Inventor

ROBERGE GARY D

US123 patents

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

ROBERGE GARY D

UNITED TECHNOLOGIES CORP

Hybrid expander cycle with pre-compression cooling and turbo-generator

Systems and methods for fan blade de-icing

Thermal management of tail cone mounted generator

Electromagnetic anti-windmilling system

Architecture for an axially compact, high performance propulsion system

Anti-windmilling system for a gas turbine engine

Cantilevered tip turbine engine

Bevel gear lubrication and cooling

Systems and methods for power transfer in cryogenic fuel applications

Hybrid expander cycle with intercooling and turbo-generator

Hybrid expander cycle with turbo-generator and cooled power electronics

Rotating airfoil with tip pocket

Fan drive gear system

Integrated heat exchangers for low fan pressure ratio geared turbofan

Geared turbofan with high speed generator

Gas turbine engine systems and related methods involving multiple gas turbine cores

Ejector cooling of outer case for tip turbine engine

Vectoring transition duct for turbine engine

Axial compressor for tip turbine engine

Decoupled ducting for twin-engine reaction rotor drive

Duct mounted heat exchanger

Thermal management system for gas turbine engine

Rotor assembly with internal vanes

Variable speed boost compressor for gas turbine engine cooling air supply

Oil thermal management system for cold weather operations of a gas turbine engine

Low speed fan for gas turbine engines

Gas turbine engine structure with integrated actuation features

Airfoil deicing system

Thermal shield for gas turbine engine diffuser case

Concentric power takeoff transmission

Variable speed boost compressor for gas turbine engine cooling air supply

Panel based heat exchanger

Energy absorbing beam and sandwich panel structure

Seal interface with a deflection control feature

Method of making light weight component with internal metallic foam and polymer reinforcement

Flow path routing within a gas turbine engine

ROBERGE GARY D

Gas turbine engine systems involving tip fans

Gas turbine engine systems and related methods involving multiple gas turbine cores

Systems and methods involving localized stiffening of blades

Auxiliary propulsor for a variable cycle gas turbine engine

Gas turbine engine systems involving tip fans

Rear propulsor for a variable cycle gas turbine engine

RAYTHEON TECH CORP

Multi-mode heat rejection system for a gas turbine engine

Thermal management of tail cone mounted generator

Auxiliary device for three air flow path gas turbine engine

Fan drive gear system

Anti-windmilling system for a gas turbine engine

SUCIU GABRIEL L

Stacked annular components for turbine engines

NORRIS JAMS W

Reversed-flow core for a turbofan with a fan drive gear system

SUCIU GABRIEL

Particle separator for tip turbine engine