FR2569232 B1 FR 2569232B1
Authority
FR
France
Prior art keywords
exhaust nozzle
adjustable exhaust
gas turbomachine
turbomachine
gas
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 - Fee Related
Application number
FR858512372A
Other languages
English (en)
Other versions
FR2569232A1 (fr
Inventor
Clifford Stanley Woodward
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
Publication of FR2569232A1 publication Critical patent/FR2569232A1/fr
Application granted granted Critical
Publication of FR2569232B1 publication Critical patent/FR2569232B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR858512372A 1984-08-16 1985-08-14 Tuyere d'echappement orientable pour turbomachine a gaz Expired - Fee Related FR2569232B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08420799A GB2163105B (en) 1984-08-16 1984-08-16 Vectorable exhaust nozzle for gas turbine engine

Publications (2)

Publication Number Publication Date
FR2569232A1 FR2569232A1 (fr) 1986-02-21
FR2569232B1 true FR2569232B1 (fr) 1990-08-03

Family

ID=10565409

Family Applications (1)

Application Number Title Priority Date Filing Date
FR858512372A Expired - Fee Related FR2569232B1 (fr) 1984-08-16 1985-08-14 Tuyere d'echappement orientable pour turbomachine a gaz

Country Status (6)

Country Link
US (1) US4679732A (fr)
JP (1) JPS6158958A (fr)
DE (1) DE3528989A1 (fr)
FR (1) FR2569232B1 (fr)
GB (1) GB2163105B (fr)
IT (1) IT1184821B (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5323606A (en) * 1993-02-23 1994-06-28 Rolls-Royce Plc Stowable nozzle
GB2281262B (en) * 1993-08-27 1997-04-16 Rolls Royce Plc Stowable nozzle
US20080061172A1 (en) 2006-09-12 2008-03-13 Trapp James M High pressure monitor
US7137578B2 (en) * 2003-12-26 2006-11-21 Task Force Tips, Inc. Segmented monitor
GB2419166A (en) 2004-10-14 2006-04-19 Rolls Royce Plc Retaining washer for threaded fasteners
GB2431142B (en) * 2005-10-12 2007-09-12 Rolls Royce Plc Actuator for a gas turbine engine vectorable nozzle
US8944346B2 (en) * 2010-01-04 2015-02-03 Akron Brass Company Rotatable flange for a water monitor
US8960592B1 (en) 2011-07-19 2015-02-24 D. Anthony Windisch VTOL propulsion for aircraft
US8678022B2 (en) 2012-06-22 2014-03-25 Akron Brass Co. Positionable outlet for a water monitor
US9883634B2 (en) * 2012-09-13 2018-02-06 Franco Romito Attachment for air blower
EP3181455B1 (fr) 2015-12-16 2019-04-17 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Avion avec une sortie d'air chaud qui comprend deux sections d'échappement montées de manière pivotante
CN107200113B (zh) * 2017-05-22 2019-04-12 哈尔滨工程大学 多环节矢量推进喷口装置
CN109184948B (zh) * 2018-10-11 2020-05-22 西北工业大学 一种用于短距或垂直起降飞行器的转向喷管
CN110641713A (zh) * 2019-10-31 2020-01-03 万勇 一种喷气式无人机的旋转喷嘴
US11661183B2 (en) 2020-03-16 2023-05-30 D. Anthony Windisch Small light vertical take-off and landing capable delta wing aircraft

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL91723C (fr) * 1952-10-23
DE1066428B (fr) * 1959-01-17
DE1210329B (de) * 1961-09-14 1966-02-03 Rolls Royce Strahlrohr, insbesondere fuer Flugzeugtriebwerke
DE1260318B (de) * 1965-10-29 1968-02-01 Entwicklungsring Sued G M B H Strahlrohr mit mehreren hintereinander angeordneten und gegeneinander verdrehbaren Rohrabschnitten
GB1108622A (en) * 1966-02-25 1968-04-03 Rolls Royce Improvements relating to jet pipes
DE1481606A1 (de) * 1966-03-03 1970-01-22 Man Turbo Gmbh Vorrichtung zur Betaetigung einer aus drei um ihre Laengsachsen gegeneinander verdrehbaren Rohrabschnitten bestehenden Strahlablenkvorrichtung
GB1122760A (en) * 1966-11-29 1968-08-07 Rolls Royce Improvements relating to jet pipes
DE1481546A1 (de) * 1967-03-14 1969-02-20 Entwicklungsring Sued Gmbh Insbesondere fuer VTOL- und STOL-Flugzeuge bestimmte schwenkbare Schubduese
US3480236A (en) * 1967-09-05 1969-11-25 Gen Electric Thrust vectoring exhaust system
US3485450A (en) * 1967-12-19 1969-12-23 United Aircraft Corp Planetary gear system drive mechanism
US3687374A (en) * 1970-07-02 1972-08-29 Gen Electric Swivelable jet nozzle
DE2056088C2 (de) * 1970-11-14 1975-10-23 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Strahlrohr, für den Antrieb von Fahrzeugen <·
GB1381397A (en) * 1971-02-26 1975-01-22 Mtu Muenchen Gmbh Jet pipe arrangement for a jet-propulsion engine
US3989193A (en) * 1974-03-02 1976-11-02 Motoren- Und Turbinen-Union Munchen Gmbh M.A.N. Maybach Mercedes-Benz Device for varying the gas exit area of an exhaust nozzle for a jet deflecting device
GB1499887A (en) * 1974-03-02 1978-02-01 Mtu Muenchen Gmbh Device for varying the gas exit area of an exhaust nozzle in a jet deflecting device
US4000854A (en) * 1975-10-02 1977-01-04 General Electric Company Thrust vectorable exhaust nozzle
US4550877A (en) * 1982-08-03 1985-11-05 Rolls-Royce Inc. Streamlined nozzle for turbomachines

Also Published As

Publication number Publication date
GB2163105B (en) 1988-02-10
FR2569232A1 (fr) 1986-02-21
JPS6158958A (ja) 1986-03-26
IT1184821B (it) 1987-10-28
US4679732A (en) 1987-07-14
GB2163105A (en) 1986-02-19
IT8521926A0 (it) 1985-08-13
DE3528989A1 (de) 1986-03-27

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Legal Events

Date Code Title Description
ST Notification of lapse