IT1098088B - Raffreddatore dell'aria di raffreddamento per motore a gas a turboventilatore - Google Patents

Raffreddatore dell'aria di raffreddamento per motore a gas a turboventilatore

Info

Publication number
IT1098088B
IT1098088B IT26716/78A IT2671678A IT1098088B IT 1098088 B IT1098088 B IT 1098088B IT 26716/78 A IT26716/78 A IT 26716/78A IT 2671678 A IT2671678 A IT 2671678A IT 1098088 B IT1098088 B IT 1098088B
Authority
IT
Italy
Prior art keywords
turbo
cooling air
air cooler
gas engine
fan gas
Prior art date
Application number
IT26716/78A
Other languages
English (en)
Other versions
IT7826716A0 (it
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IT7826716A0 publication Critical patent/IT7826716A0/it
Application granted granted Critical
Publication of IT1098088B publication Critical patent/IT1098088B/it

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
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185Cooling means for reducing the temperature of the cooling air or gas
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D21/0001Recuperative heat exchangers
    • F28D21/0014Recuperative heat exchangers the heat being recuperated from waste air or from vapors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/024Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising cooling means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28DHEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Gas After Treatment (AREA)
IT26716/78A 1977-08-18 1978-08-11 Raffreddatore dell'aria di raffreddamento per motore a gas a turboventilatore IT1098088B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/825,614 US4254618A (en) 1977-08-18 1977-08-18 Cooling air cooler for a gas turbofan engine

Publications (2)

Publication Number Publication Date
IT7826716A0 IT7826716A0 (it) 1978-08-11
IT1098088B true IT1098088B (it) 1985-08-31

Family

ID=25244478

Family Applications (1)

Application Number Title Priority Date Filing Date
IT26716/78A IT1098088B (it) 1977-08-18 1978-08-11 Raffreddatore dell'aria di raffreddamento per motore a gas a turboventilatore

Country Status (5)

Country Link
US (1) US4254618A (it)
JP (1) JPS5452216A (it)
DE (1) DE2835903A1 (it)
FR (1) FR2400618A1 (it)
IT (1) IT1098088B (it)

