PL2809904T3 - Sposób wyrzucania gazów spalinowych z turbiny gazowej oraz zespół wydechowy o zoptymalizowanej konfiguracji - Google Patents

Sposób wyrzucania gazów spalinowych z turbiny gazowej oraz zespół wydechowy o zoptymalizowanej konfiguracji

Info

Publication number
PL2809904T3
PL2809904T3 PL13706619T PL13706619T PL2809904T3 PL 2809904 T3 PL2809904 T3 PL 2809904T3 PL 13706619 T PL13706619 T PL 13706619T PL 13706619 T PL13706619 T PL 13706619T PL 2809904 T3 PL2809904 T3 PL 2809904T3
Authority
PL
Poland
Prior art keywords
exhaust
optimised
gas turbine
exiting
unit
Prior art date
Application number
PL13706619T
Other languages
English (en)
Inventor
Fabian Ammon
Alexandre Brisson
Guy Crabe
Jacques Demolis
Laurent Houssaye
Julien Munoz
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL2809904T3 publication Critical patent/PL2809904T3/pl

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
    • B01F—MIXING, e.g. DISSOLVING, EMULSIFYING OR DISPERSING
    • B01F25/00—Flow mixers; Mixers for falling materials, e.g. solid particles
    • B01F25/30—Injector mixers
    • B01F25/31—Injector mixers in conduits or tubes through which the main component flows
    • B01F25/314—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced at the circumference of the conduit
    • B01F25/3143—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced at the circumference of the conduit characterised by the specific design of the injector
    • B01F25/31432—Injector mixers in conduits or tubes through which the main component flows wherein additional components are introduced at the circumference of the conduit characterised by the specific design of the injector being a slit extending in the circumferential direction only
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F01D25/305—Exhaust heads, chambers, or the like with fluid, e.g. liquid injection
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/32—Inducing air flow by fluid jet, e.g. ejector action
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/60—Fluid transfer
    • F05B2260/601—Fluid transfer using an ejector or a jet pump
    • 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)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)
PL13706619T 2012-02-01 2013-02-01 Sposób wyrzucania gazów spalinowych z turbiny gazowej oraz zespół wydechowy o zoptymalizowanej konfiguracji PL2809904T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1250934A FR2986275B1 (fr) 2012-02-01 2012-02-01 Procede d'ejection de gaz d'echappement de turbine a gaz et ensemble d'echappement de configuration optimisee
EP13706619.7A EP2809904B1 (fr) 2012-02-01 2013-02-01 Procede d'ejection de gaz d'echappement de turbine a gaz et ensemble d'echappement de configuration optimisee
PCT/FR2013/050222 WO2013114058A1 (fr) 2012-02-01 2013-02-01 Procede d'ejection de gaz d'echappement de turbine a gaz et ensemble d'echappement de configuration optimisee

Publications (1)

Publication Number Publication Date
PL2809904T3 true PL2809904T3 (pl) 2018-03-30

Family

ID=47754808

Family Applications (1)

Application Number Title Priority Date Filing Date
PL13706619T PL2809904T3 (pl) 2012-02-01 2013-02-01 Sposób wyrzucania gazów spalinowych z turbiny gazowej oraz zespół wydechowy o zoptymalizowanej konfiguracji

Country Status (11)

