EP1446556B1
(de)
|
2001-10-30 |
2006-03-29 |
Alstom Technology Ltd |
Turbomaschine
|
DE10233113A1
(de)
*
|
2001-10-30 |
2003-05-15 |
Alstom Switzerland Ltd |
Turbomaschine
|
DE10305038A1
(de)
*
|
2003-02-07 |
2004-08-19 |
Pfeiffer Vacuum Gmbh |
Vakuumpumpanordnung
|
WO2004090291A1
(de)
*
|
2003-04-07 |
2004-10-21 |
Alstom Technology Ltd |
Turbomaschine
|
DE10352089A1
(de)
*
|
2003-11-07 |
2005-06-09 |
Alstom Technology Ltd |
Verfahren zum Betreiben einer Turbomaschine, und Turbomaschine
|
JP2006037855A
(ja)
*
|
2004-07-28 |
2006-02-09 |
Mitsubishi Heavy Ind Ltd |
車室ケーシング及びガスタービン
|
DE102004041271A1
(de)
*
|
2004-08-23 |
2006-03-02 |
Alstom Technology Ltd |
Einrichtung und Verfahren zum Kühlen eines Gehäuses einer Gasturbine bzw. einer Brennkammer
|
US20060162338A1
(en)
*
|
2005-01-21 |
2006-07-27 |
Pratt & Whitney Canada Corp. |
Evacuation of hot gases accumulated in an inactive gas turbine engine
|
US7987660B2
(en)
|
2005-06-10 |
2011-08-02 |
Mitsubishi Heavy Industries, Ltd. |
Gas turbine, method of controlling air supply and computer program product for controlling air supply
|
US8210802B2
(en)
*
|
2008-01-22 |
2012-07-03 |
General Electric Company |
Turbine casing
|
EP2112335A1
(de)
*
|
2008-04-21 |
2009-10-28 |
Siemens Aktiengesellschaft |
Dampfturbine mit Kühlvorrichtung
|
US8061971B2
(en)
*
|
2008-09-12 |
2011-11-22 |
General Electric Company |
Apparatus and method for cooling a turbine
|
US8047763B2
(en)
*
|
2008-10-30 |
2011-11-01 |
General Electric Company |
Asymmetrical gas turbine cooling port locations
|
US9151182B2
(en)
|
2011-04-22 |
2015-10-06 |
General Electric Company |
System and method for removing heat from a turbomachine
|
EP2565401A1
(de)
|
2011-09-05 |
2013-03-06 |
Siemens Aktiengesellschaft |
Verfahren zur Temperaturausgleichung in einer Dampfturbine
|
US9664062B2
(en)
*
|
2011-12-08 |
2017-05-30 |
Siemens Energy, Inc. |
Gas turbine engine with multiple component exhaust diffuser operating in conjunction with an outer case ambient external cooling system
|
US8894359B2
(en)
*
|
2011-12-08 |
2014-11-25 |
Siemens Aktiengesellschaft |
Gas turbine engine with outer case ambient external cooling system
|
US20130149107A1
(en)
*
|
2011-12-08 |
2013-06-13 |
Mrinal Munshi |
Gas turbine outer case active ambient cooling including air exhaust into a sub-ambient region of exhaust flow
|
US10094285B2
(en)
*
|
2011-12-08 |
2018-10-09 |
Siemens Aktiengesellschaft |
Gas turbine outer case active ambient cooling including air exhaust into sub-ambient cavity
|
US9719372B2
(en)
|
2012-05-01 |
2017-08-01 |
General Electric Company |
Gas turbomachine including a counter-flow cooling system and method
|
US8973372B2
(en)
*
|
2012-09-05 |
2015-03-10 |
Siemens Aktiengesellschaft |
Combustor shell air recirculation system in a gas turbine engine
|
US8820090B2
(en)
*
|
2012-09-05 |
2014-09-02 |
Siemens Aktiengesellschaft |
Method for operating a gas turbine engine including a combustor shell air recirculation system
|
US9091171B2
(en)
*
|
2012-10-30 |
2015-07-28 |
Siemens Aktiengesellschaft |
Temperature control within a cavity of a turbine engine
|
US8893510B2
(en)
|
2012-11-07 |
2014-11-25 |
Siemens Aktiengesellschaft |
Air injection system in a gas turbine engine
|
US8820091B2
(en)
|
2012-11-07 |
2014-09-02 |
Siemens Aktiengesellschaft |
External cooling fluid injection system in a gas turbine engine
|
US9494081B2
(en)
|
2013-05-09 |
2016-11-15 |
Siemens Aktiengesellschaft |
Turbine engine shutdown temperature control system with an elongated ejector
|
EP2818646A1
(de)
|
2013-06-28 |
2014-12-31 |
Siemens Aktiengesellschaft |
Gasturbine, umfassend ein Verdichtergehäuse mit einer Einlassöffnung für die Temperierung des Verdichtergehäuses und Verwendung der Gasturbine
|
EP2987966A1
(de)
|
2014-08-21 |
2016-02-24 |
Siemens Aktiengesellschaft |
Gasturbine mit in Ringsektoren unterteiltem Kühlringkanal
|
US9664070B1
(en)
|
2016-02-12 |
2017-05-30 |
United Technologies Corporation |
Bowed rotor prevention system
|
US10125691B2
(en)
|
2016-02-12 |
2018-11-13 |