Families Citing this family (200)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4709545A (en) * 1983-05-31 1987-12-01 United Technologies Corporation Bearing compartment protection system
US4546605A (en) * 1983-12-16 1985-10-15 United Technologies Corporation Heat exchange system
US4542623A (en) * 1983-12-23 1985-09-24 United Technologies Corporation Air cooler for providing buffer air to a bearing compartment
US4561246A (en) * 1983-12-23 1985-12-31 United Technologies Corporation Bearing compartment for a gas turbine engine
US4574584A (en) * 1983-12-23 1986-03-11 United Technologies Corporation Method of operation for a gas turbine engine
US4608819A (en) * 1983-12-27 1986-09-02 General Electric Company Gas turbine engine component cooling system
US4601202A (en) * 1983-12-27 1986-07-22 General Electric Company Gas turbine engine component cooling system
DE3514352A1 (de) * 1985-04-20 1986-10-23 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Gasturbinentriebwerk mit einrichtungen zur abzweigung von verdichterluft zur kuehlung von heissteilen
GB2194592B (en) * 1986-08-27 1990-07-04 Rolls Royce Plc Fluid outlet duct
WO1990001624A1 (en) * 1988-08-09 1990-02-22 Sundstrand Corporation High pressure intercooled turbine engine
GB2224080B (en) * 1988-10-22 1993-04-07 Rolls Royce Plc Fluid outlet duct
US5012646A (en) * 1988-11-28 1991-05-07 Machen, Inc. Turbine engine having combustor air precooler
US4991394A (en) * 1989-04-03 1991-02-12 Allied-Signal Inc. High performance turbine engine
DE3916477A1 (de) * 1989-05-20 1990-11-22 Mak Maschinenbau Krupp Verfahren und einrichtung zum entleeren von kraftstoffleitungen und einspritzduesen in gasturbinen
US5144794A (en) * 1989-08-25 1992-09-08 Hitachi, Ltd. Gas turbine engine with cooling of turbine blades
FR2656657A1 (fr) * 1989-12-28 1991-07-05 Snecma Turbomachine refroidie par air et procede de refroidissement de cette turbomachine.
US5203163A (en) * 1990-08-01 1993-04-20 General Electric Company Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air
CA2046797A1 (en) * 1990-08-01 1992-02-02 Franklin D. Parsons Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air
US5269133A (en) * 1991-06-18 1993-12-14 General Electric Company Heat exchanger for cooling a gas turbine
US5269135A (en) * 1991-10-28 1993-12-14 General Electric Company Gas turbine engine fan cooled heat exchanger
US5392614A (en) * 1992-03-23 1995-02-28 General Electric Company Gas turbine engine cooling system
US5305616A (en) * 1992-03-23 1994-04-26 General Electric Company Gas turbine engine cooling system
GB9215316D0 (en) * 1992-07-18 1992-09-02 Rolls Royce Plc Ducted fan gas turbine engine
FR2695161B1 (fr) * 1992-08-26 1994-11-04 Snecma Système de refroidissement d'un compresseur de turbomachine et de contrôle des jeux.
US5394687A (en) * 1993-12-03 1995-03-07 The United States Of America As Represented By The Department Of Energy Gas turbine vane cooling system
FR2734320B1 (fr) * 1995-05-15 1997-07-18 Aerospatiale Dispositif pour prelever et refroidir de l'air chaud au niveau d'un moteur d'aeronef
US5581996A (en) * 1995-08-16 1996-12-10 General Electric Company Method and apparatus for turbine cooling
RU2143574C1 (ru) * 1997-10-03 1999-12-27 Открытое акционерное общество "А.Люлька-Сатурн" Охлаждаемая многоступенчатая турбина турбореактивного двигателя
US6058696A (en) * 1997-12-22 2000-05-09 United Technologies Corporation Inlet and outlet module for a heat exchanger for a flowpath for working medium gases
US6106229A (en) * 1997-12-22 2000-08-22 United Technologies Corporation Heat exchanger system for a gas turbine engine
US6134880A (en) * 1997-12-31 2000-10-24 Concepts Eti, Inc. Turbine engine with intercooler in bypass air passage
DE10009655C1 (de) 2000-02-29 2001-05-23 Mtu Aero Engines Gmbh Kühlluftsystem
IT1317538B1 (it) * 2000-05-15 2003-07-09 Nuovo Pignone Spa Dispositivo per il controllo dei flussi di refrigerazione delleturbine a gas
