IL115248A - Hydraulic failsafe system and method for an axisymmetric vectoring nozzle - Google Patents
Hydraulic failsafe system and method for an axisymmetric vectoring nozzleInfo
- Publication number
- IL115248A IL115248A IL11524895A IL11524895A IL115248A IL 115248 A IL115248 A IL 115248A IL 11524895 A IL11524895 A IL 11524895A IL 11524895 A IL11524895 A IL 11524895A IL 115248 A IL115248 A IL 115248A
- Authority
- IL
- Israel
- Prior art keywords
- vectoring nozzle
- failsafe system
- axisymmetric vectoring
- hydraulic
- hydraulic failsafe
- Prior art date
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
- F02K1/15—Control or regulation
-
- 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
- F02K1/008—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 in any rearward direction
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US31412494A | 1994-09-29 | 1994-09-29 |
Publications (2)
Publication Number | Publication Date |
---|---|
IL115248A0 IL115248A0 (en) | 1995-12-31 |
IL115248A true IL115248A (en) | 2000-07-16 |
Family
ID=23218663
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IL11524895A IL115248A (en) | 1994-09-29 | 1995-09-11 | Hydraulic failsafe system and method for an axisymmetric vectoring nozzle |
Country Status (6)
Country | Link |
---|---|
US (1) | US6142416A (xx) |
EP (1) | EP0704615B1 (xx) |
JP (1) | JP3694549B2 (xx) |
DE (1) | DE69524345T2 (xx) |
ES (1) | ES2168338T3 (xx) |
IL (1) | IL115248A (xx) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6195981B1 (en) | 1998-07-22 | 2001-03-06 | General Electric Company | Vectoring nozzle control system |
US6109021A (en) * | 1998-07-22 | 2000-08-29 | General Electric Company | Vectoring nozzle calibration |
ES2153300B1 (es) * | 1998-09-04 | 2001-07-16 | Turbo Propulsores Ind | Mecanismo de guiado para toberas orientables de geometria variable aplicables a turbinas de gas. |
US6240720B1 (en) * | 1999-09-09 | 2001-06-05 | General Electric Company | Hybrid-composite gas turbine exhaust nozzle compression link |
US6415599B1 (en) * | 2001-05-11 | 2002-07-09 | General Electric Company | Engine interface for axisymmetric vectoring nozzle |
US7032835B2 (en) * | 2004-01-28 | 2006-04-25 | United Technologies Corporation | Convergent/divergent nozzle with modulated cooling |
CN100523472C (zh) * | 2006-02-24 | 2009-08-05 | 同济大学 | 一种轴对称矢量喷管a9作动应急复位液压系统 |
CN100480500C (zh) * | 2006-02-24 | 2009-04-22 | 同济大学 | 一种轴对称矢量喷管a9/a8面积比失调防护液压系统 |
US8347601B2 (en) * | 2006-05-04 | 2013-01-08 | Volvo Aero Corporation | Device for pivoting at least one pivotable element in a gas turbine engine |
US8205454B2 (en) * | 2007-02-06 | 2012-06-26 | United Technologies Corporation | Convergent divergent nozzle with edge cooled divergent seals |
US7757477B2 (en) * | 2007-02-20 | 2010-07-20 | United Technologies Corporation | Convergent divergent nozzle with slot cooled nozzle liner |
US8029664B2 (en) | 2008-06-26 | 2011-10-04 | Hamilton Sundstrand Corporation | Wash filter with wash velocity control cone |
US8572986B2 (en) * | 2009-07-27 | 2013-11-05 | United Technologies Corporation | Retainer for suspended thermal protection elements in a gas turbine engine |
US8583294B2 (en) * | 2011-04-11 | 2013-11-12 | Hamilton Sundstrand Corporation | Actuation control system |
CN103291493B (zh) * | 2013-06-28 | 2015-10-28 | 上海交通大学 | 运动解耦的轴对称矢量喷管调节机构 |
CN103291494B (zh) * | 2013-07-02 | 2015-08-19 | 上海交通大学 | 运动解耦含有移动副的轴对称矢量喷管调节机构 |
US9488130B2 (en) | 2013-10-17 | 2016-11-08 | Honeywell International Inc. | Variable area fan nozzle systems with improved drive couplings |
CN103713531B (zh) * | 2013-12-06 | 2016-05-18 | 长安大学 | 一种航空发动机尾喷管喉部面积控制系统 |
FR3022592B1 (fr) * | 2014-06-23 | 2016-07-15 | Aircelle Sa | Procede de commande d’une tuyere a geometrie variable pour nacelle de turboreacteur |
CN106499543B (zh) * | 2016-09-26 | 2017-12-26 | 南京航空航天大学 | 一种排气喷管推力矢量控制与面积调节的装置 |
