SG119178A1 - Valve assembly for gas turbine engine - Google Patents

Valve assembly for gas turbine engine

Info

Publication number
SG119178A1
SG119178A1 SG200301637A SG200301637A SG119178A1 SG 119178 A1 SG119178 A1 SG 119178A1 SG 200301637 A SG200301637 A SG 200301637A SG 200301637 A SG200301637 A SG 200301637A SG 119178 A1 SG119178 A1 SG 119178A1
Authority
SG
Singapore
Prior art keywords
gas turbine
valve assembly
turbine engine
engine
valve
Prior art date
Application number
SG200301637A
Other languages
English (en)
Inventor
Eric J Ward
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of SG119178A1 publication Critical patent/SG119178A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/40—Movement of components
    • F05D2250/41—Movement of components with one degree of freedom
    • F05D2250/411—Movement of components with one degree of freedom in rotation
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Lift Valve (AREA)
SG200301637A 2002-03-27 2003-03-20 Valve assembly for gas turbine engine SG119178A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/109,109 US6694723B2 (en) 2002-03-27 2002-03-27 Valve assembly for gas turbine engine

Publications (1)

Publication Number Publication Date
SG119178A1 true SG119178A1 (en) 2006-02-28

Family

ID=27804399

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200301637A SG119178A1 (en) 2002-03-27 2003-03-20 Valve assembly for gas turbine engine

Country Status (4)

Country Link
US (1) US6694723B2 (de)
EP (1) EP1348835A3 (de)
CA (1) CA2422553C (de)
SG (1) SG119178A1 (de)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7584601B2 (en) * 2004-09-03 2009-09-08 Metcalfe Iii Tristram Walker Charged particle thrust engine
US7287504B2 (en) * 2004-10-29 2007-10-30 Siemens Vdo Automotive Canada Inc. Over-center actuator
US7581382B2 (en) * 2005-04-28 2009-09-01 United Technologies Corporation Gas turbine engine air valve assembly
US8015996B2 (en) 2005-04-28 2011-09-13 United Technologies Corporation Gas turbine engine air valve assembly
ATE523682T1 (de) * 2005-09-27 2011-09-15 Volvo Aero Corp Anordnung zum antrieb eines flugzeugs, flugzeug und auslassdüse für ein düsentriebwerk
FR2900445B1 (fr) * 2006-04-28 2013-02-08 Snecma Turboreacteur comprenant un canal de post combustion refroidi par un flux de ventilation a debit variable
US20080072604A1 (en) * 2006-09-26 2008-03-27 United Technologies Corporation Pressure balance control for gas turbine engine nozzle
US7854124B2 (en) * 2006-10-27 2010-12-21 United Technologies Corporation Combined control for supplying cooling air and support air in a turbine engine nozzle
US7870741B2 (en) * 2007-05-25 2011-01-18 General Electric Company Turbine engine valve assembly and method of assembling the same
US7871242B2 (en) * 2007-05-31 2011-01-18 United Technologies Corporation Single actuator controlled rotational flow balance system
US8240126B2 (en) * 2008-03-22 2012-08-14 Pratt & Whitney Rocketdyne, Inc. Valve system for a gas turbine engine
US8286416B2 (en) * 2008-04-02 2012-10-16 Pratt & Whitney Rocketdyne, Inc. Valve system for a gas turbine engine
US8402744B2 (en) * 2008-03-22 2013-03-26 Pratt & Whitney Rocketdyne, Inc. Valve system for a gas turbine engine
US8578716B2 (en) * 2008-03-22 2013-11-12 United Technologies Corporation Valve system for a gas turbine engine
GB2462413B (en) * 2008-08-04 2011-03-02 Rolls Royce Plc An actuator arrangement
US8197187B2 (en) 2008-12-29 2012-06-12 Caterpillar Inc. Inspection hole plug with a ball swivel
US8616850B2 (en) 2010-06-11 2013-12-31 United Technologies Corporation Gas turbine engine blade mounting arrangement
US8967952B2 (en) 2011-12-22 2015-03-03 United Technologies Corporation Gas turbine engine duct blocker that includes a duct blocker rotor with a plurality of roller elements
US9011082B2 (en) 2011-12-22 2015-04-21 United Technologies Corporation Gas turbine engine duct blocker with rotatable vane segments
CN103985407A (zh) 2013-02-07 2014-08-13 辉达公司 采用分段式页面配置的dram
US10352248B2 (en) * 2014-10-01 2019-07-16 United Technologies Corporation Synchronized air modulating system
US9835043B2 (en) 2014-10-01 2017-12-05 United Technologies Corporation Guided binding-resistant actuation apparatus and method
WO2021072070A1 (en) * 2019-10-09 2021-04-15 Kitty Hawk Corporation Short takeoff and landing vehicle with forward swept wings
US11247773B2 (en) 2020-06-12 2022-02-15 Kitty Hawk Corporation Pylon mounted tilt rotor

