CN100394110C - 燃气轮机 - Google Patents

燃气轮机 Download PDF

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Publication number
CN100394110C
CN100394110C CNB038215306A CN03821530A CN100394110C CN 100394110 C CN100394110 C CN 100394110C CN B038215306 A CNB038215306 A CN B038215306A CN 03821530 A CN03821530 A CN 03821530A CN 100394110 C CN100394110 C CN 100394110C
Authority
CN
China
Prior art keywords
combustion chamber
coolant
gas turbine
coolant hose
chamber
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
CNB038215306A
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English (en)
Chinese (zh)
Other versions
CN1682078A (zh
Inventor
威廉·舒尔滕
保罗-海因茨·杰佩尔
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.)
Siemens Corp
Original Assignee
Siemens Corp
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 Siemens Corp filed Critical Siemens Corp
Publication of CN1682078A publication Critical patent/CN1682078A/zh
Application granted granted Critical
Publication of CN100394110C publication Critical patent/CN100394110C/zh
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00012—Details of sealing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CNB038215306A 2002-09-13 2003-09-01 燃气轮机 Expired - Fee Related CN100394110C (zh)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP02020694A EP1398569A1 (fr) 2002-09-13 2002-09-13 Turbine à gaz
EP02020694.2 2002-09-13

Publications (2)

Publication Number Publication Date
CN1682078A CN1682078A (zh) 2005-10-12
CN100394110C true CN100394110C (zh) 2008-06-11

Family

ID=31725437

Family Applications (1)

Application Number Title Priority Date Filing Date
CNB038215306A Expired - Fee Related CN100394110C (zh) 2002-09-13 2003-09-01 燃气轮机

Country Status (5)

Country Link
US (1) US20050247062A1 (fr)
EP (2) EP1398569A1 (fr)
JP (1) JP4181546B2 (fr)
CN (1) CN100394110C (fr)
WO (1) WO2004031656A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8695989B2 (en) * 2004-04-30 2014-04-15 Siemens Aktiengesellschaft Hot gas seal
GB2434199B (en) * 2006-01-14 2011-01-05 Alstom Technology Ltd Combustor liner with heat shield
EP1862740B1 (fr) * 2006-05-31 2015-09-16 Siemens Aktiengesellschaft Paroi de chambre de combustion
US8397512B2 (en) * 2008-08-25 2013-03-19 General Electric Company Flow device for turbine engine and method of assembling same
EP2405200A1 (fr) * 2010-07-05 2012-01-11 Siemens Aktiengesellschaft Appareil de combustion et moteur de turbine à gaz
US9534783B2 (en) * 2011-07-21 2017-01-03 United Technologies Corporation Insert adjacent to a heat shield element for a gas turbine engine combustor
DE102011083814A1 (de) 2011-09-30 2013-04-04 Mtu Aero Engines Gmbh Segmentiertes Bauteil
US10422532B2 (en) 2013-08-01 2019-09-24 United Technologies Corporation Attachment scheme for a ceramic bulkhead panel
CN104454174A (zh) * 2014-10-13 2015-03-25 罗显平 一种提高燃气发动机动力输出功率的方法

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB376974A (en) * 1930-09-02 1932-07-21 Bbc Brown Boveri & Cie Improvements in and relating to combustion chambers
DE1025915B (de) * 1953-07-03 1958-03-13 Still Fa Carl Gasbeheizter Roehrenerhitzer mit einem aus Rohren gebildeten selbsttragenden Feuerraum
US5129447A (en) * 1991-05-20 1992-07-14 United Technologies Corporation Cooled bolting arrangement
DE4343332A1 (de) * 1993-12-20 1995-06-22 Abb Management Ag Vorrichtung zur Konvektivkühlung einer dichten Brennkammer
US5832718A (en) * 1995-12-19 1998-11-10 Daimler-Benz Aerospace Airbus Gmbh Combustion chamber especially for a gas turbine engine using hydrogen as fuel

