DE602008003368D1 - Vorrichtung zur Krafterzeugung, seine Verwendung, und Turbotriebwerk mit einer solchen Vorrichtung - Google Patents

Vorrichtung zur Krafterzeugung, seine Verwendung, und Turbotriebwerk mit einer solchen Vorrichtung

Info

Publication number
DE602008003368D1
DE602008003368D1 DE602008003368T DE602008003368T DE602008003368D1 DE 602008003368 D1 DE602008003368 D1 DE 602008003368D1 DE 602008003368 T DE602008003368 T DE 602008003368T DE 602008003368 T DE602008003368 T DE 602008003368T DE 602008003368 D1 DE602008003368 D1 DE 602008003368D1
Authority
DE
Germany
Prior art keywords
turbo
engine
generating power
generating
power
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.)
Active
Application number
DE602008003368T
Other languages
English (en)
Inventor
Claude Marcel M Mons
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602008003368D1 publication Critical patent/DE602008003368D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • 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
    • F01D17/00—Regulating or controlling by varying flow
    • F01D17/10—Final actuators
    • F01D17/12—Final actuators arranged in stator parts
    • F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
    • F01D17/141—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of shiftable members or valves obturating part of the flow path
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their 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
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/0215—Arrangements therefor, e.g. bleed or by-pass valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D27/00—Control, e.g. regulation, of pumps, pumping installations or pumping systems specially adapted for elastic fluids
    • F04D27/02—Surge control
    • F04D27/0207—Surge control by bleeding, bypassing or recycling fluids
    • F04D27/023—Details or means for fluid extraction
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/505—Shape memory behaviour
    • 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)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Temperature-Responsive Valves (AREA)
DE602008003368T 2007-09-05 2008-09-04 Vorrichtung zur Krafterzeugung, seine Verwendung, und Turbotriebwerk mit einer solchen Vorrichtung Active DE602008003368D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0706212A FR2920476B1 (fr) 2007-09-05 2007-09-05 Dispositif d'actionnement, systeme de decharge en etant equipe et turboreacteur les comportant

Publications (1)

Publication Number Publication Date
DE602008003368D1 true DE602008003368D1 (de) 2010-12-23

Family

ID=39327041

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602008003368T Active DE602008003368D1 (de) 2007-09-05 2008-09-04 Vorrichtung zur Krafterzeugung, seine Verwendung, und Turbotriebwerk mit einer solchen Vorrichtung

Country Status (7)

Country Link
US (1) US8448446B2 (de)
EP (1) EP2034134B1 (de)
JP (1) JP2009062993A (de)
CA (1) CA2639330C (de)
DE (1) DE602008003368D1 (de)
FR (1) FR2920476B1 (de)
RU (1) RU2472955C2 (de)

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WO2012151241A2 (en) * 2011-05-05 2012-11-08 The University Of Akron Thermal energy harvesting device
FR2976022B1 (fr) * 2011-05-31 2015-05-22 Snecma Turbomachine a vannes de decharge localisees au niveau du carter intermediaire
US9243563B2 (en) 2012-01-25 2016-01-26 Honeywell International Inc. Gas turbine engine in-board cooled cooling air system
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
FR2990241B1 (fr) * 2012-05-07 2014-06-06 Snecma Procede de montage ameliore d'un verin de commande d'une vanne de decharge d'air d'une turbomachine
US9518513B2 (en) 2012-10-12 2016-12-13 General Electric Company Gas turbine engine two degree of freedom variable bleed valve for ice extraction
US9297310B2 (en) * 2012-10-18 2016-03-29 General Electric Company Part load performance improvement using deformable bore plugs
US9982598B2 (en) 2012-10-22 2018-05-29 General Electric Company Gas turbine engine variable bleed valve for ice extraction
DE102013012377B4 (de) * 2013-07-25 2015-04-09 Astrium Gmbh Vorrichtung zum Öffnen oder Schließen eines Dichtsitzes eines Ventils und Verwendung in einem Antriebssystem
US10072584B2 (en) 2013-12-03 2018-09-11 United Technologies Corporation Multi-bypass stream gas turbine engine with enlarged bypass flow area
IT201600086511A1 (it) * 2016-08-22 2018-02-22 Gen Electric Sistemi di aspirazione dell'aria e relativi metodi di assemblaggio
US10233845B2 (en) * 2016-10-07 2019-03-19 General Electric Company Bleed valve assembly for a gas turbine engine
US10794272B2 (en) * 2018-02-19 2020-10-06 General Electric Company Axial and centrifugal compressor
US11053949B2 (en) * 2018-08-03 2021-07-06 Hamilton Sundstrand Corporation Passively controlled inline bleed valves
DE102019200593A1 (de) 2019-01-17 2020-07-23 Siemens Aktiengesellschaft Brennkammer
RU2716648C1 (ru) * 2019-07-16 2020-03-13 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ БЮДЖЕТНОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Брянский государственный технический университет" Охлаждаемая лопатка газовой турбины
CN110529351B (zh) * 2019-09-18 2021-04-09 新黎明科技股份有限公司 发电式闭门器及门
US11781506B2 (en) 2020-06-03 2023-10-10 Rtx Corporation Splitter and guide vane arrangement for gas turbine engines

