Patents/Inventors

Andrew E. Breault

Bolton, CTUS23 patents

19 Patents

US125898782026
Hybrid-electric Aircraft Propulsion System
RTX Corporation
0 cites
US125653282026
Differential Driven Open Rotor with Brake
RTX Corporation
0 cites
US125533802026
Constant Speed Accessory Gearbox for Turbine Engine
RTX CORPORATION
0 cites
US125533922026
Gas Turbine Engine with Thermal Management
RTX Corporation
0 cites
US125536092026
Intercooled Combustor Nozzle Guide Vane and Secondary Air Configuration
RTX Corporation
0 cites
US125454152026
Gas Turbine Engine Aircraft Mounting System
RTX Corporation
0 cites
US125405782026
Hybrid Electric Gas Turbine Engine Two Speed Transmission for Low Spool Drive Power Injection and Power Extraction
RTX Corporation
0 cites
US125100302025
Aft Mounted Pusher Fan for Gas Turbine Engine
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
US123788932025
Buffer Air Assembly for an Aircraft Engine
RTX Corporation
0 cites
US123521852025
Open Rotor Variable Pitch Blade with Retracting Inboard Trailing Edge
RTX Corporation
0 cites
US123202702025
Gas Turbine Engine with Bypass TOBI Cooling/purge Flow and Method
RTX Corporation
0 cites
US120186202024
AFT Mounted Pusher Fan for Gas Turbine Engine
RTX Corporation
0 cites
US119204872024
Gas Turbine Engine Including Flow Path Flex Seal with Cooling Air Bifurcation
RTX Corporation
0 cites