CA2229218A1 - Gas-turbine engine - Google Patents

Gas-turbine engine

Info

Publication number
CA2229218A1
CA2229218A1 CA002229218A CA2229218A CA2229218A1 CA 2229218 A1 CA2229218 A1 CA 2229218A1 CA 002229218 A CA002229218 A CA 002229218A CA 2229218 A CA2229218 A CA 2229218A CA 2229218 A1 CA2229218 A1 CA 2229218A1
Authority
CA
Canada
Prior art keywords
axis
turbine engine
symmetrized
gas
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.)
Granted
Application number
CA002229218A
Other languages
French (fr)
Other versions
CA2229218C (en
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
Takashi Bannai
Tsuneo Endou
Masahiko Izumi
Ken Ohya
Honda Giken Kogyo Kabushiki Kaisha
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 Takashi Bannai, Tsuneo Endou, Masahiko Izumi, Ken Ohya, Honda Giken Kogyo Kabushiki Kaisha filed Critical Takashi Bannai
Publication of CA2229218A1 publication Critical patent/CA2229218A1/en
Application granted granted Critical
Publication of CA2229218C publication Critical patent/CA2229218C/en
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

Abstract

A gas turbine engine E includes a compressor wheel 9 and a turbine wheel 10 fixed to a rotary shaft 8, a can-type combustor 18 disposed on an extension of the axis L of the rotary shaft 8, and a circular plate-type heat exchanger 12 disposed to surround a radially outer portion of the can-type combustor 18. The compressor wheel 9, the turbine wheel 10, the can-type combustor 18 and the plate-type heat exchanger 12 are disposed coaxially with the axis L of the rotary shaft 8.
Therefore, the flows of compressed air and combustion gas are symmetrized with respect to the axis L, and the distribution of temperature within a casing is also symmetrized with respect to the axis L. Thus, the flows of compressed air and combustion gas within the gas turbine engine E can be axially symmetrized, and the generation of a thermal distortion can be prevented.
CA002229218A 1995-09-08 1996-08-02 Gas-turbine engine Expired - Fee Related CA2229218C (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
JP23091195 1995-09-08
JP230911/95 1995-09-08
JP43567/96 1996-02-29
JP8043567A JP3030689B2 (en) 1995-09-08 1996-02-29 Gas turbine engine
PCT/JP1996/002179 WO1997009524A1 (en) 1995-09-08 1996-08-02 Gas-turbine engine

Publications (2)

Publication Number Publication Date
CA2229218A1 true CA2229218A1 (en) 1997-03-13
CA2229218C CA2229218C (en) 2001-07-10

Family

ID=26383361

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002229218A Expired - Fee Related CA2229218C (en) 1995-09-08 1996-08-02 Gas-turbine engine

Country Status (10)

