Descent operation for an aircraft parallel hybrid gas turbine engine propulsion system
BUILD PLATE INTEGRATED INTO ADDITIVE MANUFACTURED COMPONENT
SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM
Rating control architecture and method for hybrid electric engine
HYBRID-ELECTRIC SINGLE ENGINE DESCENT FAILURE MANAGEMENT
Hybrid electric engine including auxiliary compressor
Aircraft hybrid propulsion fan drive gear system DC motors and generators
Gas turbine engine mounted above wing and with camber
SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM
Turbine over-speed brake for hybrid electric gas turbine engine