JP3727987B2 - ガスタービン燃焼器とガスタービン段との間の移行部材 - Google Patents
ガスタービン燃焼器とガスタービン段との間の移行部材 Download PDFInfo
- Publication number
- JP3727987B2 JP3727987B2 JP32613595A JP32613595A JP3727987B2 JP 3727987 B2 JP3727987 B2 JP 3727987B2 JP 32613595 A JP32613595 A JP 32613595A JP 32613595 A JP32613595 A JP 32613595A JP 3727987 B2 JP3727987 B2 JP 3727987B2
- Authority
- JP
- Japan
- Prior art keywords
- transition member
- gas turbine
- rear end
- outer portion
- transition
- 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
Links
Images
Classifications
-
- 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
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US35949594A | 1994-12-20 | 1994-12-20 | |
| US08/359495 | 1994-12-20 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JPH08261017A JPH08261017A (ja) | 1996-10-08 |
| JPH08261017A5 JPH08261017A5 (enExample) | 2005-11-04 |
| JP3727987B2 true JP3727987B2 (ja) | 2005-12-21 |
Family
ID=23414052
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP32613595A Expired - Fee Related JP3727987B2 (ja) | 1994-12-20 | 1995-12-15 | ガスタービン燃焼器とガスタービン段との間の移行部材 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US5761898A (enExample) |
| EP (1) | EP0718468B1 (enExample) |
| JP (1) | JP3727987B2 (enExample) |
| DE (1) | DE69523545T2 (enExample) |
Families Citing this family (78)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB9813972D0 (en) * | 1998-06-30 | 1998-08-26 | Rolls Royce Plc | A combustion chamber |
| US6427453B1 (en) * | 1998-07-31 | 2002-08-06 | The Texas A&M University System | Vapor-compression evaporative air conditioning systems and components |
| US7186101B2 (en) * | 1998-07-31 | 2007-03-06 | The Texas A&M University System | Gerotor apparatus for a quasi-isothermal Brayton cycle Engine |
| JP2002521608A (ja) | 1998-07-31 | 2002-07-16 | ザ・テキサス・エイ・アンド・エム・ユニバーシティ・システム | 準等温ブライトンサイクルエンジン |
| US7726959B2 (en) * | 1998-07-31 | 2010-06-01 | The Texas A&M University | Gerotor apparatus for a quasi-isothermal Brayton cycle engine |
| US6442946B1 (en) * | 2000-11-14 | 2002-09-03 | Power Systems Mfg., Llc | Three degrees of freedom aft mounting system for gas turbine transition duct |
| JP2002243154A (ja) * | 2001-02-16 | 2002-08-28 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器 |
| US20100003152A1 (en) * | 2004-01-23 | 2010-01-07 | The Texas A&M University System | Gerotor apparatus for a quasi-isothermal brayton cycle engine |
| BR0307457A (pt) * | 2002-02-05 | 2005-05-10 | Texas A & M Univ Sys | Aparelho gerotor para um motor de ciclo de brayton quasi-isotérmico |
| US6662567B1 (en) | 2002-08-14 | 2003-12-16 | Power Systems Mfg, Llc | Transition duct mounting system |
| DE10239534A1 (de) * | 2002-08-23 | 2004-04-22 | Man Turbomaschinen Ag | Heißgas führendes Gassammelrohr |
| US6644032B1 (en) * | 2002-10-22 | 2003-11-11 | Power Systems Mfg, Llc | Transition duct with enhanced profile optimization |
| US6860108B2 (en) * | 2003-01-22 | 2005-03-01 | Mitsubishi Heavy Industries, Ltd. | Gas turbine tail tube seal and gas turbine using the same |
| US7663283B2 (en) * | 2003-02-05 | 2010-02-16 | The Texas A & M University System | Electric machine having a high-torque switched reluctance motor |
| KR100908234B1 (ko) * | 2003-02-13 | 2009-07-20 | 삼성모바일디스플레이주식회사 | 전계 발광 표시 장치 및 이의 제조방법 |
| BRPI0518276A2 (pt) * | 2004-10-22 | 2008-11-11 | Texas A & M Univ Sys | aparelho gerotor para um motor de ciclo de brayton quase isotÉrmico |
| US7278254B2 (en) * | 2005-01-27 | 2007-10-09 | Siemens Power Generation, Inc. | Cooling system for a transition bracket of a transition in a turbine engine |
| US8015818B2 (en) * | 2005-02-22 | 2011-09-13 | Siemens Energy, Inc. | Cooled transition duct for a gas turbine engine |