GB201618339D0 (en) * | 2016-10-31 | 2016-12-14 | Rolls Royce Plc | Thrust vectoring nozzle |
US10975979B2 (en) | 2018-11-15 | 2021-04-13 | General Electric Company | Actuator fail fix system |
CN110412997B (zh) * | 2019-07-22 | 2022-05-10 | 中国人民解放军军事科学院国防科技创新研究院 | 一种基于神经网络的航天器姿控喷管故障智能诊断系统及方法 |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR999277A (xx) * | 1952-01-29 | |||
US1181111A (en) * | 1915-12-09 | 1916-05-02 | Arthur Richard Carter | Steam-engine. |
US2395435A (en) * | 1940-09-27 | 1946-02-26 | Louis T E Thompson | Emergency control mechanism for aircraft |
US2893209A (en) * | 1954-03-23 | 1959-07-07 | Rolls Royce | Multi piston ram device |
US2866315A (en) * | 1955-04-14 | 1958-12-30 | Kett Corp | Variable exhaust nozzle actuator |
GB969269A (en) * | 1962-04-13 | 1964-09-09 | Ferranti Ltd | Improvements relating to flight aid systems |
DE1287862B (xx) * | 1963-09-26 | 1969-01-23 | ||
US3554084A (en) * | 1967-11-17 | 1971-01-12 | Honeywell Inc | Redundant force summing servo unit |
US3612400A (en) * | 1970-06-02 | 1971-10-12 | Gen Motors Corp | Variable jet propulsion nozzle |
US3806063A (en) * | 1971-10-08 | 1974-04-23 | Chandler Evans Inc | Thrust vector steering techniques and apparatus |
US4000854A (en) * | 1975-10-02 | 1977-01-04 | General Electric Company | Thrust vectorable exhaust nozzle |
US4030291A (en) * | 1976-01-02 | 1977-06-21 | General Electric Company | Thrust reverser for a gas turbofan engine |
US4128208A (en) * | 1977-07-11 | 1978-12-05 | General Electric Company | Exhaust nozzle flap seal arrangement |
US4718647A (en) * | 1980-02-20 | 1988-01-12 | Avm, Inc. | Pneumatic counterbalance with dual force |
US4807517A (en) * | 1982-09-30 | 1989-02-28 | Allied-Signal Inc. | Electro-hydraulic proportional actuator |
US4538504A (en) * | 1983-11-18 | 1985-09-03 | General Electric Company | Fail-safe servovalve system |
US4805515A (en) * | 1983-11-18 | 1989-02-21 | General Electric Company | Fail-safe servovalve system |
US4704865A (en) * | 1984-07-16 | 1987-11-10 | The Boeing Company | Hydraulic reserve system for aircraft |
US4711089A (en) * | 1984-07-16 | 1987-12-08 | The Boeing Company | Hydraulic system for aircraft |
US4799623A (en) * | 1987-11-04 | 1989-01-24 | United Technologies Corporation | Variable convergent/divergent nozzle |
US4994660A (en) | 1989-04-11 | 1991-02-19 | Hitachi, Ltd. | Axisymmetric vectoring exhaust nozzle |
US5011080A (en) * | 1990-04-18 | 1991-04-30 | United Technologies Corporation | Convergent/divergent nozzle construction |
US5174502A (en) | 1991-05-10 | 1992-12-29 | General Electric Company | Support for a translating nozzle vectoring ring |
FR2691508B1 (fr) * | 1992-05-20 | 1994-07-08 | Snecma | Verin a fluide sous pression et tuyere a section variable en faisant application. |
US5279107A (en) * | 1992-06-30 | 1994-01-18 | United Technologies Corporation | Fuel control system with fuel metering valve fault accommodation |
-
1995
- 1995-09-11 IL IL11524895A patent/IL115248A/xx not_active IP Right Cessation
- 1995-09-18 EP EP95306570A patent/EP0704615B1/en not_active Expired - Lifetime
- 1995-09-18 DE DE69524345T patent/DE69524345T2/de not_active Expired - Fee Related
- 1995-09-18 ES ES95306570T patent/ES2168338T3/es not_active Expired - Lifetime
- 1995-09-26 JP JP24710095A patent/JP3694549B2/ja not_active Expired - Fee Related
-
1997
- 1997-03-14 US US08/818,051 patent/US6142416A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE69524345T2 (de) | 2002-08-29 |
EP0704615A3 (en) | 1997-03-26 |
EP0704615B1 (en) | 2001-12-05 |
EP0704615A2 (en) | 1996-04-03 |
JPH08210182A (ja) | 1996-08-20 |
DE69524345D1 (de) | 2002-01-17 |
ES2168338T3 (es) | 2002-06-16 |
US6142416A (en) | 2000-11-07 |
IL115248A0 (en) | 1995-12-31 |
JP3694549B2 (ja) | 2005-09-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FF | Patent granted | ||
KB | Patent renewed | ||
MM9K | Patent not in force due to non-payment of renewal fees |