Citations (5)

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Publication number Priority date Publication date Assignee Title
GB710750A (en) * 1952-05-12 1954-06-16 Russell Lacey Mfg Co Inc Improvements in or relating to web severing means for tufting machines
FR1306025A (fr) * 1961-08-08 1962-10-13 Snecma Mélangeur à coefficient de blocage variable dans les réacteurs à double flux à flux mélangés
GB1100656A (en) * 1965-10-04 1968-01-24 Rolls Royce Jet propulsion nozzle
US3429509A (en) * 1967-05-31 1969-02-25 United Aircraft Corp Cooling scheme for a three bearing swivel nozzle
US4544098A (en) * 1982-12-27 1985-10-01 United Technologies Corporation Cooled exhaust nozzle flaps

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US2951660A (en) * 1956-06-25 1960-09-06 James V Giliberty Method and means for controlling the jet thrust of an aircraft
GB1550633A (en) * 1976-07-21 1979-08-15 Gen Electric Thrust-vectoring gas turbine engine exhaust nozzles
US4222233A (en) 1977-08-02 1980-09-16 General Electric Company Auxiliary lift propulsion system with oversized front fan
US4502636A (en) * 1982-04-07 1985-03-05 Rolls-Royce Inc. Variable geometry ejector nozzle for turbomachines
JPS59141753A (ja) * 1983-01-31 1984-08-14 Fuji Heavy Ind Ltd Ｖ／ｓｔｏｌ機用推力増大偏向装置
US5082209A (en) * 1991-03-01 1992-01-21 United Technologies Corporation Thrust reverser assembly
DE69232222T2 (de) * 1991-05-16 2002-08-22 General Electric Co., Schenectady Hitzeschild für achsymmetrische schwenkbare Schubdüse
DE4138784A1 (de) 1991-11-26 1993-05-27 Mtu Muenchen Gmbh Einrichtung zur abdichtung eines spaltes
CA2091473A1 (en) * 1992-04-20 1993-10-21 Mark J. Wagner Bypass injector valve for variable cycle aircraft engines
GB2267066B (en) 1992-05-16 1995-06-14 Rolls Royce Plc Vectorable nozzle mounting
US5351888A (en) 1993-05-14 1994-10-04 General Electric Company Multi-axis vectorable exhaust nozzle
US5484105A (en) * 1994-07-13 1996-01-16 General Electric Company Cooling system for a divergent section of a nozzle
US5706650A (en) * 1995-08-09 1998-01-13 United Technologies Corporation Vectoring nozzle using injected high pressure air
US5799874A (en) 1995-11-30 1998-09-01 United Technologies Corporation Aerodynamically controlled ejector
JPH1026353A (ja) * 1996-07-12 1998-01-27 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器のバイパス空気量制御装置
US5816042A (en) * 1996-12-27 1998-10-06 United Technologies Corporation Flow diverter system for multiple streams for gas turbine engines
US6199772B1 (en) 1999-08-25 2001-03-13 General Electric Company Linear actuation and vectoring ring support mechanism for axisymmetric vectoring nozzle

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB710750A (en) * 1952-05-12 1954-06-16 Russell Lacey Mfg Co Inc Improvements in or relating to web severing means for tufting machines
FR1306025A (fr) * 1961-08-08 1962-10-13 Snecma Mélangeur à coefficient de blocage variable dans les réacteurs à double flux à flux mélangés
GB1100656A (en) * 1965-10-04 1968-01-24 Rolls Royce Jet propulsion nozzle
US3429509A (en) * 1967-05-31 1969-02-25 United Aircraft Corp Cooling scheme for a three bearing swivel nozzle
US4544098A (en) * 1982-12-27 1985-10-01 United Technologies Corporation Cooled exhaust nozzle flaps

Also Published As

Publication number Publication date
EP1348835A3 (de) 2005-08-17
US6694723B2 (en) 2004-02-24
US20030205043A1 (en) 2003-11-06
CA2422553C (en) 2007-01-09
CA2422553A1 (en) 2003-09-27
EP1348835A2 (de) 2003-10-01

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