DE69837068D1 - Interner Zwischenkühler für Gasturbinenkompressoren - Google Patents

Interner Zwischenkühler für Gasturbinenkompressoren

Info

Publication number
DE69837068D1
DE69837068D1 DE69837068T DE69837068T DE69837068D1 DE 69837068 D1 DE69837068 D1 DE 69837068D1 DE 69837068 T DE69837068 T DE 69837068T DE 69837068 T DE69837068 T DE 69837068T DE 69837068 D1 DE69837068 D1 DE 69837068D1
Authority
DE
Germany
Prior art keywords
gas turbine
turbine compressors
internal intercooler
intercooler
internal
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
DE69837068T
Other languages
English (en)
Other versions
DE69837068T2 (de
Inventor
Michael William Horner
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
Publication of DE69837068D1 publication Critical patent/DE69837068D1/de
Application granted granted Critical
Publication of DE69837068T2 publication Critical patent/DE69837068T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/14Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F02C7/143Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/58Cooling; Heating; Diminishing heat transfer
    • F04D29/582Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • F04D29/5826Cooling at least part of the working fluid in a heat exchanger
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2214Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE69837068T 1997-10-22 1998-10-21 Interner Zwischenkühler für Gasturbinenkompressoren Expired - Lifetime DE69837068T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US955799 1997-10-22
US08/955,799 US6430931B1 (en) 1997-10-22 1997-10-22 Gas turbine in-line intercooler

Publications (2)

Publication Number Publication Date
DE69837068D1 true DE69837068D1 (de) 2007-03-29
DE69837068T2 DE69837068T2 (de) 2007-10-31

Family

ID=25497358

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69837068T Expired - Lifetime DE69837068T2 (de) 1997-10-22 1998-10-21 Interner Zwischenkühler für Gasturbinenkompressoren

Country Status (3)

Country Link
US (2) US6430931B1 (de)
EP (1) EP0911505B1 (de)
DE (1) DE69837068T2 (de)