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

Families Citing this family (77)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0942865A (en) * 1995-07-28 1997-02-14 Honda Motor Co Ltd Heat exchanger
JP3685890B2 (en) * 1996-10-17 2005-08-24 本田技研工業株式会社 Heat exchanger
EP0841301B1 (en) * 1996-11-12 2004-03-17 Ammonia Casale S.A. Reforming apparatus
US5850732A (en) * 1997-05-13 1998-12-22 Capstone Turbine Corporation Low emissions combustion system for a gas turbine engine
DE19727730A1 (en) * 1997-06-30 1999-01-07 Abb Research Ltd Gas turbine construction
US6170251B1 (en) * 1997-12-19 2001-01-09 Mark J. Skowronski Single shaft microturbine power generating system including turbocompressor and auxiliary recuperator
TW390936B (en) * 1997-12-20 2000-05-21 Allied Signal Inc Microturbine power generating system
AU772937B2 (en) * 1999-06-22 2004-05-13 Honeywell International, Inc. Microturbine power generating system
US6276124B1 (en) * 1998-06-04 2001-08-21 Alliedsignal Inc. Bi-metallic tie-bolt for microturbine power generating system
JP3986685B2 (en) * 1998-09-01 2007-10-03 本田技研工業株式会社 Combustor for gas turbine engine
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 (en) * 2000-07-07 2004-02-09 川崎重工業株式会社 Gas turbine device with heat exchanger
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
DE60138964D1 (en) * 2000-12-25 2009-07-23 Honda Motor Co Ltd Heat Exchanger
SE520559C2 (en) * 2001-02-02 2003-07-22 Volvo Lastvagnar Ab Arrangement and procedure for compressed air systems for vehicles
US6430917B1 (en) 2001-02-09 2002-08-13 The Regents Of The University Of California Single rotor turbine engine
US6631080B2 (en) 2001-06-06 2003-10-07 Hybrid Power Generation Systems Llc Systems and methods for boosting DC link voltage in turbine generators
US6516263B1 (en) 2001-08-02 2003-02-04 Honeywell Power Systems Inc. Adaptive flame-out prevention
US6727603B1 (en) 2001-08-07 2004-04-27 Hybrid Power Generation Systems Llc Automatic mode transitions for microturbine generating systems
US6560965B1 (en) 2001-08-20 2003-05-13 Honeywell Power Systems Inc. System and method of cleaning a recuperator in a microturbine power system
JP2003074856A (en) * 2001-08-28 2003-03-12 Honda Motor Co Ltd Combustion equipment of gas-turbine engine
JP2003074853A (en) * 2001-08-28 2003-03-12 Honda Motor Co Ltd Combustion equipment of gas-turbine engine
JP2003074854A (en) * 2001-08-28 2003-03-12 Honda Motor Co Ltd Combustion equipment of gas-turbine engine
US6751958B1 (en) 2001-09-06 2004-06-22 Honeywell International Inc. Physical chemistry compression
US6711889B2 (en) * 2002-06-28 2004-03-30 Industrial Technology Research Institute Gas turbine engine
US7047722B2 (en) * 2002-10-02 2006-05-23 Claudio Filippone Small scale hybrid engine (SSHE) utilizing fossil fuels
US7185483B2 (en) * 2003-01-21 2007-03-06 General Electric Company Methods and apparatus for exchanging heat
US7044718B1 (en) 2003-07-08 2006-05-16 The Regents Of The University Of California Radial-radial single rotor turbine
US7007487B2 (en) * 2003-07-31 2006-03-07 Mes International, Inc. Recuperated gas turbine engine system and method employing catalytic combustion
US7147050B2 (en) * 2003-10-28 2006-12-12 Capstone Turbine Corporation Recuperator construction for a gas turbine engine
US7065873B2 (en) * 2003-10-28 2006-06-27 Capstone Turbine Corporation Recuperator assembly and procedures
GB2410982A (en) * 2004-02-14 2005-08-17 Richard Julius Gozdawa Turbomachinery electric generator arrangement with component cooling
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
US7363762B2 (en) * 2005-11-16 2008-04-29 General Electric Company Gas turbine engines seal assembly and methods of assembling the same
US7341429B2 (en) * 2005-11-16 2008-03-11 General Electric Company Methods and apparatuses for cooling gas turbine engine rotor assemblies
US7574870B2 (en) 2006-07-20 2009-08-18 Claudio Filippone Air-conditioning systems and related methods
US8118570B2 (en) * 2007-10-31 2012-02-21 Honeywell International Inc. Anisotropic bearing supports for turbochargers
US20090282804A1 (en) * 2008-05-16 2009-11-19 Honeywell International Inc. Recuperators for gas turbine engines
US8221073B2 (en) * 2008-12-22 2012-07-17 Pratt & Whitney Canada Corp. Exhaust gas discharge system and plenum
FR2950109B1 (en) * 2009-09-17 2012-07-27 Turbomeca TURBOMOTEUR WITH PARALLEL TREES
JP5023107B2 (en) * 2009-06-25 2012-09-12 株式会社日立製作所 Regenerative cycle gas turbine system
JP5457218B2 (en) * 2010-02-12 2014-04-02 新潟原動機株式会社 Regenerative cycle gas turbine equipment
DE102010010272A1 (en) * 2010-03-05 2011-09-08 Daimler Ag Device for providing hot exhaust gases
US20120260662A1 (en) * 2011-02-14 2012-10-18 Icr Turbine Engine Corporation Radiation shield for a gas turbine combustor
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 (en) * 2012-11-16 2013-02-20 中国石油大学(华东) Cross arranged centrifugal micro-type gas turbine
CN103321748B (en) * 2013-06-19 2016-03-16 北京理工大学 Verticle gas turbine
JP2015152190A (en) * 2014-02-12 2015-08-24 トヨタ自動車株式会社 gas turbine heat exchanger
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
DE102014220296A1 (en) * 2014-10-07 2016-04-07 Dürr Systems GmbH (Micro) gas turbine assembly
CN105003339B (en) * 2015-07-14 2017-04-12 张耀明 Radial multistage turbine engine
US9745992B2 (en) 2015-08-30 2017-08-29 Honeywell International Inc. Turbocharger bearing damper assembly
US10844742B2 (en) 2016-04-18 2020-11-24 Borgwarner Inc. Heat shield
FR3054200B1 (en) * 2016-07-19 2021-08-13 Safran Landing Systems PERFORATED AIRCRAFT BRAKE WHEEL THERMAL SCREEN
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 (en) * 2017-01-22 2018-09-04 中国科学院工程热物理研究所 A kind of gas turbine with embedded blade
CN109139264A (en) * 2017-06-28 2019-01-04 武汉迈科特微型涡轮机有限责任公司 A kind of micro turbine generator for applying annular regenerator
US10502424B2 (en) * 2017-08-10 2019-12-10 General Electric Company Volute combustor for gas turbine engine
GB2573131A (en) * 2018-04-25 2019-10-30 Hieta Tech Limited Combined heat and power system
CN109113871B (en) * 2018-10-15 2024-03-15 上海和兰透平动力技术有限公司 Gas turbine of the regenerative type
US11255266B2 (en) 2019-05-14 2022-02-22 Raytheon Technologies Corporation Recuperated cycle engine
US11136901B2 (en) * 2019-05-17 2021-10-05 Raytheon Technologies Corporation Monolithic combustor for attritiable engine applications
WO2021163760A1 (en) * 2020-02-19 2021-08-26 Nathan Geoffrey Andrews A compact turbine-compressor assembly
US20240110519A1 (en) * 2022-09-30 2024-04-04 Raytheon Technologies Corporation Centrifugally pumped fuel system