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US1935659A (en) * 1930-09-01 1933-11-21 Bbc Brown Boveri & Cie Pressureproof combustion chamber
FR980028A (fr) * 1942-06-18 1951-05-07 Regent Perfectionnements apportés aux chambres de combustion
US3190070A (en) * 1950-04-05 1965-06-22 Thiokol Chemical Corp Reaction motor construction
US3043103A (en) * 1958-10-10 1962-07-10 Gen Motors Corp Liquid cooled wall
US3066702A (en) * 1959-05-28 1962-12-04 United Aircraft Corp Cooled nozzle structure
US3031844A (en) * 1960-08-12 1962-05-01 William A Tomolonius Split combustion liner
US3177935A (en) * 1963-12-17 1965-04-13 Irwin E Rosman Cooling tube structure
US3398527A (en) * 1966-05-31 1968-08-27 Air Force Usa Corrugated wall radiation cooled combustion chamber
DE2015024B2 (de) * 1970-03-28 1971-10-14 Messerschmitt Bolkow Blohm GmbH, 8000 München Verfahren zur herstellung von regenerativ gekuehlten brenn kammern und oder schubduesen
US4288980A (en) * 1979-06-20 1981-09-15 Brown Boveri Turbomachinery, Inc. Combustor for use with gas turbines
US4765145A (en) * 1987-01-20 1988-08-23 Rockwell International Corporation Connector assembly
US5024058A (en) * 1989-12-08 1991-06-18 Sundstrand Corporation Hot gas generator
US5636508A (en) * 1994-10-07 1997-06-10 Solar Turbines Incorporated Wedge edge ceramic combustor tile
JPH08270950A (ja) * 1995-02-01 1996-10-18 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
US5832719A (en) * 1995-12-18 1998-11-10 United Technologies Corporation Rocket thrust chamber
DE19751299C2 (de) * 1997-11-19 1999-09-09 Siemens Ag Brennkammer sowie Verfahren zur Dampfkühlung einer Brennkammer
DE19804232C2 (de) * 1998-02-04 2000-06-29 Daimler Chrysler Ag Brennkammer für Hochleistungstriebwerke und Düsen
WO2000032920A1 (fr) * 1998-11-27 2000-06-08 Volvo Aero Corporation Structure tuyere pour cols de tuyeres avec paroi refroidie
DE19915082C1 (de) * 1999-04-01 2000-07-13 Daimler Chrysler Ag Verfahren zur Herstellung einer gekühlten Düse für ein Raketentriebwerk
DE60212568T2 (de) * 2001-01-11 2007-06-14 Volvo Aero Corp. Raketentriebwerksglied und verfahren zur herstellung eines raketentriebwerksglied
US20020157400A1 (en) * 2001-04-27 2002-10-31 Siemens Aktiengesellschaft Gas turbine with combined can-type and annular combustor and method of operating a gas turbine
RU2289035C2 (ru) * 2001-12-18 2006-12-10 Вольво Аэро Корпорейшн Подверженный во время работы воздействию высоких тепловых нагрузок элемент конструкции и способ его изготовления
EP1511930B1 (fr) * 2002-05-28 2007-04-25 Volvo Aero Corporation Structure de paroi
EP1389714A1 (fr) * 2002-08-16 2004-02-18 Siemens Aktiengesellschaft Chambre à combustion de turbine à gaz
ES2307834T3 (es) * 2003-01-29 2008-12-01 Siemens Aktiengesellschaft Camara de combustion.
US6931855B2 (en) * 2003-05-12 2005-08-23 Siemens Westinghouse Power Corporation Attachment system for coupling combustor liners to a carrier of a turbine combustor
EP1482246A1 (fr) * 2003-05-30 2004-12-01 Siemens Aktiengesellschaft Chambre de combustion
US7213392B2 (en) * 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
US7146815B2 (en) * 2003-07-31 2006-12-12 United Technologies Corporation Combustor
US7043921B2 (en) * 2003-08-26 2006-05-16 Honeywell International, Inc. Tube cooled combustor
US7370469B2 (en) * 2004-12-13 2008-05-13 United Technologies Corporation Rocket chamber heat exchanger
US7721547B2 (en) * 2005-06-27 2010-05-25 Siemens Energy, Inc. Combustion transition duct providing stage 1 tangential turning for turbine engines

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB376974A (en) * 1930-09-02 1932-07-21 Bbc Brown Boveri & Cie Improvements in and relating to combustion chambers
DE1025915B (de) * 1953-07-03 1958-03-13 Still Fa Carl Gasbeheizter Roehrenerhitzer mit einem aus Rohren gebildeten selbsttragenden Feuerraum
US5129447A (en) * 1991-05-20 1992-07-14 United Technologies Corporation Cooled bolting arrangement
DE4343332A1 (de) * 1993-12-20 1995-06-22 Abb Management Ag Vorrichtung zur Konvektivkühlung einer dichten Brennkammer
US5832718A (en) * 1995-12-19 1998-11-10 Daimler-Benz Aerospace Airbus Gmbh Combustion chamber especially for a gas turbine engine using hydrogen as fuel

Also Published As

Publication number Publication date
EP1537363A1 (fr) 2005-06-08
EP1398569A1 (fr) 2004-03-17
US20050247062A1 (en) 2005-11-10
CN1682078A (zh) 2005-10-12
WO2004031656A1 (fr) 2004-04-15
JP4181546B2 (ja) 2008-11-19
JP2005538310A (ja) 2005-12-15

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20080611

Termination date: 20091009