DE10122695A1 (de) * 2001-05-10 2002-11-21 Siemens Ag Verfahren zur Kühlung einer Gasturbine und Gasturbinenanlage
RU2238418C2 (ru) * 2002-11-19 2004-10-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Двухконтурный газотурбинный двигатель
FR2858358B1 (fr) * 2003-07-28 2005-09-23 Snecma Moteurs Procede de refroidissement, par air refroidi en partie dans un echangeur externe, des parties chaudes d'un turboreacteur, et turboreacteur ainsi refroidi
FR2864996B1 (fr) * 2004-01-13 2006-03-10 Snecma Moteurs Systeme de refroidissement de parties chaudes d'un moteur d'aeronef, et moteur d'aeronef equipe d'un tel systeme de refroidissement
GB2413366B (en) * 2004-04-24 2006-09-13 Rolls Royce Plc Engine.
US7377100B2 (en) * 2004-08-27 2008-05-27 Pratt & Whitney Canada Corp. Bypass duct fluid cooler
US7373779B2 (en) * 2004-10-19 2008-05-20 General Electric Company Methods and apparatus for cooling gas turbine engines
FR2896275B1 (fr) * 2006-01-19 2010-05-28 Airbus France Turbomoteur a double flux pourvu d'un prerefroidisseur.
FR2896276B1 (fr) * 2006-01-19 2008-02-15 Airbus France Sas Turbomoteur a double flux pourvu d'un prerefroidisseur.
GB0607773D0 (en) * 2006-04-20 2006-05-31 Rolls Royce Plc A gas turbine engine
GB0607771D0 (en) * 2006-04-20 2006-05-31 Rolls Royce Plc A heat exchanger arrangement
US8776952B2 (en) * 2006-05-11 2014-07-15 United Technologies Corporation Thermal management system for turbofan engines
FR2902830B1 (fr) * 2006-06-27 2008-08-08 Airbus France Sas Turboreacteur pour aeronef
US7658060B2 (en) * 2006-07-19 2010-02-09 United Technologies Corporation Lubricant cooling exchanger dual intake duct
FR2904663B1 (fr) * 2006-08-01 2012-02-03 Snecma Turbomachine a double flux a variation artificielle de sa section de col
US7861512B2 (en) * 2006-08-29 2011-01-04 Pratt & Whitney Canada Corp. Turbofan bypass duct air cooled fluid cooler installation
US20080053060A1 (en) * 2006-08-29 2008-03-06 Pratt & Whitney Canada Corp. Bypass lip seal
DE602006019008D1 (de) 2006-10-12 2011-01-27 United Technologies Corp Modulationsströmung durch turbomotorkühlsystem
US8387362B2 (en) * 2006-10-19 2013-03-05 Michael Ralph Storage Method and apparatus for operating gas turbine engine heat exchangers
US7823389B2 (en) * 2006-11-15 2010-11-02 General Electric Company Compound clearance control engine
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
US8056345B2 (en) 2007-06-13 2011-11-15 United Technologies Corporation Hybrid cooling of a gas turbine engine
ES2322317B1 (es) * 2007-06-20 2010-03-31 Futur Investment Partners, S.A. Turbopropulsor aeronautico.
FR2917714B1 (fr) * 2007-06-25 2009-11-27 Airbus France Turboreacteur pour aeronef
US7856824B2 (en) * 2007-06-25 2010-12-28 Honeywell International Inc. Cooling systems for use on aircraft
US8763363B2 (en) * 2007-07-06 2014-07-01 General Electric Company Method and system for cooling fluid in a turbine engine
FR2920483B1 (fr) * 2007-08-30 2009-10-30 Snecma Sa Generation d'electricite dans une turbomachine
US7946806B2 (en) * 2007-10-10 2011-05-24 United Technologies Corporation Gas turbine engine systems and related methods involving heat exchange
US9212623B2 (en) 2007-12-26 2015-12-15 United Technologies Corporation Heat exchanger arrangement for turbine engine
US8826641B2 (en) * 2008-01-28 2014-09-09 United Technologies Corporation Thermal management system integrated pylon
US8266889B2 (en) * 2008-08-25 2012-09-18 General Electric Company Gas turbine engine fan bleed heat exchanger system
GB0818047D0 (en) * 2008-10-03 2008-11-05 Rolls Royce Plc Turbine cooling system
US8181443B2 (en) * 2008-12-10 2012-05-22 Pratt & Whitney Canada Corp. Heat exchanger to cool turbine air cooling flow
KR20110125231A (ko) 2009-02-04 2011-11-18 퍼듀 리서치 파운데이션 금속 수소화물 저장 시스템용 핀 열교환기