| JP4476152B2 (ja) * | 2005-04-01 | 2010-06-09 | 三菱重工業株式会社 | ガスタービン燃焼器 |
| US7721547B2 (en) | 2005-06-27 | 2010-05-25 | Siemens Energy, Inc. | Combustion transition duct providing stage 1 tangential turning for turbine engines |
| US7377117B2 (en) | 2005-08-09 | 2008-05-27 | Turbine Services, Ltd. | Transition piece for gas turbine |
| US8001787B2 (en) * | 2007-02-27 | 2011-08-23 | Siemens Energy, Inc. | Transition support system for combustion transition ducts for turbine engines |
| US7757492B2 (en) * | 2007-05-18 | 2010-07-20 | General Electric Company | Method and apparatus to facilitate cooling turbine engines |
| US8240045B2 (en) * | 2007-05-22 | 2012-08-14 | Siemens Energy, Inc. | Gas turbine transition duct coupling apparatus |
| US8322146B2 (en) * | 2007-12-10 | 2012-12-04 | Alstom Technology Ltd | Transition duct assembly |
| US8418474B2 (en) * | 2008-01-29 | 2013-04-16 | Alstom Technology Ltd. | Altering a natural frequency of a gas turbine transition duct |
| US8276389B2 (en) * | 2008-09-29 | 2012-10-02 | Siemens Energy, Inc. | Assembly for directing combustion gas |
| US8230688B2 (en) * | 2008-09-29 | 2012-07-31 | Siemens Energy, Inc. | Modular transvane assembly |
| US8491259B2 (en) * | 2009-08-26 | 2013-07-23 | Siemens Energy, Inc. | Seal system between transition duct exit section and turbine inlet in a gas turbine engine |
| US8511972B2 (en) * | 2009-12-16 | 2013-08-20 | Siemens Energy, Inc. | Seal member for use in a seal system between a transition duct exit section and a turbine inlet in a gas turbine engine |
| US8978388B2 (en) | 2011-06-03 | 2015-03-17 | General Electric Company | Load member for transition duct in turbine system |
| US20120324898A1 (en) * | 2011-06-21 | 2012-12-27 | Mcmahan Kevin Weston | Combustor assembly for use in a turbine engine and methods of assembling same |
| US8448450B2 (en) | 2011-07-05 | 2013-05-28 | General Electric Company | Support assembly for transition duct in turbine system |
| US8650852B2 (en) | 2011-07-05 | 2014-02-18 | General Electric Company | Support assembly for transition duct in turbine system |
| JP5848074B2 (ja) * | 2011-09-16 | 2016-01-27 | 三菱日立パワーシステムズ株式会社 | ガスタービン、尾筒及び燃焼器 |
| US8459041B2 (en) | 2011-11-09 | 2013-06-11 | General Electric Company | Leaf seal for transition duct in turbine system |
| US8974179B2 (en) | 2011-11-09 | 2015-03-10 | General Electric Company | Convolution seal for transition duct in turbine system |
| US8701415B2 (en) | 2011-11-09 | 2014-04-22 | General Electric Company | Flexible metallic seal for transition duct in turbine system |
| US20130236301A1 (en) * | 2012-03-09 | 2013-09-12 | General Electric Company | Apparatus And System For Directing Hot Gas |
| US20130255276A1 (en) * | 2012-03-27 | 2013-10-03 | Alstom Technology Ltd. | Transition Duct Mounting System |
| US9506359B2 (en) | 2012-04-03 | 2016-11-29 | General Electric Company | Transition nozzle combustion system |
| US9038394B2 (en) | 2012-04-30 | 2015-05-26 | General Electric Company | Convolution seal for transition duct in turbine system |
| US9133722B2 (en) | 2012-04-30 | 2015-09-15 | General Electric Company | Transition duct with late injection in turbine system |
| US9249678B2 (en) | 2012-06-27 | 2016-02-02 | General Electric Company | Transition duct for a gas turbine |
| US8707673B1 (en) | 2013-01-04 | 2014-04-29 | General Electric Company | Articulated transition duct in turbomachine |
| US9322335B2 (en) | 2013-03-15 | 2016-04-26 | Siemens Energy, Inc. | Gas turbine combustor exit piece with hinged connections |
| US9080447B2 (en) | 2013-03-21 | 2015-07-14 | General Electric Company | Transition duct with divided upstream and downstream portions |