Families Citing this family (81)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6374612B1 (en) * 2000-09-21 2002-04-23 Caterpillar Inc. Interstage cooling of a multi-compressor turbocharger
US7278472B2 (en) * 2002-09-20 2007-10-09 Modine Manufacturing Company Internally mounted radial flow intercooler for a combustion air changer
US6929056B2 (en) 2002-12-06 2005-08-16 Modine Manufacturing Company Tank manifold for internally mounted radial flow intercooler for a combustion air charger
WO2004074655A1 (en) * 2003-02-24 2004-09-02 Pratt & Whitney Canada Corp. Low volumetric compression ratio integrated turbo-compound rotary engine
US7272933B2 (en) * 2004-01-28 2007-09-25 General Electric Company Methods and apparatus for operating gas turbine engines
EP1793091A1 (de) * 2005-12-01 2007-06-06 Siemens Aktiengesellschaft Dampfturbine mit Lagerstreben
US20080047276A1 (en) * 2006-08-25 2008-02-28 Siemens Power Generation, Inc. Combustion turbine having a single compressor with inter-cooling between stages
FR2913063B1 (fr) * 2007-02-27 2012-03-16 Snecma Moteur d'aeronef equipe de moyens d'echange thermiques.
US7862293B2 (en) * 2007-05-03 2011-01-04 Pratt & Whitney Canada Corp. Low profile bleed air cooler
FR2920483B1 (fr) * 2007-08-30 2009-10-30 Snecma Sa Generation d'electricite dans une turbomachine
DE102008024335A1 (de) 2008-05-20 2009-11-26 Frank Schuster Gasturbinentriebwerk in Nebenstromausführung
US9033648B2 (en) 2010-12-24 2015-05-19 Rolls-Royce North American Technologies, Inc. Cooled gas turbine engine member
WO2013147953A1 (en) * 2011-12-30 2013-10-03 Rolls-Royce North American Technologies Inc. Aircraft propulsion gas turbine engine with heat exchange
US20130239542A1 (en) * 2012-03-16 2013-09-19 United Technologies Corporation Structures and methods for intercooling aircraft gas turbine engines
FR2989109B1 (fr) * 2012-04-05 2018-06-01 Safran Aircraft Engines Partie de stator comportant une aube de stator et un ensemble de lamelles
US10145253B2 (en) 2012-04-05 2018-12-04 Safran Aircraft Engines Stator vane formed by a set of vane parts
FR2989110B1 (fr) * 2012-04-05 2016-09-09 Snecma Aube de stator formee par un ensemble de parties d'aube
US8813503B2 (en) 2012-06-14 2014-08-26 General Electric Company Gas turbine control systems and methods
US9086019B2 (en) * 2012-07-02 2015-07-21 United Technologies Corporation Turbomachine thermal energy exchange
US20140027097A1 (en) * 2012-07-30 2014-01-30 Ian Alexandre Araujo De Barros Heat Exchanger for an Intercooler and Water Extraction Apparatus
US9476313B2 (en) * 2012-12-21 2016-10-25 United Technologies Corporation Gas turbine engine including a pre-diffuser heat exchanger
EP2971737B1 (de) 2013-03-14 2020-11-11 Rolls-Royce North American Technologies, Inc. Zwischengekühlte gasturbine mit einem geschlossenen kombinierten arbeitszyklus
EP3071913B1 (de) 2013-11-18 2020-06-03 General Electric Company Monolithische röhre-in einem matrixwärmetauscher
US20150260127A1 (en) * 2014-03-13 2015-09-17 Arthur J. Wennerstrom Aircraft Turbofan Engine with Multiple High-Pressure Core Modules Not Concentric with the Engine Centerline
US10660236B2 (en) 2014-04-08 2020-05-19 General Electric Company Systems and methods for using additive manufacturing for thermal management
US10356945B2 (en) 2015-01-08 2019-07-16 General Electric Company System and method for thermal management using vapor chamber
US10371055B2 (en) 2015-02-12 2019-08-06 United Technologies Corporation Intercooled cooling air using cooling compressor as starter
US10731560B2 (en) 2015-02-12 2020-08-04 Raytheon Technologies Corporation Intercooled cooling air
US10006370B2 (en) 2015-02-12 2018-06-26 United Technologies Corporation Intercooled cooling air with heat exchanger packaging
US9856793B2 (en) 2015-02-12 2018-01-02 United Technologies Corporation Intercooled cooling air with improved air flow
US11808210B2 (en) 2015-02-12 2023-11-07 Rtx Corporation Intercooled cooling air with heat exchanger packaging
US9797310B2 (en) 2015-04-02 2017-10-24 General Electric Company Heat pipe temperature management system for a turbomachine
US10598094B2 (en) 2015-04-02 2020-03-24 General Electric Company Heat pipe temperature management system for wheels and buckets in a turbomachine
US9909448B2 (en) 2015-04-15 2018-03-06 General Electric Company Gas turbine engine component with integrated heat pipe
US10480419B2 (en) 2015-04-24 2019-11-19 United Technologies Corporation Intercooled cooling air with plural heat exchangers
US9850819B2 (en) 2015-04-24 2017-12-26 United Technologies Corporation Intercooled cooling air with dual pass heat exchanger
US10221862B2 (en) 2015-04-24 2019-03-05 United Technologies Corporation Intercooled cooling air tapped from plural locations
US10830148B2 (en) 2015-04-24 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air with dual pass heat exchanger
US10100739B2 (en) 2015-05-18 2018-10-16 United Technologies Corporation Cooled cooling air system for a gas turbine engine
