237080 ⎘
System and method for reducing specific fuel consumption (SFC) in a turbine powered aircraft
#2Integrated wireless data system for avionics performance indication
#3Auxiliary power unit with electrically driven compressor
#4Unmanned aerial vehicle system and method with environmental sensing
#5Systems and methods for detecting landing gear ground loads
#6Engine assembly for an auxiliary power unit
#7System and method for reducing specific fuel consumption (SFC) in a turbine powered aircraft
#8Fibre-optic communication system and an aircraft
#9Methods and devices for light distribution in an aircraft, and aircraft including such devices
#10Apparatuses, methods and systems for active counter directed energy platform protection
#11Integrated wireless data system for avionics performance indication
#12Unmanned aircraft system (UAS) with active energy harvesting and power management
#13Engine assembly with direct drive of generator
#14Engine assembly with combined engine and cooling exhaust
#15Composite panel power system
#16System and method for harvesting energy from a moving vehicle
#17Auxiliary power unit with combined cooling of generator
#18Auxiliary power unit with electrically driven compressor
#19Compound engine assembly with bleed air
#20Auxiliary power unit with excess air recovery
#21Auxiliary power unit with intercooler
#22Self-contained power unit for implementing a method for optimizing the operability of an aircraft propulsive unit
#23Layer material for arranging on a rotor blade tip of a helicopter, helicopter light system, and helicopter comprising the same
#24Power supply system for an electronic flight bag
#25Apparatuses, methods and systems for active counter directed energy platform protection
#26Aircraft comprising at least one emergency beacon, and such an emergency beacon
#27System for recovering and converting kinetic energy and potential energy as electrical energy for an aircraft
#28System and method for aviation electric power production
#29Energy recovery of an aircraft
#30Self charging door sensor system
#31Stall recovery system for a ram air turbine
#32Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter
#33Aircraft instrument and backup power therefor provided by magneto P-lead
#34Airborne kinetic energy conversion system
#35Emergency lighting system for an aircraft and aircraft comprising such emergency lighting system
#36Methods for recovering waste energy from bleed air ducts
#37Method and system for regulating power in the event of at least one aircraft engine failure
#38Method and architecture for recovery of energy in an aircraft
#39Electronic kit bag
#40Unmanned aerial vehicle
#41Thermoelectric generator in turbine engine nozzles
#42Aircraft air inlet diverter assemblies with improved aerodynamic characteristics
#43Method for optimizing the overall energy efficiency of an aircraft, and main power package for implementing same
#44Method for optimizing the operability of an aircraft propulsive unit, and self-contained power unit for implementing same
#45Apparatus for aircraft with high peak power equipment
#46Apparatus for recovering kinetic energy released during landing of an aircraft after contact with the ground, and method
#47Passenger seat for a system of seats of an aircraft cabin
#48Power supply system with at least a primary power source and an auxiliary power source for powering an electronic flight bag depending on an whether an aircraft is in a flight condition
#49Aircraft capable of hovering having an exhaust duct with thermoelectric conversion circuit
#50Systems and methods for detecting landing gear ground loads
#51Systems and methods for energy conserving wireless sensing with situational awareness
#52Thermoelectric generation for a gas turbine
#53Assembly of actuators and of a system for supplying electrical power from a network
#54Aircraft landing gear monitoring apparatus
#55Lightning strike detection