PL3128155T3 - Zespół silnika turbośmigłowego z połączonym wylotem silnika i układu chłodzenia - Google Patents

Zespół silnika turbośmigłowego z połączonym wylotem silnika i układu chłodzenia

Info

Publication number
PL3128155T3
PL3128155T3 PL16183252T PL16183252T PL3128155T3 PL 3128155 T3 PL3128155 T3 PL 3128155T3 PL 16183252 T PL16183252 T PL 16183252T PL 16183252 T PL16183252 T PL 16183252T PL 3128155 T3 PL3128155 T3 PL 3128155T3
Authority
PL
Poland
Prior art keywords
engine
cooling exhaust
turboprop
assembly
combined
Prior art date
Application number
PL16183252T
Other languages
English (en)
Inventor
Andre Julien
Jean Thomassin
Serge Dussault
Original Assignee
Pratt & Whitney Canada 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 Pratt & Whitney Canada Corp. filed Critical Pratt & Whitney Canada Corp.
Publication of PL3128155T3 publication Critical patent/PL3128155T3/pl

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38—Introducing air inside the jet
    • F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/04—Aircraft characterised by the type or position of power plants of piston type
    • B64D27/08—Aircraft characterised by the type or position of power plants of piston type within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/08—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of power plant cooling systems
    • B64D33/10—Radiator arrangement
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
    • F01N13/00—Exhaust or silencing apparatus characterised by constructional features
    • F01N13/08—Other arrangements or adaptations of exhaust conduits
    • F01N13/082—Other arrangements or adaptations of exhaust conduits of tailpipe, e.g. with means for mixing air with exhaust for exhaust cooling, dilution or evacuation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
    • F01N3/00—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust
    • F01N3/02—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust
    • F01N3/05—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of air, e.g. by mixing exhaust with air
    • F01N3/055—Exhaust or silencing apparatus having means for purifying, rendering innocuous, or otherwise treating exhaust for cooling, or for removing solid constituents of, exhaust by means of air, e.g. by mixing exhaust with air without contact between air and exhaust gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B53/14—Adaptations of engines for driving, or engine combinations with, other devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B61/00—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing
    • F02B61/04—Adaptations of engines for driving vehicles or for driving propellers; Combinations of engines with gearing for driving propellers
    • 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
    • F01N2260/00—Exhaust treating devices having provisions not otherwise provided for
    • F01N2260/02—Exhaust treating devices having provisions not otherwise provided for for cooling the device
    • F01N2260/022—Exhaust treating devices having provisions not otherwise provided for for cooling the device using air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01N—GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
    • F01N2270/00—Mixing air with exhaust gases
    • F01N2270/02—Mixing air with exhaust gases for cooling exhaust gases or the apparatus
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • F02B2053/005—Wankel engines
    • 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
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Toxicology (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
PL16183252T 2015-08-07 2016-08-08 Zespół silnika turbośmigłowego z połączonym wylotem silnika i układu chłodzenia PL3128155T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201562202275P 2015-08-07 2015-08-07
US15/227,506 US10267191B2 (en) 2015-08-07 2016-08-03 Turboprop engine assembly with combined engine and cooling exhaust
EP16183252.2A EP3128155B1 (en) 2015-08-07 2016-08-08 Turboprop engine assembly with combined engine and cooling exhaust

Publications (1)

Publication Number Publication Date
PL3128155T3 true PL3128155T3 (pl) 2019-07-31

Family

ID=56852068

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16183252T PL3128155T3 (pl) 2015-08-07 2016-08-08 Zespół silnika turbośmigłowego z połączonym wylotem silnika i układu chłodzenia

Country Status (7)