US8778063B2 (en) 2009-02-04 2014-07-15 Purdue Research Foundation Coiled and microchannel heat exchangers for metal hydride storage systems
GB2468346B (en) * 2009-03-06 2011-06-22 Rolls Royce Plc Cooling system for an aero gas turbine engine
DE102009011924A1 (de) * 2009-03-10 2010-09-16 Rolls-Royce Deutschland Ltd & Co Kg Nebenstromkanal eines Turbofantriebwerks
GB0912270D0 (en) * 2009-07-15 2009-08-26 Rolls Royce Plc System for cooling cooling-air in a gas turbine engine
DE102009033755A1 (de) * 2009-07-17 2011-01-20 Rolls-Royce Deutschland Ltd & Co Kg Turbofantriebwerk
US8307662B2 (en) * 2009-10-15 2012-11-13 General Electric Company Gas turbine engine temperature modulated cooling flow
EP2336525B1 (fr) * 2009-12-21 2015-08-26 Techspace Aero S.A. Intégration d'un échangeur de chaleur air-liquide sur moteur
US8756910B2 (en) * 2009-12-31 2014-06-24 Rolls-Royce North American Technologies, Inc. Gas turbine engine and cooling system
US8910465B2 (en) 2009-12-31 2014-12-16 Rolls-Royce North American Technologies, Inc. Gas turbine engine and heat exchange system
US8256229B2 (en) * 2010-04-09 2012-09-04 United Technologies Corporation Rear hub cooling for high pressure compressor
US8266888B2 (en) * 2010-06-24 2012-09-18 Pratt & Whitney Canada Corp. Cooler in nacelle with radial coolant
EP2447543A1 (de) * 2010-10-27 2012-05-02 Siemens Aktiengesellschaft Axialverdichter und zugehöriges Betriebsverfahren
US8602717B2 (en) 2010-10-28 2013-12-10 United Technologies Corporation Compression system for turbomachine heat exchanger
US8784047B2 (en) * 2010-11-04 2014-07-22 Hamilton Sundstrand Corporation Gas turbine engine heat exchanger with tapered fins
US9051943B2 (en) 2010-11-04 2015-06-09 Hamilton Sundstrand Corporation Gas turbine engine heat exchanger fins with periodic gaps
US9410482B2 (en) * 2010-12-24 2016-08-09 Rolls-Royce North American Technologies, Inc. Gas turbine engine heat exchanger
US8397487B2 (en) 2011-02-28 2013-03-19 General Electric Company Environmental control system supply precooler bypass
US8789376B2 (en) * 2011-05-27 2014-07-29 General Electric Company Flade duct turbine cooling and power and thermal management
DE102011106965A1 (de) * 2011-07-08 2013-01-10 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinentriebwerk mit Wärmetauscher im Kerntriebwerksgehäuse
DE102011106961A1 (de) * 2011-07-08 2013-01-10 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinentriebwerk mit Kühlelementen am Kerntriebwerksgehäuse
US9045998B2 (en) 2011-12-12 2015-06-02 Honeywell International Inc. System for directing air flow to a plurality of plena
GB201121426D0 (en) 2011-12-14 2012-01-25 Rolls Royce Plc Controller
GB201121428D0 (en) * 2011-12-14 2012-01-25 Rolls Royce Plc Controller
US9222411B2 (en) 2011-12-21 2015-12-29 General Electric Company Bleed air and hot section component cooling air system and method
WO2013147953A1 (en) * 2011-12-30 2013-10-03 Rolls-Royce North American Technologies Inc. Aircraft propulsion gas turbine engine with heat exchange
US9109514B2 (en) 2012-01-10 2015-08-18 Hamilton Sundstrand Corporation Air recovery system for precooler heat-exchanger
US9243563B2 (en) * 2012-01-25 2016-01-26 Honeywell International Inc. Gas turbine engine in-board cooled cooling air system
US9267434B2 (en) 2012-01-29 2016-02-23 United Technologies Corporation Heat exchanger
US9394803B2 (en) * 2012-03-14 2016-07-19 United Technologies Corporation Bypass air-pump system within the core engine to provide air for an environmental control system in a gas turbine engine
US9267390B2 (en) 2012-03-22 2016-02-23 Honeywell International Inc. Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine
US9388739B2 (en) 2012-05-02 2016-07-12 Pratt & Whitney Canada Corp. Air cooler system for gas turbine engines
US9945252B2 (en) * 2012-07-05 2018-04-17 United Technologies Corporation Gas turbine engine oil tank with integrated packaging configuration