US10794288B2 (en) 2015-07-07 2020-10-06 Raytheon Technologies Corporation Cooled cooling air system for a turbofan engine
US10267191B2 (en) 2015-08-07 2019-04-23 Pratt & Whitney Canada Corp. Turboprop engine assembly with combined engine and cooling exhaust
US10240522B2 (en) 2015-08-07 2019-03-26 Pratt & Whitney Canada Corp. Auxiliary power unit with combined cooling of generator
US10253726B2 (en) 2015-08-07 2019-04-09 Pratt & Whitney Canada Corp. Engine assembly with combined engine and cooling exhaust
US10443508B2 (en) 2015-12-14 2019-10-15 United Technologies Corporation Intercooled cooling air with auxiliary compressor control
US11125160B2 (en) * 2015-12-28 2021-09-21 General Electric Company Method and system for combination heat exchanger
US20170191750A1 (en) * 2015-12-31 2017-07-06 General Electric Company System and method for compressor intercooler
US10209009B2 (en) 2016-06-21 2019-02-19 General Electric Company Heat exchanger including passageways
US10309242B2 (en) * 2016-08-10 2019-06-04 General Electric Company Ceramic matrix composite component cooling
US10563577B2 (en) 2016-08-22 2020-02-18 United Technologies Corporation Low rotor boost compressor for engine cooling circuit
US10746181B2 (en) 2016-08-22 2020-08-18 Raytheon Technologies Corporation Variable speed boost compressor for gas turbine engine cooling air supply
US10669940B2 (en) 2016-09-19 2020-06-02 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and turbine drive
US10794290B2 (en) 2016-11-08 2020-10-06 Raytheon Technologies Corporation Intercooled cooled cooling integrated air cycle machine
US10550768B2 (en) 2016-11-08 2020-02-04 United Technologies Corporation Intercooled cooled cooling integrated air cycle machine
KR101882104B1 (ko) * 2016-12-20 2018-07-25 두산중공업 주식회사 가스터빈
US10961911B2 (en) 2017-01-17 2021-03-30 Raytheon Technologies Corporation Injection cooled cooling air system for a gas turbine engine
US10995673B2 (en) 2017-01-19 2021-05-04 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
US10577964B2 (en) 2017-03-31 2020-03-03 United Technologies Corporation Cooled cooling air for blade air seal through outer chamber
US10711640B2 (en) 2017-04-11 2020-07-14 Raytheon Technologies Corporation Cooled cooling air to blade outer air seal passing through a static vane
US11022037B2 (en) * 2018-01-04 2021-06-01 General Electric Company Gas turbine engine thermal management system
US10738703B2 (en) 2018-03-22 2020-08-11 Raytheon Technologies Corporation Intercooled cooling air with combined features
US10808619B2 (en) 2018-04-19 2020-10-20 Raytheon Technologies Corporation Intercooled cooling air with advanced cooling system
US10830145B2 (en) 2018-04-19 2020-11-10 Raytheon Technologies Corporation Intercooled cooling air fleet management system
US10718233B2 (en) 2018-06-19 2020-07-21 Raytheon Technologies Corporation Intercooled cooling air with low temperature bearing compartment air
US11255268B2 (en) 2018-07-31 2022-02-22 Raytheon Technologies Corporation Intercooled cooling air with selective pressure dump
US11333173B2 (en) * 2019-04-26 2022-05-17 Pratt & Whitney Canada Corp. Inter-compressor cross-over pipe heat exchanger
US20200386189A1 (en) * 2019-04-30 2020-12-10 General Electric Company High Speed Aircraft Flight Technologies
US11267551B2 (en) 2019-11-15 2022-03-08 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11260976B2 (en) 2019-11-15 2022-03-01 General Electric Company System for reducing thermal stresses in a leading edge of a high speed vehicle
US11260953B2 (en) 2019-11-15 2022-03-01 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11427330B2 (en) 2019-11-15 2022-08-30 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11352120B2 (en) 2019-11-15 2022-06-07 General Electric Company System and method for cooling a leading edge of a high speed vehicle
EP3892949A3 (de) * 2020-01-03 2021-11-17 Raytheon Technologies Corporation Wärmetauscher und -platten für flugzeuge
US11448132B2 (en) 2020-01-03 2022-09-20 Raytheon Technologies Corporation Aircraft bypass duct heat exchanger
US11525637B2 (en) 2020-01-19 2022-12-13 Raytheon Technologies Corporation Aircraft heat exchanger finned plate manufacture
US11674758B2 (en) 2020-01-19 2023-06-13 Raytheon Technologies Corporation Aircraft heat exchangers and plates
US11585273B2 (en) 2020-01-20 2023-02-21 Raytheon Technologies Corporation Aircraft heat exchangers
US11585605B2 (en) 2020-02-07 2023-02-21 Raytheon Technologies Corporation Aircraft heat exchanger panel attachment
US11745847B2 (en) 2020-12-08 2023-09-05 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11407488B2 (en) 2020-12-14 2022-08-09 General Electric Company System and method for cooling a leading edge of a high speed vehicle
US11577817B2 (en) 2021-02-11 2023-02-14 General Electric Company System and method for cooling a leading edge of a high speed vehicle
CN114151188B (zh) * 2021-12-06 2023-11-03 中国空气动力研究与发展中心空天技术研究所 一种发动机进口空气冷却方法