Country Link
US (1) US9926809B2 (pl)
EP (1) EP2809904B1 (pl)
JP (1) JP6423718B2 (pl)
KR (1) KR102015154B1 (pl)
CN (1) CN104040147B (pl)
CA (1) CA2860080C (pl)
ES (1) ES2649019T3 (pl)
FR (1) FR2986275B1 (pl)
PL (1) PL2809904T3 (pl)
RU (1) RU2635001C2 (pl)
WO (1) WO2013114058A1 (pl)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
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FR3028888B1 (fr) * 2014-11-25 2016-12-09 Snecma Dispositif de refroidissement pour une turbomachine alimente par un circuit de decharge
CA2996285C (en) 2015-09-02 2023-10-31 Jetoptera, Inc. Ejector and airfoil configurations
US11965456B2 (en) * 2015-09-02 2024-04-23 Jetoptera, Inc. Fluidic turbo heater system
USD868627S1 (en) 2018-04-27 2019-12-03 Jetoptera, Inc. Flying car
US20170283080A1 (en) * 2015-09-02 2017-10-05 Jetoptera, Inc. Winglet ejector configurations
US10464668B2 (en) 2015-09-02 2019-11-05 Jetoptera, Inc. Configuration for vertical take-off and landing system for aerial vehicles
CN106988850A (zh) * 2017-03-15 2017-07-28 中国航空工业集团公司西安飞机设计研究所 一种飞机发动机排气管及具有其的飞机
CN108614920B (zh) * 2018-04-03 2021-10-12 同济大学 一种多台设备局部排风同时系数确定方法
RU2696521C1 (ru) * 2018-05-17 2019-08-02 Общество с ограниченной ответственностью "Газпром трансгаз Ухта" Способ снижения температуры воздуха в полости между коническим корпусом силовой турбины двигателя ал-31стн и внутренним корпусом улитки газоперекачивающего агрегата ц1-16л/76-1,44
US11105511B2 (en) * 2018-12-14 2021-08-31 General Electric Company Rotating detonation propulsion system
KR20200113593A (ko) * 2019-03-26 2020-10-07 이태준 배관 직결형 터보압축기
US11772783B2 (en) * 2020-05-19 2023-10-03 Lockheed Martin Corporation Turbine engine secondary ejector system
FR3143008B1 (fr) * 2022-12-09 2024-11-01 Airbus Helicopters Aéronef muni d’un moteur et d’un conduit d’échappement autour d’une tuyère d’éjection du moteur

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US4018046A (en) * 1975-07-17 1977-04-19 Avco Corporation Infrared radiation suppressor for gas turbine engine
US4178760A (en) * 1976-12-02 1979-12-18 Filterwerk Mann & Hummel Gmbh Filter dust ejector and check valve arrangement in exhaust system of internal combustion engine
SU1804042A1 (ru) * 1991-03-28 1994-01-15 Киевский механический завод им.О.К.Антонова Система охлаждения теплообменника двигателя
US5265408A (en) * 1992-02-13 1993-11-30 Allied-Signal Inc. Exhaust eductor cooling system
US5628623A (en) * 1993-02-12 1997-05-13 Skaggs; Bill D. Fluid jet ejector and ejection method
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
DE19619535C1 (de) * 1996-05-15 1997-10-30 Daimler Benz Aerospace Airbus Ejektor-Ölkühlsystem für ein Flugzeug-Hilfstriebwerk
US6092360A (en) * 1998-07-01 2000-07-25 The Boeing Company Auxiliary power unit passive cooling system
US6202413B1 (en) * 1999-02-04 2001-03-20 Cummins Engine Company, Inc. Multiple nozzle ejector for wastegated turbomachinery
US6651929B2 (en) * 2001-10-29 2003-11-25 Pratt & Whitney Canada Corp. Passive cooling system for auxiliary power unit installation
US7152410B2 (en) * 2004-06-10 2006-12-26 Honeywell International, Inc. System and method for dumping surge flow into eductor primary nozzle for free turbine
US20060059891A1 (en) * 2004-09-23 2006-03-23 Honeywell International, Inc. Quiet chevron/tab exhaust eductor system
US7500353B2 (en) * 2005-10-25 2009-03-10 Honeywell International Inc. Eductor swirl buster
EP2032829B1 (en) * 2006-06-09 2014-03-05 Bell Helicopter Textron Inc. Engine exhaust system with directional nozzle
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Also Published As

Publication number Publication date
ES2649019T3 (es) 2018-01-09
US20140373546A1 (en) 2014-12-25
CN104040147A (zh) 2014-09-10
CN104040147B (zh) 2017-04-05
RU2635001C2 (ru) 2017-11-08
US9926809B2 (en) 2018-03-27
KR102015154B1 (ko) 2019-08-27
KR20140116858A (ko) 2014-10-06
EP2809904A1 (fr) 2014-12-10
FR2986275B1 (fr) 2016-07-01
JP2015510070A (ja) 2015-04-02
CA2860080A1 (fr) 2013-08-08
FR2986275A1 (fr) 2013-08-02
JP6423718B2 (ja) 2018-11-14
RU2014127484A (ru) 2016-03-20
CA2860080C (fr) 2020-04-07
EP2809904B1 (fr) 2017-11-08
WO2013114058A1 (fr) 2013-08-08

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