FR2993610B1 (fr) * 2012-07-19 2014-07-11 Snecma Refroidissement du circuit d'huile d'une turbomachine
US20140027097A1 (en) * 2012-07-30 2014-01-30 Ian Alexandre Araujo De Barros Heat Exchanger for an Intercooler and Water Extraction Apparatus
EP2900965B1 (en) * 2012-09-28 2017-11-22 United Technologies Corporation Gas turbine engine thermal management system for heat exchanger using bypass flow
US10385777B2 (en) * 2012-10-01 2019-08-20 United Technologies Corporation Bifurcated inlet scoop for gas turbine engine
US9714610B2 (en) * 2012-10-04 2017-07-25 United Technologies Corporation Low profile compressor bleed air-oil coolers
GB201220174D0 (en) * 2012-11-09 2012-12-26 Rolls Royce Plc Heat exchange arrangemnt
US9562475B2 (en) 2012-12-19 2017-02-07 Siemens Aktiengesellschaft Vane carrier temperature control system in a gas turbine engine
EP2971724B1 (en) * 2013-03-13 2020-05-06 Rolls-Royce North American Technologies, Inc. Compact actuation system for a gas turbine engine exhaust nozzle
EP2971688B1 (en) * 2013-03-14 2018-11-28 United Technologies Corporation Gas turbine engine disclosing a heat shield and method of mounting this heat shield
WO2014151685A1 (en) * 2013-03-15 2014-09-25 United Technologies Corporation Gas turbine engine with air-oil cooler oil tank
US9429072B2 (en) 2013-05-22 2016-08-30 General Electric Company Return fluid air cooler system for turbine cooling with optional power extraction
US9422063B2 (en) 2013-05-31 2016-08-23 General Electric Company Cooled cooling air system for a gas turbine
US20160215732A1 (en) * 2013-09-24 2016-07-28 United Technologies Corporation Bypass duct heat exchanger placement
RU2550224C1 (ru) * 2013-11-25 2015-05-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Газотурбинный двигатель
US10287983B2 (en) * 2014-01-07 2019-05-14 United Technologies Corporation Cross-stream heat exchanger
GB201406952D0 (en) * 2014-04-17 2014-06-04 Rolls Royce Plc Open rotor propulsion engine
US10066550B2 (en) 2014-05-15 2018-09-04 Rolls-Royce North American Technologies, Inc. Fan by-pass duct for intercooled turbo fan engines
US20150354465A1 (en) * 2014-06-06 2015-12-10 United Technologies Corporation Turbine stage cooling
WO2016063311A1 (ja) * 2014-10-21 2016-04-28 住友精密工業株式会社 航空機エンジン用の熱交換器
JP6174655B2 (ja) 2014-10-21 2017-08-02 ユナイテッド テクノロジーズ コーポレイションUnited Technologies Corporation ガスタービンエンジン用のダクテッド熱交換器システム、およびガスタービンエンジン用の熱交換器の製造方法
US11236639B2 (en) * 2015-02-10 2022-02-01 Raytheon Technologies Corporation Gas turbine engine and an airflow control system
US20160237905A1 (en) * 2015-02-12 2016-08-18 United Technologies Corporation Intercooled cooling air
US11808210B2 (en) 2015-02-12 2023-11-07 Rtx Corporation Intercooled cooling air with heat exchanger packaging
US10731560B2 (en) * 2015-02-12 2020-08-04 Raytheon Technologies Corporation Intercooled cooling air
US20170082028A1 (en) * 2015-02-12 2017-03-23 United Technologies Corporation Intercooled cooling air using existing heat exchanger
US20160237908A1 (en) * 2015-02-12 2016-08-18 United Technologies Corporation Intercooled cooling air using existing heat exchanger
US20160237907A1 (en) * 2015-02-12 2016-08-18 United Technologies Corporation Intercooled cooling air with auxiliary compressor control
US10371055B2 (en) 2015-02-12 2019-08-06 United Technologies Corporation Intercooled cooling air using cooling compressor as starter
US10221862B2 (en) 2015-04-24 2019-03-05 United Technologies Corporation Intercooled cooling air tapped from plural locations
US10480419B2 (en) 2015-04-24 2019-11-19 United Technologies Corporation Intercooled cooling air with plural heat exchangers
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
CA2936633C (en) 2015-08-12 2021-12-28 Rolls-Royce North American Technologies, Inc. Heat exchanger for a gas turbine engine propulsion system
US10443508B2 (en) 2015-12-14 2019-10-15 United Technologies Corporation Intercooled cooling air with auxiliary compressor control
