DE69616744D1 - Gasturbinenmotor - Google Patents

Gasturbinenmotor

Info

Publication number
DE69616744D1
DE69616744D1 DE69616744T DE69616744T DE69616744D1 DE 69616744 D1 DE69616744 D1 DE 69616744D1 DE 69616744 T DE69616744 T DE 69616744T DE 69616744 T DE69616744 T DE 69616744T DE 69616744 D1 DE69616744 D1 DE 69616744D1
Authority
DE
Germany
Prior art keywords
turbine engine
gas turbine
symmetrized
axis
rotary shaft
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.)
Expired - Fee Related
Application number
DE69616744T
Other languages
English (en)
Other versions
DE69616744T2 (de
Inventor
Takashi Bannai
Tsuneo Endou
Masahiko Izumi
Ken Ohya
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.)
Honda Motor Co Ltd
Original Assignee
Honda Motor Co Ltd
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 Honda Motor Co Ltd filed Critical Honda Motor Co Ltd
Application granted granted Critical
Publication of DE69616744D1 publication Critical patent/DE69616744D1/de
Publication of DE69616744T2 publication Critical patent/DE69616744T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • F02C3/05—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
    • 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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • F02C3/085—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage the turbine being of the radial-flow type (radial-radial)
    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0012—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the apparatus having an annular form
    • F28D9/0018—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the apparatus having an annular form without any annular circulation of the heat exchange media
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D9/00—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D9/0025—Heat-exchange apparatus having stationary plate-like or laminated conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits being formed by zig-zag bend plates
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
    • F05D2250/311—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being in line
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F2250/00—Arrangements for modifying the flow of the heat exchange media, e.g. flow guiding means; Particular flow patterns
    • F28F2250/10—Particular pattern of flow of the heat exchange media
    • F28F2250/102—Particular pattern of flow of the heat exchange media with change of flow direction
DE69616744T 1995-09-08 1996-08-02 Gasturbinenmotor Expired - Fee Related DE69616744T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP23091195 1995-09-08
JP8043567A JP3030689B2 (ja) 1995-09-08 1996-02-29 ガスタービンエンジン
PCT/JP1996/002179 WO1997009524A1 (fr) 1995-09-08 1996-08-02 Moteur de type turbine a gaz

Publications (2)

Publication Number Publication Date
DE69616744D1 true DE69616744D1 (de) 2001-12-13
DE69616744T2 DE69616744T2 (de) 2002-05-02

Family

ID=26383361

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69616744T Expired - Fee Related DE69616744T2 (de) 1995-09-08 1996-08-02 Gasturbinenmotor

Country Status (10)

Country Link
US (1) US5855112A (de)
EP (1) EP0796986B1 (de)
JP (1) JP3030689B2 (de)
KR (1) KR100316394B1 (de)
CN (1) CN1196107A (de)
AT (1) ATE208460T1 (de)
BR (1) BR9610369A (de)
CA (1) CA2229218C (de)
DE (1) DE69616744T2 (de)
WO (1) WO1997009524A1 (de)