United Technologies Corporation |
Bowed rotor start using a variable position starter valve
|
US10539079B2
(en)
|
2016-02-12 |
2020-01-21 |
United Technologies Corporation |
Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
|
US10443505B2
(en)
|
2016-02-12 |
2019-10-15 |
United Technologies Corporation |
Bowed rotor start mitigation in a gas turbine engine
|
US10174678B2
(en)
|
2016-02-12 |
2019-01-08 |
United Technologies Corporation |
Bowed rotor start using direct temperature measurement
|
US10508567B2
(en)
|
2016-02-12 |
2019-12-17 |
United Technologies Corporation |
Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory
|
US10040577B2
(en)
|
2016-02-12 |
2018-08-07 |
United Technologies Corporation |
Modified start sequence of a gas turbine engine
|
US10436064B2
(en)
|
2016-02-12 |
2019-10-08 |
United Technologies Corporation |
Bowed rotor start response damping system
|
US10443507B2
(en)
|
2016-02-12 |
2019-10-15 |
United Technologies Corporation |
Gas turbine engine bowed rotor avoidance system
|
US10125636B2
(en)
|
2016-02-12 |
2018-11-13 |
United Technologies Corporation |
Bowed rotor prevention system using waste heat
|
US10508601B2
(en)
|
2016-02-12 |
2019-12-17 |
United Technologies Corporation |
Auxiliary drive bowed rotor prevention system for a gas turbine engine
|
US10598047B2
(en)
|
2016-02-29 |
2020-03-24 |
United Technologies Corporation |
Low-power bowed rotor prevention system
|
PL232314B1
(pl)
|
2016-05-06 |
2019-06-28 |
Gen Electric |
Maszyna przepływowa zawierająca system regulacji luzu
|
US10309246B2
(en)
|
2016-06-07 |
2019-06-04 |
General Electric Company |
Passive clearance control system for gas turbomachine
|
US10787933B2
(en)
|
2016-06-20 |
2020-09-29 |
Raytheon Technologies Corporation |
Low-power bowed rotor prevention and monitoring system
|
US10358936B2
(en)
|
2016-07-05 |
2019-07-23 |
United Technologies Corporation |
Bowed rotor sensor system
|
US10605093B2
(en)
|
2016-07-12 |
2020-03-31 |
General Electric Company |
Heat transfer device and related turbine airfoil
|
US10392944B2
(en)
|
2016-07-12 |
2019-08-27 |
General Electric Company |
Turbomachine component having impingement heat transfer feature, related turbomachine and storage medium
|
US10384791B2
(en)
|
2016-07-21 |
2019-08-20 |
United Technologies Corporation |
Cross engine coordination during gas turbine engine motoring
|
US10221774B2
(en)
|
2016-07-21 |
2019-03-05 |
United Technologies Corporation |
Speed control during motoring of a gas turbine engine
|
EP3273016B1
(de)
|
2016-07-21 |
2020-04-01 |
United Technologies Corporation |
Koordination während des anlassens eines gasturbinenmotors
|
EP3273006B1
(de)
|
2016-07-21 |
2019-07-03 |
United Technologies Corporation |
Verwendung eines alternierenden anlassers während des anfahrens mit mehreren motoren
|
US10618666B2
(en)
|
2016-07-21 |
2020-04-14 |
United Technologies Corporation |
Pre-start motoring synchronization for multiple engines
|
US10787968B2
(en)
|
2016-09-30 |
2020-09-29 |
Raytheon Technologies Corporation |
Gas turbine engine motoring with starter air valve manual override
|
US10443543B2
(en)
|
2016-11-04 |
2019-10-15 |
United Technologies Corporation |
High compressor build clearance reduction
|
US10823079B2
(en)
|
2016-11-29 |
2020-11-03 |
Raytheon Technologies Corporation |
Metered orifice for motoring of a gas turbine engine
|
US10947993B2
(en)
*
|
2017-11-27 |
2021-03-16 |
General Electric Company |
Thermal gradient attenuation structure to mitigate rotor bow in turbine engine
|
CN109707470A
(zh)
*
|
2018-11-30 |
2019-05-03 |
东方电气集团东方汽轮机有限公司 |
一种小型双层筒形缸结构
|
GB2584712A
(en)
*
|
2019-06-13 |
2020-12-16 |
Rolls Royce Plc |
A forced air convection apparatus and method for cooling a turbomachine
|
US11879411B2
(en)
|
2022-04-07 |
2024-01-23 |
General Electric Company |
System and method for mitigating bowed rotor in a gas turbine engine
|
US12247517B2
(en)
|
2022-11-21 |
2025-03-11 |
Ge Infrastructure Technology Llc |
Systems and methods for model-based control of gas turbine system considering fluid injection
|