Country Link
US (2) US10267191B2 (pl)
EP (1) EP3128155B1 (pl)
CN (1) CN108138654B (pl)
CA (1) CA2938105C (pl)
ES (1) ES2712480T3 (pl)
PL (1) PL3128155T3 (pl)
WO (1) WO2017024393A1 (pl)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9771165B2 (en) 2015-06-25 2017-09-26 Pratt & Whitney Canada Corp. Compound engine assembly with direct drive of generator
US10253726B2 (en) 2015-08-07 2019-04-09 Pratt & Whitney Canada Corp. 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
US10267191B2 (en) 2015-08-07 2019-04-23 Pratt & Whitney Canada Corp. Turboprop engine assembly with combined engine and cooling exhaust
US10633104B2 (en) * 2017-05-17 2020-04-28 General Electric Company Hybrid-electric propulsion system for an aircraft
US10527012B2 (en) * 2017-06-29 2020-01-07 Pratt & Whitney Canada Corp. Engine assembly with engine and cooler compartments
CN211442740U (zh) * 2018-01-22 2020-09-08 张斌 喷气式垂直起落无人机
US10858115B2 (en) * 2018-02-19 2020-12-08 Pratt & Whitney Canada Corp. Aircraft with wheel well between heat exchangers of engine assembly
US10899433B2 (en) * 2018-07-10 2021-01-26 Pratt & Whitney Canada Corp. System and method for feathering an aircraft propeller
US11628942B2 (en) * 2019-03-01 2023-04-18 Pratt & Whitney Canada Corp. Torque ripple control for an aircraft power train
US10875660B1 (en) * 2019-06-05 2020-12-29 Pratt & Whitney Canada Corp. Aircraft power plant
KR102874401B1 (ko) * 2020-01-10 2025-10-22 한화에어로스페이스 주식회사 배기 덕트 및 이를 이용하는 배기 덕트 어셈블리와 비행체
US11820526B2 (en) * 2020-02-26 2023-11-21 Honda Motor Co., Ltd. Power supply apparatus for a flying body including a combustion gas and intake air heat exchanger
CN111469378A (zh) * 2020-04-23 2020-07-31 新昌县欧赛机械有限公司 一种高强度橡胶用双螺杆型配合设备
EP3904217B1 (en) * 2020-04-27 2022-09-28 LEONARDO S.p.A. Aircraft capable of hovering
US11719248B2 (en) * 2020-10-14 2023-08-08 Pratt & Whitney Canada Corp. Aircraft propulsion system with propeller and cooling fan
US11795837B2 (en) 2021-01-26 2023-10-24 General Electric Company Embedded electric machine
US11867121B2 (en) 2021-03-24 2024-01-09 General Electric Company Gas turbine engines with heat recovery systems
CN112977848B (zh) * 2021-03-30 2021-10-12 上海尚实能源科技有限公司 一种混合动力型涡桨发动机的动力系统
CN112937880B (zh) * 2021-03-30 2023-03-28 大连理工大学 一种飞机辅助动力装置尾喷管
CN113237663B (zh) * 2021-04-15 2023-07-04 西安航天动力试验技术研究所 一种高温燃气的冷空气插入式旋流掺混装置及方法
US12116898B2 (en) * 2023-01-26 2024-10-15 Pratt & Whitney Canada Corp. Ram air driven blade tip clearance control system for turboprop engines
US11952962B1 (en) * 2023-01-31 2024-04-09 Pratt & Whitney Canada Corp. Exhaust duct for gas turbine engine
FR3149311A1 (fr) * 2023-05-31 2024-12-06 Sas Beyond Aerospace Gaine d'air de gestion thermique pour les systèmes aéroportés à piles à combustibles