Family Cites Families (21)

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Publication number Priority date Publication date Assignee Title
US2654994A (en) * 1948-11-08 1953-10-13 Lister & Co Ltd R A Control device for fuel systems
US3915587A (en) * 1973-09-27 1975-10-28 United Technologies Corp Variable size bleed port for jet engines
US4083181A (en) * 1976-06-14 1978-04-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with recirculating bleed
SU1025875A1 (ru) * 1981-01-09 1983-06-30 Всесоюзный научно-исследовательский и проектно-конструкторский институт геофизических исследований геологоразведочных скважин Тепловой привод скважинного прибора
JPS5981781U (ja) * 1982-11-25 1984-06-02 ナイルス部品株式会社 熱駆動ポンプ
JPS6037474A (ja) * 1983-08-08 1985-02-26 Keihin Seiki Mfg Co Ltd 制御弁
JPS6131786A (ja) * 1984-07-24 1986-02-14 Mitsubishi Electric Corp 弁装置
JPH0241352Y2 (de) * 1985-02-18 1990-11-02
JPS627980A (ja) * 1985-07-01 1987-01-14 Sanden Corp 熱駆動ポンプ
SU1397616A1 (ru) * 1986-11-28 1988-05-23 Д. А. Нестеренко Тепловой привод
US4841730A (en) * 1987-07-02 1989-06-27 Pda Engineering Thermal actuator
JPS6419078U (de) * 1987-07-23 1989-01-31
RU2027958C1 (ru) * 1991-11-21 1995-01-27 Физико-технический институт АН Туркменистана Насос с тепловым приводом
US5305616A (en) * 1992-03-23 1994-04-26 General Electric Company Gas turbine engine cooling system
US6048171A (en) * 1997-09-09 2000-04-11 United Technologies Corporation Bleed valve system
US6348067B1 (en) * 1998-11-25 2002-02-19 Israel Aircraft Industries Ltd. Method and system with shape memory heating apparatus for temporarily supporting a tubular organ
US6151897A (en) * 1999-04-06 2000-11-28 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Shape memory alloy actuator
US6832477B2 (en) * 2000-05-08 2004-12-21 Mark A Gummin Shape memory alloy actuator
US7249929B2 (en) * 2003-11-13 2007-07-31 United Technologies Corporation Bleed housing
US8348952B2 (en) * 2006-01-26 2013-01-08 Depuy International Ltd. System and method for cooling a spinal correction device comprising a shape memory material for corrective spinal surgery
US7823389B2 (en) * 2006-11-15 2010-11-02 General Electric Company Compound clearance control engine

Also Published As

Publication number Publication date
CA2639330C (fr) 2015-10-27
EP2034134B1 (de) 2010-11-10
JP2009062993A (ja) 2009-03-26
CA2639330A1 (fr) 2009-03-05
FR2920476B1 (fr) 2018-04-27
US20090056307A1 (en) 2009-03-05
RU2472955C2 (ru) 2013-01-20
EP2034134A1 (de) 2009-03-11
FR2920476A1 (fr) 2009-03-06
RU2008135875A (ru) 2010-03-10
US8448446B2 (en) 2013-05-28

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