Family Cites Families (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1777782A (en) * 1929-02-11 1930-10-07 Bundy Tubing Co Externally and internally finned tube and method therefor
CH252876A (de) 1947-01-24 1948-01-31 Bbc Brown Boveri & Cie Kompressoranlage mit Axialkompressoren und Zwischenkühler.
FR1155958A (fr) * 1956-03-28 1958-05-12 Perfectionnements aux turbines à fluide compressible
US3355883A (en) * 1966-01-24 1967-12-05 Gen Motors Corp Closed loop heat exchanger for a gas turbine engine
US3628885A (en) * 1969-10-01 1971-12-21 Gen Electric Fluid-cooled airfoil
DE2042478C3 (de) * 1970-08-27 1975-08-14 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Gasturbinentriebwerk, vorzugsweise Strahltriebwerk für Flugzeuge, mit Kühlluft- und gegebenenfalls Sperrluftentnahme
US3811495A (en) * 1970-10-26 1974-05-21 Laing Nikolaus Rotary heat exchangers in the form of turbines
US3796045A (en) * 1971-07-15 1974-03-12 Turbo Dev Inc Method and apparatus for increasing power output and/or thermal efficiency of a gas turbine power plant
GB1423350A (en) * 1972-05-12 1976-02-04 Cooling Dev Ltd Gas-moving devices
US3756020A (en) * 1972-06-26 1973-09-04 Curtiss Wright Corp Gas turbine engine and cooling system therefor
GB1516041A (en) * 1977-02-14 1978-06-28 Secr Defence Multistage axial flow compressor stators
US4137705A (en) 1977-07-25 1979-02-06 General Electric Company Cooling air cooler for a gas turbine engine
FR2482196A1 (fr) 1980-05-07 1981-11-13 Snecma Echangeur de chaleur pour moteur a reaction a double flux
US4550562A (en) 1981-06-17 1985-11-05 Rice Ivan G Method of steam cooling a gas generator
US4515523A (en) * 1983-10-28 1985-05-07 Westinghouse Electric Corp. Cooling arrangement for airfoil stator vane trailing edge
US4576547A (en) * 1983-11-03 1986-03-18 United Technologies Corporation Active clearance control
US4660376A (en) * 1984-04-27 1987-04-28 General Electric Company Method for operating a fluid injection gas turbine engine
US4914904A (en) 1988-11-09 1990-04-10 Avco Corporation Oil cooler for fan jet engines
US4949544A (en) * 1988-12-06 1990-08-21 General Electric Company Series intercooler
GB2242941B (en) * 1990-04-11 1994-05-04 Rolls Royce Plc A cooled gas turbine engine aerofoil
CA2093683C (en) * 1992-05-14 2002-10-15 William Miller Farrell Intercooled gas turbine engine
US5261228A (en) * 1992-06-25 1993-11-16 General Electric Company Apparatus for bleeding air
US5317877A (en) * 1992-08-03 1994-06-07 General Electric Company Intercooled turbine blade cooling air feed system
US5522356A (en) * 1992-09-04 1996-06-04 Spread Spectrum Method and apparatus for transferring heat energy from engine housing to expansion fluid employed in continuous combustion, pinned vane type, integrated rotary compressor-expander engine system
JP2684936B2 (ja) * 1992-09-18 1997-12-03 株式会社日立製作所 ガスタービン及びガスタービン翼
US5490559A (en) * 1994-07-20 1996-02-13 Dinulescu; Horia A. Heat exchanger with finned partition walls
GB9415436D0 (en) * 1994-07-30 1994-09-21 Provost Michael J Auxiliary gas turbine engines
CA2133793A1 (en) * 1994-10-06 1996-04-07 William E. Carscallen Inter compressor duct variable geometry annular diffuser/bleed valve
US5488825A (en) * 1994-10-31 1996-02-06 Westinghouse Electric Corporation Gas turbine vane with enhanced cooling
US5669217A (en) * 1995-09-25 1997-09-23 Anderson; J. Hilbert Method and apparatus for intercooling gas turbines
US5768884A (en) * 1995-11-22 1998-06-23 General Electric Company Gas turbine engine having flat rated horsepower
US5722241A (en) 1996-02-26 1998-03-03 Westinghouse Electric Corporation Integrally intercooled axial compressor and its application to power plants
US5711650A (en) * 1996-10-04 1998-01-27 Pratt & Whitney Canada, Inc. Gas turbine airfoil cooling

