Andrew E. Breault

CONTROL SYSTEM FOR OPEN ROTOR PROPULSION SYSTEM WITH ONE OR MORE SENSORS

AIRCRAFT WITH SYMMETRIC PROPULSION SYSTEM ROTATING PATTERNS

STARTING OPEN ROTOR PROPULSION SYSTEM DURING AIRCRAFT FLIGHT

Control system for open rotor propulsion system with one or more sensors

ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT

ELECTRIC MACHINE COOLING PLATE FOR AIRCRAFT POWERPLANT

SLIDABLE LINERS IN SWIRL RECOVERY VANE STRUCTURE

RIBBED STRUCTURAL GUIDE VANE WITH ACOUSTIC CAPABILITY

Slidable Liners in Fan Exit Guide Vane Structure

ADDITIVE FAN EXIT GUIDE VANE STRUCTURE WITH ACOUSTIC CAPABILITY

RIBBED STRUCTURAL SWIRL RECOVERY VANE WITH ACOUSTIC CAPABILITY

ADDITIVE SWIRL RECOVERY VANE WITH ACOUSTIC CAPABILITY

AIRCRAFT WITH SYMMETRIC OPEN PROPULSOR ROTATING PATTERNS

AIRCRAFT WITH SYMMETRIC OPEN PROPULSOR ROTATING PATTERNS

ELECTRICAL LOCKOUT SYSTEM FOR AIRCRAFT PROPULSION SYSTEM

AIRCRAFT PROPULSION SYSTEM WITH SELECTIVELY ROTATABLE OPEN PROPULSOR ROTOR

AIRCRAFT PROPULSION SYSTEM WITH SELECTIVELY ROTATABLE OPEN PROPULSOR ROTOR

VARIABLE AREA INLET FOR TURBINE ENGINE HEAT EXCHANGE SYSTEM

OPEN ROTOR PROPULSION SYSTEM WITH FORWARD EXHAUST OUTLET(S)

OPEN ROTOR PROPULSION SYSTEM WITH EXHAUST MIXER(S)

Hybrid-electric aircraft propulsion system

HIGH VOLTAGE ENGINE-MOUNTED ELECTRONICS PRESSURIZATION BLEED SYSTEM

FUEL NOZZLE THERMAL MANAGEMENT SYSTEM

ADJUSTING PITCH FOR AIRFOILS OF AN AIRCRAFT PROPULSION SYSTEM

Gas turbine engine aircraft mounting system

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH MULTI-GEAR SYSTEM GEARTRAIN

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH MULTI-GEAR SYSTEM GEARTRAIN

OPEN ROTOR WITH AERODYNAMICALLY ISOLATABLE FREE TURBINE

TURBINE ENGINE TIP CLEARANCE CONTROL SYSTEM WITH THRUST BEARING

Differential Driven Open Rotor with Brake

GAS TURBINE ENGINE BUFFER AIR AUGMENTATION SYSTEM AND METHOD

Gas Turbine Engine with Thermal Management

ACTUATABLE INSPECTION PROBE FOR NON-DESTRUCTIVE INSPECTION

Thermal management system for gas turbine engine with open propulsor

AFT GEAR BASED ENGINE WITH HEAT RECOVERY SYSTEM

OPEN PUSHER ROTOR WITH REMOTE EXHAUST

GAS TURBINE ENGINE WITH BYPASS TOBI COOLING/PURGE FLOW AND METHOD

CONTINUOUS FLOW FUEL SYSTEM

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH BYPASS FLOWPATH

Open rotor aircraft propulsion system with bypass flowpath

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH BYPASS FLOWPATH

INTERMEDIATE CASE FOR AIRCRAFT PROPULSION SYSTEM HOUSING

CONSTANT SPEED ACCESSORY GEARBOX FOR TURBINE ENGINE

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

Open rotor variable pitch blade with retracting inboard trailing edge

OPEN ROTOR AIRCRAFT PROPULSION SYSTEM WITH ANTI-ICING SYSTEM

TURBINE ENGINE ACCESSORY SYSTEM WITH MULTIPLE GEARBOXES

BUFFER AIR ASSEMBLY FOR AN AIRCRAFT ENGINE

TURBINE ENGINE TIP CLEARANCE CONTROL SYSTEM WITH THRUST BEARING

BUFFER AIR ASSEMBLY FOR AN AIRCRAFT ENGINE

WATER ACTUATED TIP CLEARANCE CONTROL SYSTEM FOR TURBINE ENGINE

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

Gas turbine engine with bypass TOBI cooling/purge flow and method

AFT MOUNTED PUSHER FAN FOR GAS TURBINE ENGINE

AFT MOUNTED PUSHER FAN FOR GAS TURBINE ENGINE

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