P

Inventor

AUXIER THOMAS A

US31 patents
⚠️ This page may combine multiple inventors who share the name “AUXIER THOMAS A”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

UNITED TECHNOLOGIES CORP

28 patents
US5419039AMay 30, 1995

Method of making an air cooled vane with film cooling pocket construction

UNITED TECHNOLOGIES CORP144 citations98
US5392515AFeb 28, 1995

Method of manufacturing an air cooled vane with film cooling pocket construction

UNITED TECHNOLOGIES CORP148 citations98
US6247896B1Jun 19, 2001

Method and apparatus for cooling an airfoil

UNITED TECHNOLOGIES CORP102 citations96
US5720431AFeb 24, 1998

Cooled blades for a gas turbine engine

UNITED TECHNOLOGIES CORP172 citations96
US5486093AJan 23, 1996

Leading edge cooling of turbine airfoils

UNITED TECHNOLOGIES CORP91 citations96
US5405242AApr 11, 1995

Cooled vane

UNITED TECHNOLOGIES CORP103 citations96
US5403158AApr 4, 1995

Aerodynamic tip sealing for rotor blades

UNITED TECHNOLOGIES CORP64 citations96
US5246341ASep 21, 1993

Turbine blade trailing edge cooling construction

UNITED TECHNOLOGIES CORP74 citations96
US4820122AApr 11, 1989

Dirt removal means for air cooled blades

UNITED TECHNOLOGIES CORP85 citations96
US4753575AJun 28, 1988

Airfoil with nested cooling channels

UNITED TECHNOLOGIES CORP147 citations96
US4676719AJun 30, 1987

Film coolant passages for cast hollow airfoils

UNITED TECHNOLOGIES CORP76 citations96
US6164912ADec 26, 2000

Hollow airfoil for a gas turbine engine

UNITED TECHNOLOGIES CORP100 citations95
US6050777AApr 18, 2000

Apparatus and method for cooling an airfoil for a gas turbine engine

UNITED TECHNOLOGIES CORP55 citations95
US5700131ADec 23, 1997

Cooled blades for a gas turbine engine

UNITED TECHNOLOGIES CORP91 citations95
US5375973ADec 27, 1994

Turbine blade outer air seal with optimized cooling

UNITED TECHNOLOGIES CORP126 citations95
US5374161ADec 20, 1994

Blade outer air seal cooling enhanced with inter-segment film slot

UNITED TECHNOLOGIES CORP95 citations95
US5271715ADec 21, 1993

Cooled turbine blade

UNITED TECHNOLOGIES CORP64 citations95
US4767268AAug 30, 1988

Triple pass cooled airfoil

UNITED TECHNOLOGIES CORP83 citations95
US6280140B1Aug 28, 2001

Method and apparatus for cooling an airfoil

UNITED TECHNOLOGIES CORP60 citations94
US5129231AJul 14, 1992

Cooled combustor dome heatshield

UNITED TECHNOLOGIES CORP163 citations94
US4773593ASep 27, 1988

Coolable thin metal sheet

UNITED TECHNOLOGIES CORP61 citations94
US4887663ADec 19, 1989

Hot gas duct liner

UNITED TECHNOLOGIES CORP54 citations93
US4770608ASep 13, 1988

Film cooled vanes and turbines

UNITED TECHNOLOGIES CORP95 citations93
US6210112B1Apr 3, 2001

Apparatus for cooling an airfoil for a gas turbine engine

UNITED TECHNOLOGIES CORP41 citations92
US5899058AMay 4, 1999

Bypass air valve for a gas turbine engine

UNITED TECHNOLOGIES CORP34 citations92
US5674050AOct 7, 1997

Turbine blade

UNITED TECHNOLOGIES CORP22 citations92
US4664597AMay 12, 1987

Coolant passages with full coverage film cooling slot

UNITED TECHNOLOGIES CORP101 citations91
US6129515AOct 10, 2000

Turbine airfoil suction aided film cooling means

UNITED TECHNOLOGIES CORP37 citations87

GEN ELECTRIC

1 patent

US OF AMERICAS AS REPRESENTED

1 patent

US AIR FORCE

1 patent