Thomas E. Clark

Electrical assembly for a hybrid-electric aircraft propulsion system

Cooling system for aircraft powerplant electronics

GAS TURBINE ENGINE WITH ADAPTIVE TURBINE COOLING AIR SYSTEM AND METHOD

OPEN ROTOR GAS TURBINE ENGINE WITH ADAPTIVE TURBINE CLEARANCE CONTROL SYSTEM AND METHOD

GAS TURBINE ENGINE WITH ADAPTIVE TURBINE CLEARANCE CONTROL SYSTEM AND METHOD

GAS TURBINE ENGINE WITH ADAPTIVE TURBINE CLEARANCE CONTROL SYSTEM AND METHOD

Spool-to-spool powertrain assembly for an aircraft propulsion system

AIRCRAFT POWERPLANT WITH ELECTRIC MACHINE SYSTEM

ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT

ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT

ACCESSORY GEARBOX WITH MULTIPLE POWER TRANSFER SYSTEMS

ELECTRIC CABLE CONDUIT FOR AIRCRAFT POWERPLANT

Aircraft powerplant with ventilated cable conduit

THERMAL MANAGEMENT SYSTEM FOR OPEN ROTOR AIRCRAFT PROPULSION SYSTEM

Electric machine cooling plate for aircraft powerplant

ELECTRICAL LOCKOUT SYSTEM FOR AIRCRAFT PROPULSION SYSTEM

VARIABLE AREA INLET FOR TURBINE ENGINE HEAT EXCHANGE SYSTEM

Aircraft air system with boost compressor(s)

MODULATED AIR FLOW HEAT EXCHANGER SYSTEM IN BI-FI DUCT

TURBINE COOLING AIR THROTTLING VALVE AND SYSTEM FOR HYBRID ELECTRIC ENGINES

Hybrid-electric aircraft propulsion system

HIGH VOLTAGE ENGINE-MOUNTED ELECTRONICS PRESSURIZATION BLEED SYSTEM

Open rotor gas turbine engine with adaptive turbine clearance control system and method

Gas turbine engine with compartment anti-icing system

Aircraft with electrically powered engine accessories

Working fluid system for aircraft powerplant

Reducing eddy current propagation in electric device housing

Aircraft air system with electric boost compressor

LOW SPOOL ELECTRICAL MACHINE ARRANGEMENTS FOR HYBRID-ELECTRIC ENGINES

GEARBOX ARRANGEMENT FOR DUAL SPOOL ENGINE ACCESSORIES

Electronic controller cooling for aircraft propulsion system

Aircraft powerplant gearbox with selectable power coupler

MULTI-SPOOL ENGINE ELECTRICAL LOAD BALANCING TO OPTIMIZE FUEL BURN BASED ON AMBIENT AND SYSTEM THERMAL CONDITIONS

POWER FEEDER CABLE CONDUIT FOR HYBRID ELECTRIC GAS TURBINE ENGINES AND FAN MOUNTED MOTOR CONTROLLERS

FAN EXIT GUIDE VANE THERMAL MANAGEMENT SYSTEM FOR CONVENTIONAL GAS TURBINE ENGINES

FAN EXIT GUIDE VANE THERMAL MANAGEMENT SYSTEM FOR HYBRID ELECTRICS

MODULATED AIR-COOLED HEAT EXCHANGER FOR HYBRID ELECTRIC THERMAL MANAGEMENT SYSTEMS

Translatable guide vanes for aircraft propulsion system

THERMAL MANAGEMENT ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM

THERMAL MANAGEMENT ASSEMBLY FOR A HYBRID-ELECTRIC AIRCRAFT PROPULSION SYSTEM

DIRECT DRIVE WITH ELECTRIC MACHINE INTEGRATED LOW SPOOL SHAFT FOR HYBRID ENGINE

Boost compressor augmentation for hybrid electric thermal management systems

Aircraft powerplant gearbox with selectable power coupler

ELECTRICAL SYSTEM FOR AIRCRAFT PROPULSION SYSTEM

HYBRID ELECTRIC GAS TURBINE ENGINE TWO SPEED TRANSMISSION FOR LOW SPOOL DRIVE POWER INJECTION AND POWER EXTRACTION

GAS TURBINE ENGINE WITH IMPROVED HIGH PRESSURE COMPRESSOR LEAKAGE PATH GUIDE STRUCTURE

GAS TURBINE ENGINE CONFIGURED FOR DECREASED DIFFUSER WINDAGE AND METHOD OF ASSEMBLING THE SAME

INTERCOOLED COMBUSTOR NOZZLE GUIDE VANE AND SECONDARY AIR CONFIGURATION

Air seal system with backside abradable layer

Gas turbine engine including flow path flex seal and heat shield

Gas turbine engine including flow path flex seal with cooling air bifurcation

Air seal system with backside abradable layer

CMC component with integral cooling channels and method of manufacture

ATTACHMENT REGION FOR CMC COMPONENTS