NL7105761A - - Google Patents

Info

Publication number
NL7105761A
NL7105761A NL7105761A NL7105761A NL7105761A NL 7105761 A NL7105761 A NL 7105761A NL 7105761 A NL7105761 A NL 7105761A NL 7105761 A NL7105761 A NL 7105761A NL 7105761 A NL7105761 A NL 7105761A
Authority
NL
Netherlands
Application number
NL7105761A
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 filed Critical
Publication of NL7105761A publication Critical patent/NL7105761A/xx

Links

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
    • 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
    • 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
NL7105761A 1970-04-29 1971-04-28 NL7105761A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US3292670A 1970-04-29 1970-04-29

Publications (1)

Publication Number Publication Date
NL7105761A true NL7105761A (fr) 1971-11-02

Family

ID=21867610

Family Applications (1)

Application Number Title Priority Date Filing Date
NL7105761A NL7105761A (fr) 1970-04-29 1971-04-28

Country Status (7)

Country Link
US (1) US3609968A (fr)
BE (1) BE766326A (fr)
CA (1) CA929464A (fr)
DE (1) DE2119113A1 (fr)
FR (1) FR2086462B1 (fr)
GB (1) GB1299684A (fr)
NL (1) NL7105761A (fr)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US4016718A (en) * 1975-07-21 1977-04-12 United Technologies Corporation Gas turbine engine having an improved transition duct support
JPS53104020A (en) * 1977-02-23 1978-09-09 Hitachi Ltd Gas turbine combustor
US4251986A (en) * 1978-12-05 1981-02-24 General Electric Company Seal vibration-reducing apparatus
US4422288A (en) * 1981-03-02 1983-12-27 General Electric Company Aft mounting system for combustion transition duct members
IT1216611B (it) * 1988-04-21 1990-03-08 Nuovo Pignone Spa Dispositivo per mantenere la bocca anulare di uscita del convogliatore dei gas sempre centrata rispetto al gruppo ugelli di una turbina agas.
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly
US5414999A (en) * 1993-11-05 1995-05-16 General Electric Company Integral aft frame mount for a gas turbine combustor transition piece
US5412939A (en) * 1993-12-20 1995-05-09 Alliedsignal Inc. Seal compression tool for gas turbine engine
WO2000040851A1 (fr) * 1999-01-04 2000-07-13 Allison Advanced Development Company Melangeur des gaz d'echappement et appareil l'utilisant
US7096668B2 (en) * 2003-12-22 2006-08-29 Martling Vincent C Cooling and sealing design for a gas turbine combustion system
US7721547B2 (en) * 2005-06-27 2010-05-25 Siemens Energy, Inc. Combustion transition duct providing stage 1 tangential turning for turbine engines
US7762766B2 (en) * 2006-07-06 2010-07-27 Siemens Energy, Inc. Cantilevered framework support for turbine vane
US8240045B2 (en) * 2007-05-22 2012-08-14 Siemens Energy, Inc. Gas turbine transition duct coupling apparatus
US8616007B2 (en) * 2009-01-22 2013-12-31 Siemens Energy, Inc. Structural attachment system for transition duct outlet
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
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
US10436445B2 (en) * 2013-03-18 2019-10-08 General Electric Company Assembly for controlling clearance between a liner and stationary nozzle within a gas turbine
US9470422B2 (en) 2013-10-22 2016-10-18 Siemens Energy, Inc. Gas turbine structural mounting arrangement between combustion gas duct annular chamber and turbine vane carrier
DE112015003797B4 (de) * 2014-08-19 2022-08-18 Mitsubishi Heavy Industries, Ltd. Gasturbine
CN104373965B (zh) * 2014-10-28 2016-08-03 北京华清燃气轮机与煤气化联合循环工程技术有限公司 过渡段后密封结构
US9810434B2 (en) * 2016-01-21 2017-11-07 Siemens Energy, Inc. Transition duct system with arcuate ceramic liner for delivering hot-temperature gases in a combustion turbine engine
US11098652B2 (en) * 2019-05-29 2021-08-24 Raytheon Technologies Corporation Isolation seals for gas turbine engines

Also Published As

Publication number Publication date
CA929464A (en) 1973-07-03
FR2086462A1 (fr) 1971-12-31
US3609968A (en) 1971-10-05
DE2119113A1 (de) 1971-11-11
FR2086462B1 (fr) 1974-06-21
BE766326A (fr) 1971-10-27
GB1299684A (en) 1972-12-13

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