loadpatents
Patent applications and USPTO patent grants for Auxier; Thomas A..The latest application filed is for "method and apparatus for cooling an airfoil".
Patent | Date |
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Method and apparatus for cooling an airfoil Grant 6,280,140 - Soechting , et al. August 28, 2 | 2001-08-28 |
Method and apparatus for cooling an airfoil Grant 6,247,896 - Auxier , et al. June 19, 2 | 2001-06-19 |
Apparatus for cooling an airfoil for a gas turbine engine Grant 6,210,112 - Tabbita , et al. April 3, 2 | 2001-04-03 |
Hollow airfoil for a gas turbine engine Grant 6,164,912 - Tabbita , et al. December 26, 2 | 2000-12-26 |
Turbine airfoil suction aided film cooling means Grant 6,129,515 - Soechting , et al. October 10, 2 | 2000-10-10 |
Apparatus and method for cooling an airfoil for a gas turbine engine Grant 6,050,777 - Tabbita , et al. April 18, 2 | 2000-04-18 |
Bypass air valve for a gas turbine engine Grant 5,899,058 - Narcus , et al. May 4, 1 | 1999-05-04 |
Cooled blades for a gas turbine engine Grant 5,720,431 - Sellers , et al. February 24, 1 | 1998-02-24 |
Cooled blades for a gas turbine engine Grant 5,700,131 - Hall , et al. December 23, 1 | 1997-12-23 |
Turbine blade Grant 5,674,050 - Hall , et al. October 7, 1 | 1997-10-07 |
Leading edge cooling of turbine airfoils Grant 5,486,093 - Auxier , et al. January 23, 1 | 1996-01-23 |
Method of making an air cooled vane with film cooling pocket construction Grant 5,419,039 - Auxier , et al. May 30, 1 | 1995-05-30 |
Cooled vane Grant 5,405,242 - Auxier , et al. * April 11, 1 | 1995-04-11 |
Method of manufacturing an air cooled vane with film cooling pocket construction Grant 5,392,515 - Auxier , et al. February 28, 1 | 1995-02-28 |
Turbine blade outer air seal with optimized cooling Grant 5,375,973 - Sloop , et al. December 27, 1 | 1994-12-27 |
Blade outer air seal cooling enhanced with inter-segment film slot Grant 5,374,161 - Kelch , et al. December 20, 1 | 1994-12-20 |
Cooled turbine blade Grant 5,271,715 - Zelesky , et al. December 21, 1 | 1993-12-21 |
Turbine blade trailing edge cooling construction Grant 5,246,341 - Hall , et al. September 21, 1 | 1993-09-21 |
Cooled combustor dome heatshield Grant 5,129,231 - Becker , et al. July 14, 1 | 1992-07-14 |
Hot gas duct liner Grant 4,887,663 - Auxier , et al. December 19, 1 | 1989-12-19 |
Dirt removal means for air cooled blades Grant 4,820,122 - Hall , et al. April 11, 1 | 1989-04-11 |
Coolable thin metal sheet Grant 4,773,593 - Auxier , et al. September 27, 1 | 1988-09-27 |
Film cooled vanes and turbines Grant 4,770,608 - Anderson , et al. September 13, 1 | 1988-09-13 |
Triple pass cooled airfoil Grant 4,767,268 - Auxier , et al. August 30, 1 | 1988-08-30 |
Airfoil with nested cooling channels Grant 4,753,575 - Levengood , et al. June 28, 1 | 1988-06-28 |
Film coolant passages for cast hollow airfoils Grant 4,676,719 - Auxier , et al. June 30, 1 | 1987-06-30 |
Coolant passages with full coverage film cooling slot Grant 4,664,597 - Auxier , et al. May 12, 1 | 1987-05-12 |
Turbine band cooling system Grant 4,187,054 - Landis, Jr. , et al. February 5, 1 | 1980-02-05 |
Turbine blade with increased film cooling Grant 3,891,348 - Auxier June 24, 1 | 1975-06-24 |
Cooled High Strength Turbine Bucket Grant 3,844,678 - Sterman , et al. October 29, 1 | 1974-10-29 |
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