FR2569232B1 - Tuyere d'echappement orientable pour turbomachine a gaz - Google Patents
Tuyere d'echappement orientable pour turbomachine a gazInfo
- 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
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
- F02K1/002—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
- F02K1/004—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 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)
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)
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)
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 |
-
1984
- 1984-08-16 GB GB08420799A patent/GB2163105B/en not_active Expired
-
1985
- 1985-07-31 US US06/760,767 patent/US4679732A/en not_active Expired - Lifetime
- 1985-08-13 DE DE19853528989 patent/DE3528989A1/de not_active Withdrawn
- 1985-08-13 IT IT21926/85A patent/IT1184821B/it active
- 1985-08-14 FR FR858512372A patent/FR2569232B1/fr not_active Expired - Fee Related
- 1985-08-15 JP JP60178693A patent/JPS6158958A/ja active Pending
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 |