US9976479B2 (en) * 2015-12-15 2018-05-22 General Electric Company Power plant including a static mixer and steam generating system via turbine extraction and compressor extraction
US9890710B2 (en) * 2015-12-15 2018-02-13 General Electric Company Power plant with steam generation via combustor gas extraction
US9970354B2 (en) * 2015-12-15 2018-05-15 General Electric Company Power plant including an ejector and steam generating system via turbine extraction and compressor extraction
US10072573B2 (en) * 2015-12-15 2018-09-11 General Electric Company Power plant including an ejector and steam generating system via turbine extraction
US9964035B2 (en) * 2015-12-15 2018-05-08 General Electric Company Power plant including exhaust gas coolant injection system and steam generating system via turbine extraction
US20170184027A1 (en) * 2015-12-29 2017-06-29 General Electric Company Method and system for compressor and turbine cooling
US10125684B2 (en) 2015-12-29 2018-11-13 Pratt & Whitney Canada Corp. Surface cooler for aero engine
US20170307311A1 (en) * 2016-04-26 2017-10-26 United Technologies Corporation Simple Heat Exchanger Using Super Alloy Materials for Challenging Applications
RU2623854C1 (ru) * 2016-07-06 2017-06-29 Публичное акционерное общество "Научно-производственное объединение "Сатурн" Способ смазки и охлаждения передней опоры ротора газотурбинного двигателя
US10436115B2 (en) * 2016-08-22 2019-10-08 United Technologies Corporation Heat exchanger for gas turbine engine with support damper mounting
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
FR3060057B1 (fr) * 2016-12-14 2019-08-30 Safran Aircraft Engines Circuit fluidique dans une turbomachine
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
US10837364B2 (en) * 2017-01-27 2020-11-17 Raytheon Technologies Corporation Thermal shield for gas turbine engine diffuser case
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
US11268444B2 (en) * 2017-05-18 2022-03-08 Raytheon Technologies Corporation Turbine cooling arrangement
US10364750B2 (en) * 2017-10-30 2019-07-30 General Electric Company Thermal management system
GB201718796D0 (en) * 2017-11-14 2017-12-27 Rolls Royce Plc Gas turbine engine having an air-oil heat exchanger
FR3075865B1 (fr) * 2017-12-21 2020-07-17 Safran Nacelles Ensemble propulsif pour aeronef et procede de ventilation d’une enceinte moteur
US11725584B2 (en) 2018-01-17 2023-08-15 General Electric Company Heat engine with heat exchanger
RU2679573C1 (ru) * 2018-02-16 2019-02-11 Валерий Николаевич Сиротин Система охлаждения подшипников турбин газотурбинного двигателя
US10738703B2 (en) 2018-03-22 2020-08-11 Raytheon Technologies Corporation Intercooled cooling air with combined features
US10808572B2 (en) * 2018-04-02 2020-10-20 General Electric Company Cooling structure for a turbomachinery component
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
CN110513162B (zh) * 2018-05-22 2022-06-14 通用电气公司 斗式入口
RU187493U1 (ru) * 2018-05-28 2019-03-11 Публичное Акционерное Общество "Одк-Сатурн" Устройство охлаждения теплообменника
US10718233B2 (en) 2018-06-19 2020-07-21 Raytheon Technologies Corporation Intercooled cooling air with low temperature bearing compartment air
US11060484B2 (en) * 2018-06-29 2021-07-13 The Boeing Company Nozzle wall for an air-breathing engine of a vehicle and method therefor
US11255268B2 (en) 2018-07-31 2022-02-22 Raytheon Technologies Corporation Intercooled cooling air with selective pressure dump
US11300002B2 (en) 2018-12-07 2022-04-12 Pratt & Whitney Canada Corp. Static take-off port
US11078837B2 (en) * 2019-02-06 2021-08-03 Raytheon Technologies Corporation Engine bleed air ducting into heat exchanger
BE1027057B1 (fr) * 2019-02-18 2020-09-14 Safran Aero Boosters Sa Échangeur de chaleur air-huile
US11174816B2 (en) 2019-02-25 2021-11-16 Rolls-Royce Corporation Bypass duct conformal heat exchanger array