Also Published As

Publication number Publication date
US20030029158A1 (en) 2003-02-13
US6637208B2 (en) 2003-10-28
EP0911505A2 (de) 1999-04-28
EP0911505A3 (de) 2000-11-08
DE69837068T2 (de) 2007-10-31
EP0911505B1 (de) 2007-02-14
US6430931B1 (en) 2002-08-13

Similar Documents

Publication Publication Date Title
DE69837068D1 (de) Interner Zwischenkühler für Gasturbinenkompressoren
DE69816952D1 (de) Gasturbinentriebwerk
DE69816013D1 (de) Gasturbinentriebwerk
DE69511802D1 (de) Zusatzliche Gasturbinentriebwerke
DE69828916D1 (de) Emissionsarmes Verbrennungssystem für Gasturbinentriebwerke
DE60124572D1 (de) Halbaxial- und kreiselverdichter für ein gasturbinentriebwerk
ITRM980722A1 (it) Turbocompressore a gas di scarico a flusso radiale
DE69726626D1 (de) Dreikanaldiffusor für Gasturbinentriebwerk
DE69819290D1 (de) Luftabscheider für gasturbinen
DE69939346D1 (de) Brennstoffeinspritzdüse für Gasturbinentriebwerk
DE69730458D1 (de) Auspuffschalldämpfer für einen Verdichter
DE69721626D1 (de) Gasturbinenbrennkamer
DE69820207T2 (de) Rotor für gasturbinen
GB2345942B (en) Gas turbine engine internal air system
DE69833811D1 (de) Luftgekühlte Gasturbine
DE69828023D1 (de) Deckband für gekühlte gasturbinenschaufeln
GB9820226D0 (en) Gas turbine engine casing
DE69806540D1 (de) Lufteinlass für eine Turbomaschine
DE60005580D1 (de) Gasturbinentriebwerk
DE60028127D1 (de) Brennkammer für Gasturbinen
DE59709685D1 (de) Lufteinlauf für Triebwerke
DE69513133T2 (de) Flügel für Flügelzellenkompressor
DE69908540T2 (de) Gasturbinentriebwerk
DE69800844D1 (de) Luftreiniger für Verbrennungskraftmaschine
DE69713682D1 (de) Gasturbinenmotor

Legal Events

Date Code Title Description
8364 No opposition during term of opposition