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2553867A (en) * 1946-05-24 1951-05-22 Continental Aviat & Engineerin Power plant
US3831374A (en) * 1971-08-30 1974-08-27 Power Technology Corp Gas turbine engine and counterflow heat exchanger with outer air passageway
US3818984A (en) * 1972-01-31 1974-06-25 Nippon Denso Co Heat exchanger
US4141212A (en) * 1977-06-20 1979-02-27 Avco Corporation Differentially geared regenerative reverse flow turbo shaft engine
DE2744899C3 (en) * 1977-10-06 1982-02-11 Kernforschungsanlage Jülich GmbH, 5170 Jülich Gas turbine system for driving vehicles
JPS5681229A (en) * 1979-12-04 1981-07-03 Nissan Motor Co Ltd Two-shaft gas turbine power generator
JPS584172A (en) * 1981-07-01 1983-01-11 Ricoh Co Ltd Drum-like photosensitive element for electro- photographic copying machine
JPS5855331A (en) * 1981-09-22 1983-04-01 Seiichi Kondo Hydrophobic silica gel and its manufacture
JPS6014017A (en) * 1983-07-05 1985-01-24 Toshiba Corp Gas turbine combustor
JPH01290926A (en) * 1988-05-19 1989-11-22 Nissan Motor Co Ltd Heat exchanger
JPH02153231A (en) * 1988-12-02 1990-06-12 Ishikawajima Harima Heavy Ind Co Ltd Gas turbine
JPH076403B2 (en) * 1989-03-09 1995-01-30 日産自動車株式会社 gas turbine
US5050668A (en) * 1989-09-11 1991-09-24 Allied-Signal Inc. Stress relief for an annular recuperator
US5004044A (en) * 1989-10-02 1991-04-02 Avco Corporation Compact rectilinear heat exhanger
JPH0629479Y2 (en) * 1990-06-14 1994-08-10 川崎重工業株式会社 Gas turbine engine
CH687269A5 (en) * 1993-04-08 1996-10-31 Abb Management Ag Gas turbine group.

Also Published As

Publication number Publication date
JPH09133029A (en) 1997-05-20
EP0796986A1 (en) 1997-09-24
DE69616744D1 (en) 2001-12-13
US5855112A (en) 1999-01-05
WO1997009524A1 (en) 1997-03-13
EP0796986A4 (en) 1998-02-11
CN1196107A (en) 1998-10-14
BR9610369A (en) 1999-07-06
EP0796986B1 (en) 2001-11-07
CA2229218C (en) 2001-07-10
KR100316394B1 (en) 2002-02-19
ATE208460T1 (en) 2001-11-15
JP3030689B2 (en) 2000-04-10
KR19990037711A (en) 1999-05-25
DE69616744T2 (en) 2002-05-02

Similar Documents

Publication Publication Date Title
CA2229218A1 (en) Gas-turbine engine
US7384236B2 (en) Exhaust-gas-turbine casing
CA2119519C (en) Gas turbine group
US4251185A (en) Expansion control ring for a turbine shroud assembly
US7007482B2 (en) Combustion liner seal with heat transfer augmentation
US6334298B1 (en) Gas turbine combustor having dome-to-liner joint
CA2048764C (en) Fuel injector nozzle support
US3831374A (en) Gas turbine engine and counterflow heat exchanger with outer air passageway
CA2522950C (en) Methods and apparatus for cooling gas turbine engines
KR950011818A (en) Gas turbine combustor
CA2288555A1 (en) Gas turbine combustor
US5079911A (en) Gas-turbine power plant
EP0701093A3 (en) Catalytic combustion method for a gas turbine
US5085038A (en) Gas turbine engine
CA2343888A1 (en) Sealing device for segmented stator ring
US6357113B1 (en) Method of manufacture of a gas turbine engine recuperator
CA1113263A (en) Double wall combustion chamber for a combustion turbine
US4373326A (en) Ceramic duct system for turbine engine
CA1037267A (en) Recuperative mounting
US5182904A (en) Gas turbine engine power unit
US7360364B2 (en) Method and apparatus for assembling gas turbine engine combustors
RU94001662A (en) GAS TURBINE ENGINE
CA1097285A (en) Insulated hub arrangement for high temperature centrifugal fan
JP2895831B1 (en) Gas turbine with improved scroll cooling
GB2017222A (en) Gas Turbine Unit

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed