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
|
EP1141534B1
(en)
|
1999-01-04 |
2005-04-06 |
Allison Advanced Development Company |
Exhaust mixer and apparatus using same
|
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
|
CN106537043B
(zh)
*
|
2014-08-19 |
2021-09-24 |
三菱动力株式会社 |
燃气轮机
|
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
|