| US9458732B2 (en) | 2013-10-25 | 2016-10-04 | General Electric Company | Transition duct assembly with modified trailing edge in turbine system |
| US10072514B2 (en) | 2014-07-17 | 2018-09-11 | Siemens Energy, Inc. | Method and apparatus for attaching a transition duct to a turbine section in a gas turbine engine |
| US9359955B2 (en) * | 2014-08-28 | 2016-06-07 | Siemens Energy, Inc. | Apparatus and method incorporating a transition AFT support for a gas turbine engine |
| WO2016080957A1 (en) * | 2014-11-18 | 2016-05-26 | Siemens Aktiengesellschaft | Transition duct exit frame with insert |
| EP3783200B1 (en) | 2014-12-11 | 2024-03-06 | Siemens Energy Global GmbH & Co. KG | Transition duct for a gas turbine engine |
| US10520193B2 (en) | 2015-10-28 | 2019-12-31 | General Electric Company | Cooling patch for hot gas path components |
| US10260360B2 (en) * | 2016-03-24 | 2019-04-16 | General Electric Company | Transition duct assembly |
| US10260752B2 (en) | 2016-03-24 | 2019-04-16 | General Electric Company | Transition duct assembly with late injection features |
| US10227883B2 (en) | 2016-03-24 | 2019-03-12 | General Electric Company | Transition duct assembly |
| US10260424B2 (en) | 2016-03-24 | 2019-04-16 | General Electric Company | Transition duct assembly with late injection features |
| US10145251B2 (en) | 2016-03-24 | 2018-12-04 | General Electric Company | Transition duct assembly |
| US11428413B2 (en) | 2016-03-25 | 2022-08-30 | General Electric Company | Fuel injection module for segmented annular combustion system |
| US10584876B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system |
| US10655541B2 (en) | 2016-03-25 | 2020-05-19 | General Electric Company | Segmented annular combustion system |
| US10641491B2 (en) | 2016-03-25 | 2020-05-05 | General Electric Company | Cooling of integrated combustor nozzle of segmented annular combustion system |
| US10830442B2 (en) | 2016-03-25 | 2020-11-10 | General Electric Company | Segmented annular combustion system with dual fuel capability |
| US10563869B2 (en) | 2016-03-25 | 2020-02-18 | General Electric Company | Operation and turndown of a segmented annular combustion system |
| US10520194B2 (en) | 2016-03-25 | 2019-12-31 | General Electric Company | Radially stacked fuel injection module for a segmented annular combustion system |
| US10584880B2 (en) | 2016-03-25 | 2020-03-10 | General Electric Company | Mounting of integrated combustor nozzles in a segmented annular combustion system |
| US10605459B2 (en) | 2016-03-25 | 2020-03-31 | General Electric Company | Integrated combustor nozzle for a segmented annular combustion system |
| US11156362B2 (en) | 2016-11-28 | 2021-10-26 | General Electric Company | Combustor with axially staged fuel injection |
| US10690350B2 (en) | 2016-11-28 | 2020-06-23 | General Electric Company | Combustor with axially staged fuel injection |
| US11022240B2 (en) | 2017-06-12 | 2021-06-01 | General Electric Company | Cooling and insulating manifold seal assembly for a propulsion system |
| US11460191B2 (en) | 2020-08-31 | 2022-10-04 | General Electric Company | Cooling insert for a turbomachine |
| US11994293B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus support structure and method of manufacture |
| US11994292B2 (en) | 2020-08-31 | 2024-05-28 | General Electric Company | Impingement cooling apparatus for turbomachine |
| US11371702B2 (en) | 2020-08-31 | 2022-06-28 | General Electric Company | Impingement panel for a turbomachine |
| US11614233B2 (en) | 2020-08-31 | 2023-03-28 | General Electric Company | Impingement panel support structure and method of manufacture |