Family Cites Families (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2164545A (en) 1937-11-13 1939-07-04 Aviat Mfg Corp Airplane
FR864010A (fr) 1939-11-11 1941-04-16 Aviation Louis Breguet Sa Perfectionnements aux dispositifs de refroidissement des groupes motopropulseurs d'aéronefs
GB622768A (en) 1947-04-03 1949-05-06 Napier & Son Ltd Improvements in or relating to cooling apparatus for use with aero or other engines
US2593541A (en) 1947-04-03 1952-04-22 Napier & Son Ltd Cooling apparatus for use with aero or other engines
US4815282A (en) 1987-02-24 1989-03-28 Teledyne Industries, Inc. Turbocharged compund cycle ducted fan engine system
EP0440640A1 (en) 1988-04-28 1991-08-14 AlliedSignal Inc. Spinner ducted exhaust for pusher turboprop engines
US5012646A (en) 1988-11-28 1991-05-07 Machen, Inc. Turbine engine having combustor air precooler
US5284012A (en) 1991-05-16 1994-02-08 General Electric Company Nacelle cooling and ventilation system
US5265408A (en) 1992-02-13 1993-11-30 Allied-Signal Inc. Exhaust eductor cooling system
JPH06107295A (ja) 1992-09-29 1994-04-19 Toyota Motor Corp 航空機駆動用内燃機関の冷却装置
US5471834A (en) * 1994-02-14 1995-12-05 Kapich; Davorin Engine driven propulsion fan with turbochargers in series
ES2199243T3 (es) 1994-03-01 2004-02-16 Auxiliary Power Dynamics, Llc Sistema compacto de suministro de energia auxiliar para motor diesel de gran potencia.
JP3525538B2 (ja) * 1995-03-08 2004-05-10 株式会社デンソー 車両用内燃機関の冷却系装置
GB2301632B (en) 1995-03-18 1998-06-24 Rolls Royce Plc Aircraft compound cycle propulsion engine
US5655359A (en) 1995-05-15 1997-08-12 The Boeing Company Passive cooling device and method for cooling an auxiliary power unit on an airplane
DE19524731A1 (de) 1995-07-07 1997-01-09 Bmw Rolls Royce Gmbh Turboprop-Triebwerk mit einem Luft-Ölkühler
US6430931B1 (en) 1997-10-22 2002-08-13 General Electric Company Gas turbine in-line intercooler
EP1141534B1 (en) 1999-01-04 2005-04-06 Allison Advanced Development Company Exhaust mixer and apparatus using same
FR2788308A1 (fr) * 1999-01-07 2000-07-13 Snecma Dispositif de refroidissement d'un reducteur de vitesse de turbomachine
US6615576B2 (en) 2001-03-29 2003-09-09 Honeywell International Inc. Tortuous path quiet exhaust eductor system
US6827104B2 (en) 2001-10-24 2004-12-07 Mcfarland Rory S. Seal and valve systems and methods for use in expanders and compressors of energy conversion systems
US6651929B2 (en) 2001-10-29 2003-11-25 Pratt & Whitney Canada Corp. Passive cooling system for auxiliary power unit installation
US6668553B1 (en) 2002-09-13 2003-12-30 Honeywell International Inc. Ejector-based cooling system for turbochargers
WO2004074653A1 (en) 2003-02-24 2004-09-02 Pratt & Whitney Canada Corp. Compact compound engine package
WO2004074655A1 (en) 2003-02-24 2004-09-02 Pratt & Whitney Canada Corp. Low volumetric compression ratio integrated turbo-compound rotary engine
ES2668356T3 (es) 2003-10-06 2018-05-17 Powersys, Llc Sistemas de generación energía y métodos de generación de energía
US7337605B2 (en) 2003-10-10 2008-03-04 Hamilton Sundstrand Corporation Thermal management for aircraft auxiliary power unit compartment
US7111462B2 (en) 2004-07-21 2006-09-26 Steward-Davis International, Inc. Onboard supplemental power system at varying high altitudes
US7089744B2 (en) 2004-07-21 2006-08-15 Steward Davis International, Inc. Onboard supplemental power system at varying high altitudes
US7637099B2 (en) * 2005-10-19 2009-12-29 Gm Global Technology Operations, Inc. Fluid entrainment apparatus
US7690189B2 (en) 2007-05-09 2010-04-06 United Technologies Corporation Aircraft combination engines inlet airflow control system
US7851102B2 (en) 2007-06-14 2010-12-14 Gm Global Technology Operations, Inc. Fuel cell stack compression retention system using overlapping sheets
US7836680B2 (en) 2007-06-20 2010-11-23 United Technologies Corporation Aircraft combination engines thermal management system
US7753036B2 (en) 2007-07-02 2010-07-13 United Technologies Corporation Compound cycle rotary engine
US7578369B2 (en) 2007-09-25 2009-08-25 Hamilton Sundstrand Corporation Mixed-flow exhaust silencer assembly
US8480460B2 (en) 2007-10-01 2013-07-09 United Technologies Corporation Cabin air supercharged aircraft internal combustion engine
US20090217643A1 (en) 2008-02-29 2009-09-03 Sokhey Jagdish S Gas discharge device for a vehicle engine
US9467021B2 (en) 2010-02-16 2016-10-11 Sine Waves, Inc. Engine and induction generator
US9027345B2 (en) 2011-07-28 2015-05-12 Pratt & Whitney Canada Corp. Compound engine system with rotary engine
WO2013054406A1 (ja) * 2011-10-12 2013-04-18 トヨタ自動車株式会社 車両前部構造
GB201202990D0 (en) 2012-02-22 2012-04-04 Rolls Royce Plc An auxiliary power system
CN102673793B (zh) 2012-06-08 2015-04-29 中国航空工业集团公司西安飞机设计研究所 一种飞机辅助动力装置排气引射系统
US9512721B2 (en) * 2012-07-20 2016-12-06 Pratt & Whitney Canada Corp. Compound cycle engine
FR2997726B1 (fr) * 2012-11-05 2018-03-02 Safran Aircraft Engines Carter de turbomachine
US8978628B2 (en) 2013-06-06 2015-03-17 The Boeing Company Engine cooling system
US9470442B2 (en) 2013-06-25 2016-10-18 Mcogen, Inc. Power generation system and method
US9771165B2 (en) 2015-06-25 2017-09-26 Pratt & Whitney Canada Corp. Compound engine assembly with direct drive of generator
US10696417B2 (en) 2015-06-25 2020-06-30 Pratt & Whitney Canada Corp. Auxiliary power unit with excess air recovery
US10590842B2 (en) 2015-06-25 2020-03-17 Pratt & Whitney Canada Corp. Compound engine assembly with bleed air
US10267191B2 (en) 2015-08-07 2019-04-23 Pratt & Whitney Canada Corp. Turboprop engine assembly with combined engine and cooling exhaust
US11214381B2 (en) 2015-08-07 2022-01-04 Pratt & Whitney Canada Corp. Aircraft heating assembly with liquid cooled internal combustion engine and heating element using waste heat
US10240521B2 (en) 2015-08-07 2019-03-26 Pratt & Whitney Canada Corp. Auxiliary power unit with variable speed ratio
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
US10961911B2 (en) * 2017-01-17 2021-03-30 Raytheon Technologies Corporation Injection cooled cooling air system for a gas turbine engine

