EP1312865A1
(de)
*
|
2001-11-15 |
2003-05-21 |
Siemens Aktiengesellschaft |
Ringbrennkammer für eine Gasturbine
|
US6725667B2
(en)
*
|
2002-08-22 |
2004-04-27 |
General Electric Company |
Combustor dome for gas turbine engine
|
US6779268B1
(en)
*
|
2003-05-13 |
2004-08-24 |
General Electric Company |
Outer and inner cowl-wire wrap to one piece cowl conversion
|
FR2867507B1
(fr)
*
|
2004-03-15 |
2006-06-23 |
Snecma Moteurs |
Pontet de positionnement et son utilisation au canal support de tuyere d'un turbopropulseur
|
US8015818B2
(en)
*
|
2005-02-22 |
2011-09-13 |
Siemens Energy, Inc. |
Cooled transition duct for a gas turbine engine
|
US7976274B2
(en)
*
|
2005-12-08 |
2011-07-12 |
General Electric Company |
Methods and apparatus for assembling turbine engines
|
DE102005060704A1
(de)
*
|
2005-12-19 |
2007-06-28 |
Rolls-Royce Deutschland Ltd & Co Kg |
Gasturbinenbrennkammer
|
US7908867B2
(en)
*
|
2007-09-14 |
2011-03-22 |
Siemens Energy, Inc. |
Wavy CMC wall hybrid ceramic apparatus
|
US8202588B2
(en)
*
|
2008-04-08 |
2012-06-19 |
Siemens Energy, Inc. |
Hybrid ceramic structure with internal cooling arrangements
|
US8327648B2
(en)
*
|
2008-12-09 |
2012-12-11 |
Pratt & Whitney Canada Corp. |
Combustor liner with integrated anti-rotation and removal feature
|
US8904799B2
(en)
*
|
2009-05-25 |
2014-12-09 |
Majed Toqan |
Tangential combustor with vaneless turbine for use on gas turbine engines
|
US8327644B2
(en)
*
|
2009-11-06 |
2012-12-11 |
Jhrg Inc. |
Micro-turbine combustor
|
US8707708B2
(en)
*
|
2010-02-22 |
2014-04-29 |
United Technologies Corporation |
3D non-axisymmetric combustor liner
|
RU2530685C2
(ru)
*
|
2010-03-25 |
2014-10-10 |
Дженерал Электрик Компани |
Структуры ударного воздействия для систем охлаждения
|
US20120208141A1
(en)
*
|
2011-02-14 |
2012-08-16 |
General Electric Company |
Combustor
|
JP6134732B2
(ja)
*
|
2011-12-05 |
2017-05-24 |
ゼネラル・エレクトリック・カンパニイ |
マルチゾーン燃焼器
|
US8960525B2
(en)
*
|
2013-01-31 |
2015-02-24 |
General Electric Company |
Brazing process and plate assembly
|
WO2014123850A1
(en)
|
2013-02-06 |
2014-08-14 |
United Technologies Corporation |
Gas turbine engine component with upstream-directed cooling film holes
|
US10174949B2
(en)
|
2013-02-08 |
2019-01-08 |
United Technologies Corporation |
Gas turbine engine combustor liner assembly with convergent hyperbolic profile
|
EP2971973B1
(en)
|
2013-03-14 |
2018-02-21 |
United Technologies Corporation |
Combustor panel and combustor with heat shield with increased durability
|
WO2015038293A1
(en)
|
2013-09-11 |
2015-03-19 |
United Technologies Corporation |
Combustor liner
|
EP3037728B1
(en)
*
|
2014-12-22 |
2020-04-29 |
Ansaldo Energia Switzerland AG |
Axially staged mixer with dilution air injection
|
CN104896514A
(zh)
*
|
2015-05-13 |
2015-09-09 |
广东电网有限责任公司电力科学研究院 |
燃气轮机主燃烧室防振隔热壁
|
CN105605605A
(zh)
*
|
2016-01-25 |
2016-05-25 |
西北工业大学 |
一种地面燃机燃烧室的防振冷却壁
|
US10495309B2
(en)
*
|
2016-02-12 |
2019-12-03 |
General Electric Company |
Surface contouring of a flowpath wall of a gas turbine engine
|
US10584880B2
(en)
|
2016-03-25 |
2020-03-10 |
General Electric Company |
Mounting of integrated combustor nozzles in a segmented annular combustion system
|
US10830442B2
(en)
|
2016-03-25 |
2020-11-10 |
General Electric Company |
Segmented annular combustion system with dual fuel capability
|
US10605459B2
(en)
|
2016-03-25 |
2020-03-31 |
General Electric Company |
Integrated combustor nozzle for a segmented annular combustion system
|
US10563869B2
(en)
|
2016-03-25 |
2020-02-18 |
General Electric Company |
Operation and turndown of a 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
|
US10641175B2
(en)
|
2016-03-25 |
2020-05-05 |
General Electric Company |
Panel fuel injector
|
US10641491B2
(en)
|
2016-03-25 |
2020-05-05 |
General Electric Company |
Cooling of integrated combustor nozzle of segmented annular combustion system
|
US11428413B2
(en)
|
2016-03-25 |
2022-08-30 |
General Electric Company |
Fuel injection module for 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
|
US10690350B2
(en)
|
2016-11-28 |
2020-06-23 |
General Electric Company |
Combustor with axially staged fuel injection
|
US11156362B2
(en)
|
2016-11-28 |
2021-10-26 |
General Electric Company |
Combustor with axially staged fuel injection
|
US10738646B2
(en)
|
2017-06-12 |
2020-08-11 |
Raytheon Technologies Corporation |
Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section
|
US10612555B2
(en)
|
2017-06-16 |
2020-04-07 |
United Technologies Corporation |
Geared turbofan with overspeed protection
|
US11371702B2
(en)
|
2020-08-31 |
2022-06-28 |
General Electric Company |
Impingement panel 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
|
US11614233B2
(en)
|
2020-08-31 |
2023-03-28 |
General Electric Company |
Impingement panel support structure and method of manufacture
|
US11460191B2
(en)
|
2020-08-31 |
2022-10-04 |
General Electric Company |
Cooling insert for a turbomachine
|
US11255545B1
(en)
|
2020-10-26 |
2022-02-22 |
General Electric Company |
Integrated combustion nozzle having a unified head end
|
US11898755B2
(en)
|
2022-06-08 |
2024-02-13 |
General Electric Company |
Combustor with a variable volume primary zone combustion chamber
|
US11835236B1
(en)
|
2022-07-05 |
2023-12-05 |
General Electric Company |
Combustor with reverse dilution air introduction
|
US11767766B1
(en)
|
2022-07-29 |
2023-09-26 |
General Electric Company |
Turbomachine airfoil having impingement cooling passages
|