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JP3685890B2 (ja) 1996-10-17 2005-08-24 本田技研工業株式会社 熱交換器
EP1138630A3 (de) * 1996-11-12 2003-04-02 Ammonia Casale S.A. Abdichtung zur Verwendung in einer Reformiervorrichtung
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US6276124B1 (en) * 1998-06-04 2001-08-21 Alliedsignal Inc. Bi-metallic tie-bolt for microturbine power generating system
JP3986685B2 (ja) * 1998-09-01 2007-10-03 本田技研工業株式会社 ガスタービンエンジン用燃焼器
US6155780A (en) * 1999-08-13 2000-12-05 Capstone Turbine Corporation Ceramic radial flow turbine heat shield with turbine tip seal
US6357113B1 (en) 1999-11-04 2002-03-19 Williams International Co., L.L.C. Method of manufacture of a gas turbine engine recuperator
US6293338B1 (en) 1999-11-04 2001-09-25 Williams International Co. L.L.C. Gas turbine engine recuperator
US6759764B1 (en) 2000-07-05 2004-07-06 Hybrid Power Generation Systems Llc Grid load logic
JP3494217B2 (ja) 2000-07-07 2004-02-09 川崎重工業株式会社 熱交換器を備えたガスタービン装置
US6463730B1 (en) 2000-07-12 2002-10-15 Honeywell Power Systems Inc. Valve control logic for gas turbine recuperator
US6408611B1 (en) 2000-08-10 2002-06-25 Honeywell International, Inc. Fuel control method for gas turbine
US6584760B1 (en) * 2000-09-12 2003-07-01 Hybrid Power Generation Systems, Inc. Emissions control in a recuperated gas turbine engine
US6622489B1 (en) 2000-10-25 2003-09-23 Hybrid Power Generation Systems, Llc Integrated gas booster modulation control method
US6513318B1 (en) 2000-11-29 2003-02-04 Hybrid Power Generation Systems Llc Low emissions gas turbine engine with inlet air heating
US6571563B2 (en) 2000-12-19 2003-06-03 Honeywell Power Systems, Inc. Gas turbine engine with offset shroud
US6536217B2 (en) 2000-12-20 2003-03-25 Honeywell Power Systems Inc. Liquid fuel reverse purge
WO2002052214A1 (fr) * 2000-12-25 2002-07-04 Honda Giken Kogyo Kabushiki Kaisha Echangeur thermique
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US6727603B1 (en) 2001-08-07 2004-04-27 Hybrid Power Generation Systems Llc Automatic mode transitions for microturbine generating systems
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JP2003074853A (ja) * 2001-08-28 2003-03-12 Honda Motor Co Ltd ガスタービン・エンジンの燃焼器
JP2003074856A (ja) * 2001-08-28 2003-03-12 Honda Motor Co Ltd ガスタービン・エンジンの燃焼器
JP2003074854A (ja) * 2001-08-28 2003-03-12 Honda Motor Co Ltd ガスタービン・エンジンの燃焼器
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US7007487B2 (en) * 2003-07-31 2006-03-07 Mes International, Inc. Recuperated gas turbine engine system and method employing catalytic combustion
US7065873B2 (en) * 2003-10-28 2006-06-27 Capstone Turbine Corporation Recuperator assembly and procedures
US7147050B2 (en) * 2003-10-28 2006-12-12 Capstone Turbine Corporation Recuperator construction for a gas turbine engine
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US7124572B2 (en) * 2004-09-14 2006-10-24 Honeywell International, Inc. Recuperator and turbine support adapter for recuperated gas turbine engines
US7574853B2 (en) * 2005-10-17 2009-08-18 Tma Power, Llc Microturbine with CHP system having a distillation apparatus
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US8118570B2 (en) * 2007-10-31 2012-02-21 Honeywell International Inc. Anisotropic bearing supports for turbochargers
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EP2673490A1 (de) * 2011-02-14 2013-12-18 ICR Turbine Engine Corporation Strahlenschutzschild für eine gasturbinenbrennkammer
US9394828B2 (en) * 2011-02-28 2016-07-19 Pratt & Whitney Canada Corp. Gas turbine engine recuperator with floating connection
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
CN102937049A (zh) * 2012-11-16 2013-02-20 中国石油大学(华东) 十字型排列的离心式微小型燃气轮机
CN103321748B (zh) * 2013-06-19 2016-03-16 北京理工大学 立式燃气轮机
JP2015152190A (ja) * 2014-02-12 2015-08-24 トヨタ自動車株式会社 ガスタービン用熱交換器
US10233838B2 (en) * 2014-09-09 2019-03-19 The United States Of America, As Represented By The Secretary Of The Navy Recuperated gas turbine engine
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CN105003339B (zh) * 2015-07-14 2017-04-12 张耀明 径向多级涡轮发动机
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FR3054200B1 (fr) * 2016-07-19 2021-08-13 Safran Landing Systems Ecran thermique de roue freinee d`aeronef perfore
GB2554384A (en) * 2016-09-23 2018-04-04 Hieta Tech Limited Combustion chamber and heat exchanger
GB201618016D0 (en) 2016-10-25 2016-12-07 Jiang Kyle Gas turbine engine
CN106762139B (zh) * 2017-01-22 2018-09-04 中国科学院工程热物理研究所 一种具有嵌入式叶片的燃气轮机
CN109139264A (zh) * 2017-06-28 2019-01-04 武汉迈科特微型涡轮机有限责任公司 一种应用环形回热器的微型涡轮发电机
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Also Published As

Publication number Publication date
CN1196107A (zh) 1998-10-14
EP0796986A4 (de) 1998-02-11
EP0796986A1 (de) 1997-09-24
JP3030689B2 (ja) 2000-04-10
DE69616744T2 (de) 2002-05-02
ATE208460T1 (de) 2001-11-15
EP0796986B1 (de) 2001-11-07
US5855112A (en) 1999-01-05
KR100316394B1 (ko) 2002-02-19
KR19990037711A (ko) 1999-05-25
CA2229218A1 (en) 1997-03-13
WO1997009524A1 (fr) 1997-03-13
CA2229218C (en) 2001-07-10
JPH09133029A (ja) 1997-05-20
BR9610369A (pt) 1999-07-06

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Legal Events

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8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee