Patent | Date |
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Device for separating foreign particles out of the cooling air that can be fed to the rotor blades of a turbine Grant 7,137,777 - Fried , et al. November 21, 2 | 2006-11-21 |
Cooled components with conical cooling passages Grant 6,923,247 - Ferber , et al. August 2, 2 | 2005-08-02 |
Device for separating foreign particles out of the cooling air that can be fed to the rotor blades of a turbine App 20050002778 - Fried, Reinhard ;   et al. | 2005-01-06 |
Arrangement for cooling a flow-passage wall surrounding a flow passage, having at least one rib feature Grant 6,666,262 - Parneix , et al. December 23, 2 | 2003-12-23 |
Method for providing a curved cooling channel in a gas turbine component as well as coolable blade for a gas turbine component Grant 6,644,920 - Beeck , et al. November 11, 2 | 2003-11-11 |
Apparatus and process for impingement cooling of a component exposed to heat in a flow power machine Grant 6,634,859 - Weigand , et al. October 21, 2 | 2003-10-21 |
Apparatus and process for impingement cooling of a component exposed to heat in a flow power machine App 20020168264 - Weigand, Bernhard ;   et al. | 2002-11-14 |
Method for providing a curved cooling channel in a gas turbine component as well as coolable blade for a gas turbine component App 20020127104 - Beeck, Alexander ;   et al. | 2002-09-12 |
Method for visualizing and processing process runs, and a computer program for simulating the same App 20020046009 - Devaquet, Georges ;   et al. | 2002-04-18 |
Coolable blade for a gas turbine Grant 6,347,923 - Semmler , et al. February 19, 2 | 2002-02-19 |
Turbine blade with actively cooled shroud-band element Grant 6,340,284 - Beeck , et al. January 22, 2 | 2002-01-22 |
Arrangement for cooling a flow-passage wall surrounding a flow passage, having at least one rib element App 20020005274 - Beeck, Alexander ;   et al. | 2002-01-17 |
Sealing arrangement Grant 6,312,218 - Beeck , et al. November 6, 2 | 2001-11-06 |
Drilled cooling air openings in gas turbine components App 20010014282 - Haehnle, Hartmut ;   et al. | 2001-08-16 |
Arrangement of holes for forming a cooling film Grant 6,267,552 - Weigand July 31, 2 | 2001-07-31 |
Cooling arrangement for gas-turbine components Grant 6,261,053 - Anderson , et al. July 17, 2 | 2001-07-17 |
Turbine blade with actively cooled shroud-band element App 20010006600 - El-Nashar, Ibrahim ;   et al. | 2001-07-05 |
Turbomachine with cooled rotor shaft Grant 6,224,328 - Weigand , et al. May 1, 2 | 2001-05-01 |
Cooling system for the leading-edge region of a hollow gas-turbine blade Grant 6,168,380 - Weigand January 2, 2 | 2001-01-02 |
Cooling system for the leading-edge region of a hollow gas-turbine blade Grant 6,068,445 - Beeck , et al. May 30, 2 | 2000-05-30 |
Coolable blade Grant 5,919,031 - Hall , et al. July 6, 1 | 1999-07-06 |