Also Published As

Publication number Publication date
CA2938105C (en) 2023-12-12
EP3128155A1 (en) 2017-02-08
ES2712480T3 (es) 2019-05-13
CA2938105A1 (en) 2017-02-07
WO2017024393A1 (en) 2017-02-16
EP3128155B1 (en) 2019-02-06
US10267191B2 (en) 2019-04-23
CN108138654A (zh) 2018-06-08
CN108138654B (zh) 2020-06-05
US20190203620A1 (en) 2019-07-04
US20170037756A1 (en) 2017-02-09
US10927734B2 (en) 2021-02-23

Similar Documents

Publication Publication Date Title
PL3128155T3 (pl) Zespół silnika turbośmigłowego z połączonym wylotem silnika i układu chłodzenia
PL3135881T3 (pl) Zespół silnika z łączonym wyciągiem gazów spalinowych silnika i układu chłodzenia
GB201521937D0 (en) Gas turbine engine turbine cooling system
GB2536796B (en) Unducted fan for an aircraft turbine engine
GB201511454D0 (en) Aircraft engine nacelle
PL3572638T3 (pl) Silnik turbośmigłowy
GB2536357B (en) Gas turbine engine with gas bleed arrangement
PL3059387T3 (pl) Zespół silnika sprzężonego ze współosiową sekcją sprężarek i przesuniętą sekcją turbin
GB201520623D0 (en) Gas turbine engine
IL244983A0 (en) Combined turbo-jet and turbo-propeller engine
GB201512900D0 (en) Gas turbine engine
GB2544554B (en) Gas turbine engine
PL3321489T3 (pl) Konfiguracja pobierania powietrza gazowego silnika turbinowego
GB201617374D0 (en) Gas turbine engine
EP3108130A4 (en) Gas turbine engine having minimum cooling airflow
EP3043027B8 (en) Gas turbine engine component with conformal fillet cooling path
GB2544553B (en) Gas Turbine Engine
GB2566498B (en) Turbine exhaust case cooling
GB2564969B (en) Gas turbine engine
GB201605323D0 (en) Gas turbine engine fan assembly
GB201512494D0 (en) Gas turbine engine
GB201608234D0 (en) Gas turbine engine
EP3379052A4 (en) Engine with exhaust turbocharger
GB201520451D0 (en) Gas turbine engine
GB2565506B (en) Cooling structure for gas turbine engine