Inventor

SUCIU GABRIEL L

US444 patents

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

SUCIU GABRIEL L

UNITED TECHNOLOGIES CORP

Geared architecture for high speed and small volume fan drive turbine

Geared architecture for high speed and small volume fan drive turbine

Fundamental gear system architecture

Geared architecture for high speed and small volume fan drive turbine

Segmented interstage seal assembly

Bleed valve for axial flow compressor

Low profile bearing support structure

Gas turbine engine with high speed low pressure turbine section

Turbine section of high bypass turbofan

Gas turbine engine thermal management system for heat exchanger using bypass flow

Reverse core engine with thrust reverser

Cantilevered tip turbine engine

Hydraulic seal for a gearbox of a tip turbine engine

Gas turbine engine front architecture modularity

Heat exchange system

Geared architecture for high speed and small volume fan drive turbine

Tip turbine engine support structure

Variable rotor blade for gas turbine engine

Seal assembly for a fan rotor of a tip turbine engine

Tip turbine engine with a heat exchanger

Turbine engine rotor stack

Turbine engine rotor stack

Turbine engine disk spacers

Turbine engine rotor retainer

Gas turbine engine shaft bearing configuration

Gas turbine engine shaft bearing configuration

SUCIU GABRIEL L

Gas turbine engine buffer cooling system

Gearbox assembly

Stacked annular components for turbine engines

Shared flow thermal management system

Counter-rotating low pressure turbine with gear system mounted to mid turbine frame

Ceramic matrix composite vane structures for a gas turbine engine turbine

Compression system for turbomachine heat exchanger

Gas turbine engine driving multiple fans

Gas turbine engine oil tank

Geared turbofan with three turbines all counter-rotating

Counter rotating low pressure turbine with splitter gear system

Gas turbine engine compressor arrangement

Engine mount system for a turbofan gas turbine engine

Turbomachine thermal management

Integrated actuator module for gas turbine engine

Integrated inlet vane and strut

ALVANOS IOANNIS

Integrated case and stator

Hybrid Ceramic Matrix Composite vane structures for a gas turbine engine

Hybrid rotor disk assembly with a ceramic matrix composite airfoil for a gas turbine engine

MERRY BRIAN D

Gas turbine engine shaft bearing configuration

Gas turbine engine compressor case mounting arrangement

MCCUNE MICHAEL E

Systems and methods involving multiple torque paths for gas turbine engines

ROBERGE GARY D

Gas turbine engine systems involving tip fans

HIPSKY HAROLD W

Environmental control system for aircraft utilizing turbo-compressor