145642 ⎘
Control; Purpose of the control system to cope with emergencies of one engine in a multi-engine system
AUTOMATED CONTROL OF TURBINE ENGINES OF A ROTARY-WING AIRCRAFT DURING A FAILURE ON A TURBINE ENGINE
#2VERTICAL TAKEOFF AND LANDING AIRCRAFT
#3Reduced-engine operation technique for rotorcraft
#4Restarting a gas turbine engine
#5Restarting a plurality of engines of an aircraft
#6Air system switching system to allow aero-engines to operate in standby mode
#7Aircraft propulsion system
#8Aircraft and method of operating same
#9Vertical takeoff and landing aircraft
#10Flanged integral piston bearing
#11Method for checking the maximum available power of a turbine engine of an aircraft equipped with two turbine engines
#12Device for temporarily increasing turbomachine power
#13Precision operator for an aircraft autothrottle or autopilot system with engine performance adjust
#14Air system switching system to allow aero-engines to operate in standby mode
#15Operation of a vertical takeoff and landing aircraft
#16Vertical takeoff and landing aircraft
#17Vertical takeoff and landing aircraft having a diffusion assembly for lift fan(s)
#18Vertical takeoff and landing aircraft
#19Vertical takeoff and landing aircraft
#20Precision operator for an aircraft autothrottle or autopilot system with engine performance adjust
#21Vertical takeoff and landing aircraft
#22Vertical takeoff and landing aircraft
#23Vertical takeoff and landing aircraft having a forward thrust propulsor
#24VTOL vehicle with fan blades outside of exhaust flowpath
#25Vertical takeoff and landing aircraft
#26Vertical takeoff and landing aircraft
#27Method for automatic shutdown of engines of a twin-engined aircraft
#28Aircraft comprising a turbine engine incorporated into the rear fuselage with variable supply
#29Control system for rotorcraft in-flight engine restarting
#30Pneumatic device for rapidly reactivating a turbine engine, architecture for a propulsion system of a multi-engine helicopter provided with such a device, and corresponding helicopter
#31Method for detecting a failure of a first turbine engine of a twin-engine helicopter and for operating the second turbine engine, and corresponding device
#32Hydraulic device for emergency starting a turbine engine, propulsion system of a multi-engine helicopter provided with one such device, and corresponding helicopter
#33Method for automatically controlling the operating speed of a helicopter turboshaft engine, corresponding control device and helicopter provided with such a device
#34Assisting the piloting of a multi-engined rotorcraft in an engine-failure situation, in the context of a main rotor of the rotorcraft being driven at variable speed
#35Method of stopping a rotorcraft engine in overspeed, and a system and a rotorcraft associated therewith
#36Aircraft with an engine having a by-pass air inlet opening and a bleed air outlet
#37Device and method for temporarily increasing power
#38Aircraft power system
#39POWER PLANT AND POWER PLANT OPERATING METHOD
#40Aircraft power plant, an aircraft, and a method of piloting said aircraft
#41Fan control apparatus