Patent | Date |
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Gas turbine engine with angled and radial supports Grant 8,770,924 - Beeck , et al. July 8, 2 | 2014-07-08 |
Gas turbine sealing apparatus Grant 8,376,697 - Wiebe , et al. February 19, 2 | 2013-02-19 |
Gas Turbine Engine With Angled And Radial Supports App 20130011242 - Beeck; Alexander ;   et al. | 2013-01-10 |
Gas Turbine Sealing Apparatus App 20100074731 - Wiebe; David J. ;   et al. | 2010-03-25 |
Sealing arrangement Grant 6,916,021 - Beeck , et al. July 12, 2 | 2005-07-12 |
Gap seal for sealing a gap between two adjacent components Grant 6,857,639 - Beeck , et al. February 22, 2 | 2005-02-22 |
Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint Grant 6,739,594 - Beeck , et al. May 25, 2 | 2004-05-25 |
Process for the rapid production of hollow components of flow machines for manufacturing development Grant 6,705,383 - Beeck , et al. March 16, 2 | 2004-03-16 |
Gap seal for sealing a gap between two adjacent components App 20040041350 - Beeck, Alexander ;   et al. | 2004-03-04 |
Gap seal for sealing a gap between two adjacent components App 20040041351 - Beeck, Alexander ;   et al. | 2004-03-04 |
Method for producing a cast part, model mold, and ceramic insert for use in this method Grant 6,695,036 - Brandl , et al. February 24, 2 | 2004-02-24 |
Cooled gas turbine blade Grant 6,682,304 - Beeck , et al. January 27, 2 | 2004-01-27 |
Sealing arrangement App 20040012151 - Beeck, Alexander ;   et al. | 2004-01-22 |
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 |
Device and method for cooling a platform of a turbine blade Grant 6,641,360 - Beeck , et al. November 4, 2 | 2003-11-04 |
Method for reducing variance in the coolant consumption of components of a turbo-machine Grant 6,640,597 - Beeck , et al. November 4, 2 | 2003-11-04 |
Nondestructive Method For Determining The Thickness Of A Metallic Protective Layer On A Metallic Base Material Via A Different Type Of Layer Between The Metallic Protective Layer And The Metallic Base Material Grant 6,534,975 - Beeck , et al. March 18, 2 | 2003-03-18 |
Hollow-cast component Grant 6,516,865 - Beeck , et al. February 11, 2 | 2003-02-11 |
Friction-susceptible component of a thermal turbo machine Grant 6,499,943 - Beeck , et al. December 31, 2 | 2002-12-31 |
Turbo machine Grant 6,499,944 - Beeck , et al. December 31, 2 | 2002-12-31 |
Blade for gas turbines with choke cross section at the trailing edge Grant 6,481,966 - Beeck , et al. November 19, 2 | 2002-11-19 |
Device for cooling a shroud of a gas turbine blade App 20020136635 - Beeck, Alexander ;   et al. | 2002-09-26 |
Process for nonlinear processing and identification of information App 20020138482 - Beeck, Alexander ;   et al. | 2002-09-26 |
Method for producing a cast part, model mold, and ceramic insert for use in this method App 20020129924 - Brandl, Herbert ;   et al. | 2002-09-19 |
Cooled gas turbine blade App 20020127103 - Beeck, Alexander ;   et al. | 2002-09-12 |
Method for reducing variance in the coolant consumption of components of a turbo-machine App 20020124615 - Beeck, Alexander ;   et al. | 2002-09-12 |
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 |
Process for the rapid production of hollow components of flow machines for manufacturing development App 20020108734 - Beeck, Alexander ;   et al. | 2002-08-15 |
Device and method for cooling a platform of a turbine blade App 20020098078 - Beeck, Alexander ;   et al. | 2002-07-25 |
Tool and process for casting a shaped part for the production of a turbine blade App 20020088600 - Beeck, Alexander ;   et al. | 2002-07-11 |
Component of a flow machine, with inspection aperture App 20020090298 - Beeck, Alexander ;   et al. | 2002-07-11 |
Rotor for a gas turbine Grant 6,416,282 - Beeck , et al. July 9, 2 | 2002-07-09 |
Process for producing a thermally loaded casting Grant 6,412,541 - Roesler , et al. July 2, 2 | 2002-07-02 |
Sealing arrangement between components of a rotating assembly as well as a method for producing a sealing joint App 20020061250 - Beeck, Alexander ;   et al. | 2002-05-23 |
Sealing of a thermal turbomachine App 20020015641 - Beeck, Alexander ;   et al. | 2002-02-07 |
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 |
Process for producing a thermally loaded casting App 20010042607 - Roesler, Hans-Joachim ;   et al. | 2001-11-22 |
Sealing arrangement Grant 6,312,218 - Beeck , et al. November 6, 2 | 2001-11-06 |
Platelike projecting component portion of a gas turbine App 20010036407 - Beeck, Alexander ;   et al. | 2001-11-01 |
Method and device for cooling guide vanes in a gas turbine plant Grant 6,308,511 - Beeck , et al. October 30, 2 | 2001-10-30 |
Blade for gas turbines with choke cross section at the trailing edge App 20010012484 - Beeck, Alexander ;   et al. | 2001-08-09 |
Nondestructive method for determining the thickness of a metallic protective layer on a metallic base material App 20010009368 - Beeck, Alexander ;   et al. | 2001-07-26 |
Process of plugging cooling holes of a gas turbine component Grant 6,265,022 - Fernihough , et al. July 24, 2 | 2001-07-24 |
Turbine blade Grant 6,241,469 - Beeck , et al. June 5, 2 | 2001-06-05 |
Cooling-air bore Grant 6,183,199 - Beeck , et al. February 6, 2 | 2001-02-06 |
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 |
Brush gasket Grant 6,012,723 - Beeck January 11, 2 | 2000-01-11 |
Thermally loaded blade for a turbomachine Grant 5,827,045 - Beeck October 27, 1 | 1998-10-27 |
Method and apparatus for shaft sealing and for cooling on the exhaust-gas side of an axial-flow gas turbine Grant 5,564,896 - Beeck , et al. October 15, 1 | 1996-10-15 |
Mixing chamber with vortex generators for flowing gases Grant 5,518,311 - Althaus , et al. May 21, 1 | 1996-05-21 |
Combustion chamber Grant 5,513,982 - Althaus , et al. May 7, 1 | 1996-05-07 |