Patents/Inventors

Jeffrey T. Morton

Manchester, CTUS23 patents

20 Patents

US125957652026
Bifurcation Integrated Electrical System for Hybrid Aircraft Propulsion System
RTX Corporation
0 cites
US125844442026
Suction Enabled Post Shutdown Combustor Cooling and Core Ventilation
RTX Corporation
0 cites
US125653282026
Differential Driven Open Rotor with Brake
RTX Corporation
0 cites
US125533922026
Gas Turbine Engine with Thermal Management
RTX Corporation
0 cites
US125032412025
Thermal Management Assembly for an Aircraft Propulsion System
RTX Corporation
0 cites
US124979052025
Non-uniform and Bi-tri Stator Spacing for Swirl Recovery Vane (SRV) Open Rotor Engines
RTX Corporation
0 cites
US124927112025
Open Rotor with Fixed Guide Vane/stator
RTX Corporation
0 cites
US124665442025
SRV Open Rotor with Core Inlet Forward of Rotor
RTX Corporation
0 cites
US124673842025
Translatable Guide Vanes for Aircraft Propulsion System
RTX CORPORATION
0 cites
US124605772025
AFT Gear Based Engine with Heat Recovery System
RTX CORPORATION
0 cites
US124608192025
Continuous Flow Fuel System
RTX Corporation
0 cites
US124489012025
Thermal Management System for Gas Turbine Engine with Open Propulsor
RTX Corporation
0 cites
US124218632025
Turbine Engine Tip Clearance Control System with Thrust Bearing
RTX CORPORATION
0 cites
US124048122025
Open Rotor Aircraft Propulsion System with Bypass Flowpath
RTX Corporation
0 cites
US123979242025
Open Rotor Aircraft Propulsion System with Bypass Flowpath
RTX CORPORATION
0 cites
US123521852025
Open Rotor Variable Pitch Blade with Retracting Inboard Trailing Edge
RTX Corporation
0 cites
US123522872025
Variable Guide Vane for Aircraft Propulsion System
RTX CORPORATION
0 cites
US122033852025
Telescoping Guide Vane for Aircraft Propulsion System
RTX CORPORATION
0 cites
US120185872024
Turbine Airfoil Having Cooling Hole Arrangement
RTX CORPORATION
0 cites
US116618522023
Turbine Blade Trailing Edge Cooling Feed
Raytheon Technologies Corporation
0 cites