DE69837068D1 - Interner Zwischenkühler für Gasturbinenkompressoren - Google Patents
Interner Zwischenkühler für GasturbinenkompressorenInfo
- 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
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
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
- F02C7/143—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid before or between the compressor stages
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/5826—Cooling at least part of the working fluid in a heat exchanger
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
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)
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 |
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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 |
-
1997
- 1997-10-22 US US08/955,799 patent/US6430931B1/en not_active Expired - Lifetime
-
1998
- 1998-10-21 DE DE69837068T patent/DE69837068T2/de not_active Expired - Lifetime
- 1998-10-21 EP EP98308618A patent/EP0911505B1/de not_active Expired - Lifetime
-
2002
- 2002-05-15 US US10/146,196 patent/US6637208B2/en not_active Expired - Lifetime
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 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |