RU2540350C2 - Переходная область между вторичной камерой сгорания и турбиной низкого давления газовой турбины - Google Patents

Переходная область между вторичной камерой сгорания и турбиной низкого давления газовой турбины Download PDF

Info

Publication number
RU2540350C2
RU2540350C2 RU2012152096/06A RU2012152096A RU2540350C2 RU 2540350 C2 RU2540350 C2 RU 2540350C2 RU 2012152096/06 A RU2012152096/06 A RU 2012152096/06A RU 2012152096 A RU2012152096 A RU 2012152096A RU 2540350 C2 RU2540350 C2 RU 2540350C2
Authority
RU
Russia
Prior art keywords
cavity
gas turbine
wall
width
radially
Prior art date
Application number
RU2012152096/06A
Other languages
English (en)
Russian (ru)
Other versions
RU2012152096A (ru
Inventor
Томас ХАЙНЦ-ШВАРЦМАЙЕР
Марк ВИДМЕР
Сельма ЗАХИРОВИЧ
Пол МАРЛОУ
Original Assignee
Альстом Текнолоджи Лтд.
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 Альстом Текнолоджи Лтд. filed Critical Альстом Текнолоджи Лтд.
Publication of RU2012152096A publication Critical patent/RU2012152096A/ru
Application granted granted Critical
Publication of RU2540350C2 publication Critical patent/RU2540350C2/ru

Links

Images

Classifications

    • 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
    • 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
    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • 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
    • 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
    • F02C6/003—Gas-turbine plants with heaters between turbine stages
    • 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
    • F05D2240/00—Components
    • F05D2240/10—Stators
    • F05D2240/12—Fluid guiding means, e.g. vanes
    • F05D2240/127—Vortex generators, turbulators, or the like, for mixing

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)
RU2012152096/06A 2010-05-05 2011-04-26 Переходная область между вторичной камерой сгорания и турбиной низкого давления газовой турбины RU2540350C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH00691/10 2010-05-05
CH00691/10A CH703105A1 (de) 2010-05-05 2010-05-05 Gasturbine mit einer sekundärbrennkammer.
PCT/EP2011/056582 WO2011138193A1 (de) 2010-05-05 2011-04-26 Übergangsbereich für eine sekundärbrennkammer einer gasturbine

Publications (2)

Publication Number Publication Date
RU2012152096A RU2012152096A (ru) 2014-06-10
RU2540350C2 true RU2540350C2 (ru) 2015-02-10

Family

ID=42340790

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2012152096/06A RU2540350C2 (ru) 2010-05-05 2011-04-26 Переходная область между вторичной камерой сгорания и турбиной низкого давления газовой турбины

Country Status (9)

Country Link
US (1) US9097119B2 (enExample)
EP (1) EP2567071A1 (enExample)
JP (1) JP5826253B2 (enExample)
KR (1) KR101645954B1 (enExample)
CN (1) CN102884282B (enExample)
CH (1) CH703105A1 (enExample)
MX (1) MX2012012797A (enExample)
RU (1) RU2540350C2 (enExample)
WO (1) WO2011138193A1 (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9243508B2 (en) * 2012-03-20 2016-01-26 General Electric Company System and method for recirculating a hot gas flowing through a gas turbine
JP5490191B2 (ja) * 2012-07-19 2014-05-14 三菱重工業株式会社 ガスタービン
US10443736B2 (en) 2015-10-01 2019-10-15 United Technologies Corporation Expansion seal
CN111441833B (zh) * 2020-04-22 2024-12-10 中国大唐集团科学技术研究院有限公司华东电力试验研究院 一种用于透平进口工质降温的导流装置

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5785492A (en) * 1997-03-24 1998-07-28 United Technologies Corporation Method and apparatus for sealing a gas turbine stator vane assembly
RU2133384C1 (ru) * 1995-11-22 1999-07-20 Открытое акционерное общество "Самарский научно-технический комплекс им.Н.Д.Кузнецова" Статор многоступенчатой турбомашины
US6276692B1 (en) * 1998-07-14 2001-08-21 Asea Brown Boveri Ag Non-contact sealing of gaps in gas turbines
US7178340B2 (en) * 2003-09-24 2007-02-20 Power Systems Mfg., Llc Transition duct honeycomb seal
US7527469B2 (en) * 2004-12-10 2009-05-05 Siemens Energy, Inc. Transition-to-turbine seal apparatus and kit for transition/turbine junction of a gas turbine engine

