Patents/Inventors

James T. Roach

Vernon, CTUS31 patents

22 Patents

US126006792026
Method to Tie Composite Vane Platform and Airfoil Design Details
RTX Corporation
0 cites
US125650332026
Ceramic Matrix Composite Sandwich Structure Reinforced with Z-tows
RTX Corporation
0 cites
US124350082025
Auxetic Materials and Structures for Ceramic Matrix Composite Airfoil Mandrels
RTX Corporation
0 cites
US124356402025
Gas Turbine Engine Vane Outer Diameter Platform Integrated with Blade Outer Air Seal
RTX Corporation
0 cites
US124289652025
Load Bearing Feature for Ceramic Matrix Composite Turbine Components
RTX Corporation
0 cites
US123922472025
Airfoil with Sandwich Composite Flange
RTX CORPORATION
0 cites
US123854022025
CMC Airfoil with Cooling Passage Formed in Fiber Plies
RTX CORPORATION
0 cites
US123656332025
Method to Tie Composite Vane Platform and Airfoil Design Details
RTX Corporation
0 cites
US123260932025
Gas Turbine Engine Vane and Spar Combination with Variable Air Flow Path
RTX Corporation
0 cites
US123055302025
Airfoil with Venturi Tube
RTX CORPORATION
0 cites
US122921932025
Combustor Liner with Pattern of Voids in CMC Fiber Ply for Cooling Channels
RTX CORPORATION
0 cites
US121960952025
Gas Turbine Engine Component Having an Airfoil with Internal Cross-ribs
RTX Corporation
0 cites
US120849822024
Flange and Assembly for Gas Turbine Engine Case
RTX Corporation
0 cites
US120780812024
Airfoil with CMC Ply Cutouts for Cooling Channels
RTX CORPORATION
0 cites
US120550682024
Airfoil Leading Edge Venturi Cooling Passage
RTX CORPORATION
0 cites
US120441322024
Seal Arc Segment with CMC Ply Cutouts for Cooling Channels
RTX CORPORATION
0 cites
US120068422024
Airfoil with Sandwich Composite
RTX CORPORATION
0 cites
US119133482024
Gas Turbine Engine Vane and Spar Combination with Variable Air Flow Path
RTX Corporation
0 cites
US119058472024
Airfoil with Venturi Tube
RTX CORPORATION
0 cites
US119058512024
CMC Trailing Edge 3D Weaved Cross Brace
RTX Corporation
0 cites
US118793512024
Composite Component with Damper for Gas Turbine Engine
RTX CORPORATION
0 cites
US117884192023
Airfoil Leading Edge Venturi Cooling Passage
RTX CORPORATION
0 cites