UA97357C2 - Dual-flow turbomachine - Google Patents

Dual-flow turbomachine

Info

Publication number
UA97357C2
UA97357C2 UAA200810773A UAA200810773A UA97357C2 UA 97357 C2 UA97357 C2 UA 97357C2 UA A200810773 A UAA200810773 A UA A200810773A UA A200810773 A UAA200810773 A UA A200810773A UA 97357 C2 UA97357 C2 UA 97357C2
Authority
UA
Ukraine
Prior art keywords
dual
exchangers
radial arm
working chamber
flow
Prior art date
Application number
UAA200810773A
Other languages
English (en)
Ukrainian (uk)
Inventor
Ален ФУКО
Этьенн ЖЮШО
Арно ПЬЕРРО
Стефан Русселен
Original Assignee
Снекма
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 Снекма filed Critical Снекма
Publication of UA97357C2 publication Critical patent/UA97357C2/ru

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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/14—Combined heat and power generation [CHP]
    • 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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

Турбомашина содержит по меньшей мере один тепловой двигатель с циклом Стирлинга, который установлен на конце радиальной стойки (36) выходного кожуха (24) и содержит рабочую камеру (40), расположенную вне первичного (В) и вторичного (А) потоков, перемещаемый поршень (42), взаимодействующий с подвижным элементом (44) системы генерирования энергии, и два теплообменника, соответственно, нагревания (58) и охлаждения (62), выполненные в частях радиальной стойки, которые проходят соответственно через первичный поток (В) и через вторичный поток (А), при этом оба теплообменника (58, 62) соединяются друг с другом и с рабочей камерой (40) для циркуляции рабочей текучей среды.
UAA200810773A 2007-08-30 2008-08-29 Dual-flow turbomachine UA97357C2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0706072A FR2920483B1 (fr) 2007-08-30 2007-08-30 Generation d'electricite dans une turbomachine

Publications (1)

Publication Number Publication Date
UA97357C2 true UA97357C2 (en) 2012-02-10

Family

ID=39469574

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA200810773A UA97357C2 (en) 2007-08-30 2008-08-29 Dual-flow turbomachine

Country Status (10)

Country Link
US (1) US7685828B2 (ru)
EP (1) EP2031234B1 (ru)
JP (1) JP2009057969A (ru)
CN (1) CN101377175A (ru)
CA (1) CA2639217A1 (ru)
DE (1) DE602008002974D1 (ru)
ES (1) ES2354133T3 (ru)
FR (1) FR2920483B1 (ru)
RU (1) RU2470175C2 (ru)
UA (1) UA97357C2 (ru)

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US8144125B2 (en) 2006-03-30 2012-03-27 Cypress Semiconductor Corporation Apparatus and method for reducing average scan rate to detect a conductive object on a sensing device
US8144126B2 (en) 2007-05-07 2012-03-27 Cypress Semiconductor Corporation Reducing sleep current in a capacitance sensing system
US8596036B2 (en) * 2008-10-08 2013-12-03 The Invention Science Fund I Llc Hybrid propulsive engine including at least one independently rotatable compressor rotor
US20100126178A1 (en) * 2008-10-08 2010-05-27 Searete Llc, A Limited Liability Corporation Of The State Of Delaware Hybrid propulsive engine including at least one independently rotatable turbine stator
US20100083632A1 (en) * 2008-10-08 2010-04-08 Searete Llc, A Limited Liability Corporation Of The State Of Delaware Hybrid propulsive engine including at least one independently rotatable compressor rotor
US8291716B2 (en) * 2008-10-08 2012-10-23 The Invention Science Fund I Llc Hybrid propulsive engine including at least one independently rotatable turbine stator
JP5572471B2 (ja) * 2010-07-28 2014-08-13 川崎重工業株式会社 ガスタービンの中間冷却装置、これを用いたガスタービン
DE102011122071B4 (de) * 2011-12-22 2013-10-31 Eads Deutschland Gmbh Stirlingmotor mit Schlagflügel für ein emissionsfreies Fluggerät
CN106499514A (zh) * 2016-12-29 2017-03-15 深圳智慧能源技术有限公司 能回收燃机尾气热能和lng冷能的联合循环发电系统
US11371379B2 (en) 2017-08-22 2022-06-28 General Electric Company Turbomachine with alternatingly spaced turbine rotor blades
US11156128B2 (en) 2018-08-22 2021-10-26 General Electric Company Embedded electric machine
JP7269761B2 (ja) * 2019-03-15 2023-05-09 三菱重工業株式会社 原料流体の処理プラント、及び原料流体の処理方法
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

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US4254618A (en) * 1977-08-18 1981-03-10 General Electric Company Cooling air cooler for a gas turbofan engine
US4187675A (en) * 1977-10-14 1980-02-12 The United States Of America As Represented By The Secretary Of The Air Force Compact air-to-air heat exchanger for jet engine application
GB2041090A (en) * 1979-01-31 1980-09-03 Rolls Royce By-pass gas turbine engines
DE3031872A1 (de) * 1980-08-23 1982-04-01 Klöckner-Humboldt-Deutz AG, 5000 Köln Brennkraftmaschine mit einem zusatzmotor
SU1325179A1 (ru) * 1985-10-08 1987-07-23 Предприятие П/Я А-1619 Силова установка
US4796430A (en) * 1987-08-14 1989-01-10 Cryodynamics, Inc. Cam drive for cryogenic refrigerator
JPH01151724A (ja) * 1987-12-08 1989-06-14 Mitsubishi Heavy Ind Ltd スターリングエンジンとガスタービンの複合機関
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
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GB2301632B (en) * 1995-03-18 1998-06-24 Rolls Royce Plc Aircraft compound cycle propulsion engine
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TW426798B (en) * 1998-02-06 2001-03-21 Sanyo Electric Co Stirling apparatus
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FR2920482B1 (fr) * 2007-08-30 2009-10-30 Snecma Sa Ventilation et pressurisation de composants dans une turbomachine

Also Published As

Publication number Publication date
FR2920483B1 (fr) 2009-10-30
EP2031234A1 (fr) 2009-03-04
FR2920483A1 (fr) 2009-03-06
DE602008002974D1 (de) 2010-11-25
ES2354133T3 (es) 2011-03-10
CA2639217A1 (fr) 2009-02-28
RU2008135296A (ru) 2010-03-10
US20090058089A1 (en) 2009-03-05
EP2031234B1 (fr) 2010-10-13
RU2470175C2 (ru) 2012-12-20
US7685828B2 (en) 2010-03-30
JP2009057969A (ja) 2009-03-19
CN101377175A (zh) 2009-03-04

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