JP4340769B2 - ガスタービンエンジンの空気流に生じる歪み損失を減少させるための方法及び装置 - Google Patents

ガスタービンエンジンの空気流に生じる歪み損失を減少させるための方法及び装置 Download PDF

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Publication number
JP4340769B2
JP4340769B2 JP2002280107A JP2002280107A JP4340769B2 JP 4340769 B2 JP4340769 B2 JP 4340769B2 JP 2002280107 A JP2002280107 A JP 2002280107A JP 2002280107 A JP2002280107 A JP 2002280107A JP 4340769 B2 JP4340769 B2 JP 4340769B2
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JP
Japan
Prior art keywords
blade
air flow
assembly
passage
vane assembly
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
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JP2002280107A
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English (en)
Japanese (ja)
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JP2003148246A (ja
JP2003148246A5 (enExample
Inventor
ジョン・マイケル・コショーファー
ケビン・ロバート・ドレーク
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General Electric Co
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General Electric Co
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Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of JP2003148246A publication Critical patent/JP2003148246A/ja
Publication of JP2003148246A5 publication Critical patent/JP2003148246A5/ja
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • 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
    • F05D2220/00—Application
    • F05D2220/90—Application in vehicles adapted for vertical or short take off and landing (v/stol vehicles)
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device to control boundary layer

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)
JP2002280107A 2001-09-27 2002-09-26 ガスタービンエンジンの空気流に生じる歪み損失を減少させるための方法及び装置 Expired - Fee Related JP4340769B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/965,351 US6715983B2 (en) 2001-09-27 2001-09-27 Method and apparatus for reducing distortion losses induced to gas turbine engine airflow
US09/965351 2001-09-27

Publications (3)

Publication Number Publication Date
JP2003148246A JP2003148246A (ja) 2003-05-21
JP2003148246A5 JP2003148246A5 (enExample) 2005-11-10
JP4340769B2 true JP4340769B2 (ja) 2009-10-07

Family

ID=25509849

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002280107A Expired - Fee Related JP4340769B2 (ja) 2001-09-27 2002-09-26 ガスタービンエンジンの空気流に生じる歪み損失を減少させるための方法及び装置

Country Status (4)

Country Link
US (1) US6715983B2 (enExample)
EP (1) EP1298286B1 (enExample)
JP (1) JP4340769B2 (enExample)
ES (1) ES2382241T3 (enExample)

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US6997676B2 (en) * 2004-03-10 2006-02-14 General Electric Company Bifurcated outlet guide vanes
US6983601B2 (en) * 2004-05-28 2006-01-10 General Electric Company Method and apparatus for gas turbine engines
US8171732B2 (en) * 2006-09-08 2012-05-08 General Electric Company Turbocharger for a vehicle with a coanda device
EP2092163A4 (en) * 2006-11-14 2013-04-17 Volvo Aero Corp RUNWAY ARRANGEMENT CONFIGURATED FOR ROTATING AN ELECTRICITY IN A GAS TURBINE ENGINE, STATOR COMPONENT WITH THE ROW ROD ARRANGEMENT, GAS TURBINE AND AIRCRAFT RADIATOR
ES2334717T3 (es) * 2007-01-18 2010-03-15 Siemens Aktiengesellschaft Alabe conductor para una turbina de gas.
WO2008155243A1 (de) * 2007-06-20 2008-12-24 Alstom Technology Ltd Leitschaufelreihe
US7985053B2 (en) * 2008-09-12 2011-07-26 General Electric Company Inlet guide vane
DE102009013399A1 (de) * 2009-03-16 2010-09-23 Mtu Aero Engines Gmbh Tandemschaufelkonstruktion
US8572981B2 (en) 2010-11-08 2013-11-05 General Electric Company Self-oscillating fuel injection jets
US9062559B2 (en) 2011-08-02 2015-06-23 Siemens Energy, Inc. Movable strut cover for exhaust diffuser
US9032721B2 (en) * 2011-12-14 2015-05-19 Siemens Energy, Inc. Gas turbine engine exhaust diffuser including circumferential vane
US20130170969A1 (en) * 2012-01-04 2013-07-04 General Electric Company Turbine Diffuser
US9422864B2 (en) * 2012-12-20 2016-08-23 General Electric Company Staggered double row, slotted airfoil design for gas turbine exhaust frame
WO2014133612A1 (en) * 2013-02-26 2014-09-04 Bloxham Matthew J Gas turbine engine variable geometry flow component
US9488191B2 (en) 2013-10-30 2016-11-08 Siemens Aktiengesellschaft Gas turbine diffuser strut including coanda flow injection
US10094223B2 (en) 2014-03-13 2018-10-09 Pratt & Whitney Canada Corp. Integrated strut and IGV configuration
CN105443162B (zh) * 2014-09-26 2017-04-19 中航商用航空发动机有限责任公司 发动机过渡段以及航空发动机
FR3027053B1 (fr) * 2014-10-10 2019-09-13 Safran Aircraft Engines Stator de turbomachine d'aeronef
BR112017015561B1 (pt) * 2015-01-28 2022-11-16 Nuovo Pignone Tecnologie Srl Dispositivo para controle do fluxo em uma turbomáquina e turbomáquina
US10151322B2 (en) * 2016-05-20 2018-12-11 United Technologies Corporation Tandem tip blade
US10704418B2 (en) 2016-08-11 2020-07-07 General Electric Company Inlet assembly for an aircraft aft fan
US10253779B2 (en) 2016-08-11 2019-04-09 General Electric Company Inlet guide vane assembly for reducing airflow swirl distortion of an aircraft aft fan
US10259565B2 (en) 2016-08-11 2019-04-16 General Electric Company Inlet assembly for an aircraft aft fan
US10252790B2 (en) 2016-08-11 2019-04-09 General Electric Company Inlet assembly for an aircraft aft fan
US11149639B2 (en) 2016-11-29 2021-10-19 Rolls-Royce North American Technologies Inc. Systems and methods of reducing distortions of the inlet airflow to a turbomachine
GB201708050D0 (en) * 2017-05-19 2017-07-05 Rolls Royce Plc A Stator arrangement
US11002141B2 (en) * 2017-05-22 2021-05-11 General Electric Company Method and system for leading edge auxiliary turbine vanes
US10883515B2 (en) 2017-05-22 2021-01-05 General Electric Company Method and system for leading edge auxiliary vanes
DE102019200885A1 (de) * 2019-01-24 2020-07-30 MTU Aero Engines AG Leitgitter für eine Strömungsmaschine
GB201917171D0 (en) * 2019-11-26 2020-01-08 Rolls Royce Plc Gas turbine engine
CN112031879A (zh) * 2020-09-18 2020-12-04 中国航发四川燃气涡轮研究院 涡轮后支板叶片及其航空发动机
DE102021113234B4 (de) 2021-05-21 2022-12-15 Naber Holding Gmbh & Co. Kg Rohrbogen für einen Abluftkanal einer Dunstabzugshaube
CA3212474A1 (en) * 2022-09-21 2024-03-21 Pratt & Whitney Canada Corp. Turbine exhaust case with slotted struts

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Also Published As

Publication number Publication date
US20030059291A1 (en) 2003-03-27
US6715983B2 (en) 2004-04-06
JP2003148246A (ja) 2003-05-21
ES2382241T3 (es) 2012-06-06
EP1298286B1 (en) 2012-03-14
EP1298286A3 (en) 2005-02-09
EP1298286A2 (en) 2003-04-02

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