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3224194A (en) * 1963-06-26 1965-12-21 Curtiss Wright Corp Gas turbine engine
US3965066A (en) * 1974-03-15 1976-06-22 General Electric Company Combustor-turbine nozzle interconnection
JPS62176448U (enExample) 1986-04-30 1987-11-09
EP0902164B1 (de) 1997-09-15 2003-04-02 ALSTOM (Switzerland) Ltd Plattformkühlung für Gasturbinen
DE59709283D1 (de) * 1997-12-23 2003-03-13 Abb Turbo Systems Ag Baden Verfahren und Vorrichtung zum berührungsfreien Abdichten eines zwischen einem Rotor und einem Stator ausgebildeten Trennspalts
US6347508B1 (en) * 2000-03-22 2002-02-19 Allison Advanced Development Company Combustor liner support and seal assembly
US6345494B1 (en) * 2000-09-20 2002-02-12 Siemens Westinghouse Power Corporation Side seal for combustor transitions
JP3600912B2 (ja) * 2001-09-12 2004-12-15 川崎重工業株式会社 燃焼器ライナのシール構造
DE10336432A1 (de) 2003-08-08 2005-03-10 Alstom Technology Ltd Baden Gasturbine und zugehöriges Kühlverfahren
US7363763B2 (en) 2003-10-23 2008-04-29 United Technologies Corporation Combustor
EP1731714A1 (de) * 2005-06-08 2006-12-13 Siemens Aktiengesellschaft Spaltsperrvorrichtung und Verwendung einer solchen
EP1731711A1 (de) * 2005-06-10 2006-12-13 Siemens Aktiengesellschaft Übergang zwischen Brennkammer und Turbineneinheit, Hitzeschild und Turbinenleitschaufel für eine Gasturbine
US20070033945A1 (en) * 2005-08-10 2007-02-15 Goldmeer Jeffrey S Gas turbine system and method of operation
WO2007068538A1 (de) * 2005-12-14 2007-06-21 Alstom Technology Ltd Strömungsmaschine
DE102006015530A1 (de) * 2006-03-31 2007-10-04 Alstom Technology Ltd. Turbomaschine
US7797948B2 (en) * 2007-03-27 2010-09-21 Siemens Energy, Inc. Transition-to-turbine seal apparatus and transition-to-turbine seal junction of a gas turbine engine
DE502008002497D1 (de) 2007-08-06 2011-03-10 Alstom Technology Ltd Spaltkühlung zwischen brennkammerwand und turbinenwand einer gasturbinenanlage
EP2227522A1 (en) 2007-11-28 2010-09-15 Shell Internationale Research Maatschappij B.V. Gasoline compositions
EP2229507B1 (de) 2007-12-29 2017-02-08 General Electric Technology GmbH Gasturbine
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2133384C1 (ru) * 1995-11-22 1999-07-20 Открытое акционерное общество "Самарский научно-технический комплекс им.Н.Д.Кузнецова" Статор многоступенчатой турбомашины
US5785492A (en) * 1997-03-24 1998-07-28 United Technologies Corporation Method and apparatus for sealing a gas turbine stator vane assembly
US6276692B1 (en) * 1998-07-14 2001-08-21 Asea Brown Boveri Ag Non-contact sealing of gaps in gas turbines
US7178340B2 (en) * 2003-09-24 2007-02-20 Power Systems Mfg., Llc Transition duct honeycomb seal
US7527469B2 (en) * 2004-12-10 2009-05-05 Siemens Energy, Inc. Transition-to-turbine seal apparatus and kit for transition/turbine junction of a gas turbine engine

Also Published As

Publication number Publication date
CN102884282A (zh) 2013-01-16
MX2012012797A (es) 2013-01-17
US9097119B2 (en) 2015-08-04
WO2011138193A1 (de) 2011-11-10
KR20130094184A (ko) 2013-08-23
JP5826253B2 (ja) 2015-12-02
KR101645954B1 (ko) 2016-08-12
EP2567071A1 (de) 2013-03-13
US20130055717A1 (en) 2013-03-07
CH703105A1 (de) 2011-11-15
RU2012152096A (ru) 2014-06-10
JP2013528738A (ja) 2013-07-11
CN102884282B (zh) 2015-07-29

Similar Documents

Publication Publication Date Title
US8266914B2 (en) Heat shield sealing for gas turbine engine combustor
US10041675B2 (en) Multiple ventilated rails for sealing of combustor heat shields
US9909761B2 (en) Combustor wall assembly for a turbine engine
US10801415B2 (en) Heat shield labyrinth seal
CN105531545B (zh) 燃气轮机燃烧室的楔形陶瓷热屏
JP6366180B2 (ja) シール構造
US7201559B2 (en) Stationary ring assembly for a gas turbine
CN107916996B (zh) 用于燃气涡轮动力装置的定子热屏蔽件节段
US9097118B2 (en) Transitional region for a combustion chamber of a gas turbine
RU2540350C2 (ru) Переходная область между вторичной камерой сгорания и турбиной низкого давления газовой турбины
JP6512573B2 (ja) シール部材
US7011492B2 (en) Turbine vane cooled by a reduced cooling air leak
EP3623703B1 (en) Metallic heat-insulating tile for a combustion chamber of a gas turbine
KR101842746B1 (ko) 가스터빈의 트랜지션피스와 터빈의 연결장치
KR101574489B1 (ko) 시일 구조체
CN106437868B (zh) 燃气涡轮
WO2017029689A1 (ja) 軸流タービン

Legal Events

Date Code Title Description
PD4A Correction of name of patent owner
PC41 Official registration of the transfer of exclusive right

Effective date: 20170426