Inventor
BREAULT ANDREW E
US19 patents
⚠️ This page may combine multiple inventors who share the name “BREAULT ANDREW E”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
RTX CORP
15 patentsUS12352185B1Jul 8, 2025
Open rotor variable pitch blade with retracting inboard trailing edge
RTX CORP0 citations62
US12448901B1Oct 21, 2025
Thermal management system for gas turbine engine with open propulsor
RTX CORP0 citations61
US12545415B1Feb 10, 2026
Gas turbine engine aircraft mounting system
RTX CORP0 citations60
US12510030B2Dec 30, 2025
Aft mounted pusher fan for gas turbine engine
RTX CORP0 citations60
US12018620B1Jun 25, 2024
AFT mounted pusher fan for gas turbine engine
RTX CORP0 citations60
US12565328B2Mar 3, 2026
Differential driven open rotor with brake
RTX CORP0 citations51
US12553609B2Feb 17, 2026
Intercooled combustor nozzle guide vane and secondary air configuration
RTX CORP0 citations51
US12540578B2Feb 3, 2026
Hybrid electric gas turbine engine two speed transmission for low spool drive power injection and power extraction
RTX CORP0 citations51
US12404812B1Sep 2, 2025
Open rotor aircraft propulsion system with bypass flowpath
RTX CORP0 citations51
US12553392B2Feb 17, 2026
Gas turbine engine with thermal management
RTX CORP0 citations50
US12460819B2Nov 4, 2025
Continuous flow fuel system
RTX CORP0 citations50
US12460577B2Nov 4, 2025
AFT gear based engine with heat recovery system
RTX CORP0 citations50
US12397924B2Aug 26, 2025
Open rotor aircraft propulsion system with bypass flowpath
RTX CORP0 citations50
US12589878B1Mar 31, 2026
Hybrid-electric aircraft propulsion system
RTX CORP0 citations47
US12553380B2Feb 17, 2026
Constant speed accessory gearbox for turbine engine
RTX CORP0 citations38
RAYTHEON TECH CORP
4 patentsUS11920487B1Mar 5, 2024
Gas turbine engine including flow path flex seal with cooling air bifurcation
RAYTHEON TECH CORP0 citations62
US12378893B2Aug 5, 2025
Buffer air assembly for an aircraft engine
RAYTHEON TECH CORP0 citations51
US12421863B2Sep 23, 2025
Turbine engine tip clearance control system with thrust bearing
RAYTHEON TECH CORP0 citations50
US12320270B2Jun 3, 2025
Gas turbine engine with bypass TOBI cooling/purge flow and method
RAYTHEON TECH CORP0 citations45