ES2284455T3 - Mecanismo de apoyo y accionador lineal para un anillo unisono de una tobera vectorial axisimetrica. - Google Patents

Mecanismo de apoyo y accionador lineal para un anillo unisono de una tobera vectorial axisimetrica. Download PDF

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Publication number
ES2284455T3
ES2284455T3 ES00307004T ES00307004T ES2284455T3 ES 2284455 T3 ES2284455 T3 ES 2284455T3 ES 00307004 T ES00307004 T ES 00307004T ES 00307004 T ES00307004 T ES 00307004T ES 2284455 T3 ES2284455 T3 ES 2284455T3
Authority
ES
Spain
Prior art keywords
vector
ring
actuator
vector ring
support
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 - Lifetime
Application number
ES00307004T
Other languages
English (en)
Spanish (es)
Inventor
Bernard James Renggli
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
Application granted granted Critical
Publication of ES2284455T3 publication Critical patent/ES2284455T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K1/002—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
    • 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)
  • Control Of Turbines (AREA)
  • Transmission Devices (AREA)
  • Supercharger (AREA)
ES00307004T 1999-08-25 2000-08-16 Mecanismo de apoyo y accionador lineal para un anillo unisono de una tobera vectorial axisimetrica. Expired - Lifetime ES2284455T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US383134 1999-08-25
US09/383,134 US6199772B1 (en) 1999-08-25 1999-08-25 Linear actuation and vectoring ring support mechanism for axisymmetric vectoring nozzle

Publications (1)

Publication Number Publication Date
ES2284455T3 true ES2284455T3 (es) 2007-11-16

Family

ID=23511876

Family Applications (1)

Application Number Title Priority Date Filing Date
ES00307004T Expired - Lifetime ES2284455T3 (es) 1999-08-25 2000-08-16 Mecanismo de apoyo y accionador lineal para un anillo unisono de una tobera vectorial axisimetrica.

Country Status (5)

Country Link
US (1) US6199772B1 (enExample)
EP (1) EP1079093B1 (enExample)
JP (1) JP4578652B2 (enExample)
DE (1) DE60034404T2 (enExample)
ES (1) ES2284455T3 (enExample)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2792366B1 (fr) * 1999-04-15 2005-08-19 Snecma Tuyere d'ejection axisymetrique, convergente divergente et orientable
US6415599B1 (en) 2001-05-11 2002-07-09 General Electric Company Engine interface for axisymmetric vectoring nozzle
US6622472B2 (en) * 2001-10-17 2003-09-23 Gateway Space Transport, Inc. Apparatus and method for thrust vector control
US6694723B2 (en) 2002-03-27 2004-02-24 United Technologies Corporation Valve assembly for gas turbine engine
US9759087B2 (en) 2007-08-08 2017-09-12 Rohr, Inc. Translating variable area fan nozzle providing an upstream bypass flow exit
EP2181262B1 (en) * 2007-08-08 2012-05-16 Rohr, Inc. Variable area fan nozzle with bypass flow
GB2462413B (en) * 2008-08-04 2011-03-02 Rolls Royce Plc An actuator arrangement
US8572986B2 (en) * 2009-07-27 2013-11-05 United Technologies Corporation Retainer for suspended thermal protection elements in a gas turbine engine
US8875486B2 (en) * 2010-05-17 2014-11-04 Rohr, Inc. Guide system for nacelle assembly
US9650991B2 (en) * 2013-06-27 2017-05-16 The Boeing Company Pivoting ring petal actuation for variable area fan nozzle
CN105134408B (zh) * 2015-09-18 2017-09-22 中国航空工业集团公司沈阳发动机设计研究所 一种二元塞式喷管单作动系统控制机构
US10837402B2 (en) * 2020-01-09 2020-11-17 Guanhao Wu Thrust vector nozzle
CN113982777B (zh) * 2021-11-10 2023-03-28 南京航空航天大学 一种可线性化控制的双喉道气动矢量喷管
CN114109645B (zh) * 2021-11-12 2023-12-19 中国航发沈阳发动机研究所 一种轴对称收扩喷管运动机构
CN116198730B (zh) * 2023-04-19 2025-07-01 广东信稳能控技术研究有限公司 电涵垂升共转翼飞机的发动机飞行攻角电动调节机构

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3004385A (en) * 1958-06-25 1961-10-17 Gen Motors Corp Variable convergent-divergent jet nozzle
US4994660A (en) * 1989-04-11 1991-02-19 Hitachi, Ltd. Axisymmetric vectoring exhaust nozzle
US5261605A (en) * 1990-08-23 1993-11-16 United Technologies Corporation Axisymmetric nozzle with gimbled unison ring
US5150839A (en) * 1991-03-14 1992-09-29 General Electric Company Nozzle load management
US5174502A (en) * 1991-05-10 1992-12-29 General Electric Company Support for a translating nozzle vectoring ring
DE69232222T2 (de) * 1991-05-16 2002-08-22 General Electric Co., Schenectady Hitzeschild für achsymmetrische schwenkbare Schubdüse
ES2075782B1 (es) 1992-02-20 1998-03-16 Sener Ing & Sist Tobera orientable de geometria variable para turbinas de gas.
US5437411A (en) 1992-12-14 1995-08-01 General Electric Company Vectoring exhaust nozzle flap and seal positioning apparatus
US5442909A (en) 1994-05-13 1995-08-22 General Electric Company Control system for limiting the vector angle in an axisymmetric vectoring exhaust nozzle
US5680755A (en) * 1995-09-25 1997-10-28 General Electric Company Convertible ejector selectively cooled thrust vectoring exhaust nozzle
US5893518A (en) 1995-11-30 1999-04-13 United Technologies Corporation Attachment means for flaps of variable exhaust nozzle
US5779152A (en) 1997-01-16 1998-07-14 General Electric Company Coordinated vectoring exhaust nozzle with scissors linkage
DE69725432T2 (de) * 1997-06-16 2004-08-19 Industria De Turbo Propulsores S.A., Zamudio Befestigungsvorrichtung für eine divergierende Master-Düsenklappe einer Schubüse mit veränderlicher Geometrie

Also Published As

Publication number Publication date
JP2001132540A (ja) 2001-05-15
EP1079093A3 (en) 2004-03-31
EP1079093A2 (en) 2001-02-28
DE60034404T2 (de) 2008-01-10
EP1079093B1 (en) 2007-04-18
JP4578652B2 (ja) 2010-11-10
US6199772B1 (en) 2001-03-13
DE60034404D1 (de) 2007-05-31

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