| US11255545B1 (en) | 2020-10-26 | 2022-02-22 | General Electric Company | Integrated combustion nozzle having a unified head end |
| DE112022001110T5 (de) * | 2021-02-18 | 2024-01-18 | Siemens Energy Global GmbH & Co. KG | Übergang mit unebener Fläche |
| US11767766B1 (en) | 2022-07-29 | 2023-09-26 | General Electric Company | Turbomachine airfoil having impingement cooling passages |
Family Cites Families (23)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2511432A (en) * | 1945-02-20 | 1950-06-13 | Power Jets Res & Dev Ltd | Support for multiple flame tubes |
| FR963256A (enExample) * | 1947-03-14 | 1950-07-05 | ||
| US2547619A (en) * | 1948-11-27 | 1951-04-03 | Gen Electric | Combustor with sectional housing and liner |
| US2748567A (en) * | 1949-10-13 | 1956-06-05 | Gen Motors Corp | Gas turbine combustion chamber with telescoping casing and liner sections |
| US2608057A (en) * | 1949-12-24 | 1952-08-26 | A V Roe Canada Ltd | Gas turbine nozzle box |
| US2765620A (en) * | 1951-06-23 | 1956-10-09 | Gen Motors Corp | Flow deflector for combustion chamber apparatus |
| US3657882A (en) * | 1970-11-13 | 1972-04-25 | Westinghouse Electric Corp | Combustion apparatus |
| US3750398A (en) * | 1971-05-17 | 1973-08-07 | Westinghouse Electric Corp | Static seal structure |
| US3759038A (en) * | 1971-12-09 | 1973-09-18 | Westinghouse Electric Corp | Self aligning combustor and transition structure for a gas turbine |
| CA1032480A (en) * | 1973-02-08 | 1978-06-06 | Josef Hoeltzenbein | Plate dialyzer |
| US4195474A (en) * | 1977-10-17 | 1980-04-01 | General Electric Company | Liquid-cooled transition member to turbine inlet |
| FR2422037A1 (fr) * | 1977-12-13 | 1979-11-02 | Alsthom Atlantique | Turbine a gaz |
| US4191011A (en) * | 1977-12-21 | 1980-03-04 | General Motors Corporation | Mount assembly for porous transition panel at annular combustor outlet |
| JPS5554636A (en) * | 1978-10-16 | 1980-04-22 | Hitachi Ltd | Combustor of gas turbine |
| US4232527A (en) * | 1979-04-13 | 1980-11-11 | General Motors Corporation | Combustor liner joints |
| US4422288A (en) * | 1981-03-02 | 1983-12-27 | General Electric Company | Aft mounting system for combustion transition duct members |
| US4465284A (en) * | 1983-09-19 | 1984-08-14 | General Electric Company | Scalloped cooling of gas turbine transition piece frame |
| US4640092A (en) * | 1986-03-03 | 1987-02-03 | United Technologies Corporation | Combustion chamber rear outer seal |
| US4785623A (en) * | 1987-12-09 | 1988-11-22 | United Technologies Corporation | Combustor seal and support |
| FR2624953B1 (fr) * | 1987-12-16 | 1990-04-20 | Snecma | Chambre de combustion, pour turbomachines, possedant un convergent a doubles parois |
| FR2677954B1 (fr) * | 1991-06-19 | 1993-09-10 | Snecma | Structure de suspension arriere du carter d'echappement d'un turboreacteur. |
| US5265412A (en) * | 1992-07-28 | 1993-11-30 | General Electric Company | Self-accommodating brush seal for gas turbine combustor |
| US5414999A (en) * | 1993-11-05 | 1995-05-16 | General Electric Company | Integral aft frame mount for a gas turbine combustor transition piece |
-
1995
- 1995-11-30 DE DE69523545T patent/DE69523545T2/de not_active Expired - Fee Related
- 1995-11-30 EP EP95308621A patent/EP0718468B1/en not_active Expired - Lifetime
- 1995-12-15 JP JP32613595A patent/JP3727987B2/ja not_active Expired - Fee Related
-
1996
- 1996-08-01 US US08/690,954 patent/US5761898A/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH08261017A (ja) | 1996-10-08 |
| US5761898A (en) | 1998-06-09 |
| DE69523545D1 (de) | 2001-12-06 |
| DE69523545T2 (de) | 2002-05-29 |
| EP0718468B1 (en) | 2001-10-31 |
| EP0718468A1 (en) | 1996-06-26 |
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