FR3096444B1 (fr) 2019-05-20 2021-05-07 Safran Systeme d’echange de chaleur optimise
FR3096409B1 (fr) 2019-05-20 2021-04-30 Safran Systeme d’echange de chaleur optimise
US11492971B2 (en) * 2019-09-06 2022-11-08 Raytheon Technologies Corporation Turbine engine system with heat exchanger in bypassable secondary duct
CN111577466A (zh) * 2020-06-22 2020-08-25 中国航空发动机研究院 航空发动机防冰引气预热与涡轮冷却引气预冷系统
CN112228226A (zh) * 2020-10-16 2021-01-15 中国航发四川燃气涡轮研究院 一种航空发动机涡轮转子冷却热管理系统
US11788469B2 (en) 2020-11-16 2023-10-17 General Electric Company Thermal management system for a gas turbine engine
US11512639B2 (en) * 2021-01-26 2022-11-29 General Electric Company Heat transfer system
US11965463B2 (en) * 2021-02-16 2024-04-23 Pratt & Whitney Canada Corp. Fluid cooler installation and method for turbofan engine
US11788470B2 (en) 2021-03-01 2023-10-17 General Electric Company Gas turbine engine thermal management
US11591965B2 (en) 2021-03-29 2023-02-28 General Electric Company Thermal management system for transferring heat between fluids
US11674396B2 (en) 2021-07-30 2023-06-13 General Electric Company Cooling air delivery assembly
US12410752B2 (en) 2021-09-23 2025-09-09 General Electric Company System and method of detecting an airflow fault condition
US11702958B2 (en) 2021-09-23 2023-07-18 General Electric Company System and method of regulating thermal transport bus pressure
FR3132328B1 (fr) * 2022-02-01 2024-01-12 Safran Echangeur de chaleur equipe d’un systeme de diffusion d’air et turbomachine correspondante
CN114876644B (zh) * 2022-05-09 2024-01-19 北京航空航天大学 一种周期性多孔承力支板
US12253033B2 (en) 2022-10-04 2025-03-18 General Electric Company Hydrogen fuel leak detection system for a vehicle
US12410753B2 (en) 2022-11-01 2025-09-09 General Electric Company Gas turbine engine
US12392290B2 (en) 2022-11-01 2025-08-19 General Electric Company Gas turbine engine
US12428992B2 (en) 2022-11-01 2025-09-30 General Electric Company Gas turbine engine
US12196131B2 (en) 2022-11-01 2025-01-14 General Electric Company Gas turbine engine
US12503980B2 (en) 2022-11-01 2025-12-23 General Electric Company Gas turbine engine
US12535033B2 (en) 2022-11-01 2026-01-27 General Electric Company Gas turbine engine
US12173651B2 (en) * 2023-05-15 2024-12-24 Rtx Corporation Pressure control for bifurcated flow of a turbine engine
US11976595B1 (en) * 2023-06-13 2024-05-07 Pratt & Whitney Canada Corp. Gas turbine engine with air/oil cooler having an airflow control baffle
US20250305454A1 (en) * 2024-03-28 2025-10-02 General Electric Company Gas turbine engine with heat exchanger assembly
FR3165286A1 (fr) * 2024-08-05 2026-02-06 Safran Aircraft Engines Carter interne à conduites d’échangeur thermique intégrées
US12540551B1 (en) 2025-07-01 2026-02-03 General Electric Company Gas turbine engines including splittered airfoils

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3034298A (en) * 1958-06-12 1962-05-15 Gen Motors Corp Turbine cooling system
US3224194A (en) * 1963-06-26 1965-12-21 Curtiss Wright Corp Gas turbine engine
US3528250A (en) * 1969-04-16 1970-09-15 Gen Motors Corp Bypass engine with afterburning and compressor bleed air heat exchanger in bypass duct
DE1951356C3 (de) * 1969-10-11 1980-08-28 Mtu Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Gasturbinentriebwerk für Flugzeuge
US3584458A (en) * 1969-11-25 1971-06-15 Gen Motors Corp Turbine cooling
GB1322405A (en) * 1970-10-02 1973-07-04 Secr Defence Oil systems for gas turbine engines
US3842597A (en) * 1973-03-16 1974-10-22 Gen Electric Gas turbine engine with means for reducing the formation and emission of nitrogen oxides

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JPS5452216A (en) 1979-04-24
US4254618A (en) 1981-03-10
FR2400618A1 (fr) 1979-03-16
IT7826716A0 (it) 1978-08-11
DE2835903A1 (de) 1979-03-01

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