An electrical harness including at least one upstream connector arranged to be electrically connected to a computer, at least one
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An electrical harness including at least one upstream connector arranged to be electrically connected to a computer, at least one
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An aircraft electrical apparatus comprises an engine starter motor control unit (1) configured to provide an AC input voltage to a
...Electrical circuit for control of an electrical device with high integrity
The invention relates to: Control circuit (1) for an electrical device (2), said control circuit (1) receiving as input a discrete
...Electrical architecture for aircraft
The invention relates to an electrical architecture (2) for an aircraft, comprising:-a first propulsion power distribution system (16
...ELECTRICAL CIRCUIT FOR CONTROL OF AN ELECTRICAL DEVICE WITH HIGH INTEGRITY
The invention relates to: Control circuit (1) for an electrical device (2), said control circuit (1) receiving as input a discrete
...Control method for an electrical braking system and electrical braking system for aircraft
A control method of an electrical braking system for aircraft includes a plurality of electromechanical actuators capable of applying a
...CONTROL METHOD FOR AN ELECTRICAL BRAKING SYSTEM AND ELECTRICAL BRAKING SYSTEM FOR AIRCRAFT
A control method of an electrical braking system for aircraft includes a plurality of electromechanical actuators capable of applying a
...AIRCRAFT ELECTRICAL ENERGY SUPPLY NETWORK
An electrical energy supply network of an aircraft equipped with a plurality of electrical loads to be supplied includes at least two
...PROTECTION DEVICE FOR ELECTRICAL CABINET
A protection device for an electrical cabinet is divided into a plurality of compartments, the protection device including a rain guard
...Electrical harness for a turbomachine
The present invention relates to an electrical harness (1) comprising at least one first cable strand (2) and at least one second cable
...AIRCRAFT ELECTRICAL ENERGY SUPPLY NETWORK
The invention concerns an electrical energy supply network (1) of an aircraft equipped with a plurality of electrical loads (C1, C2) to
...APPARATUS FOR PROVIDING AN ELECTRICAL CONNECTION
STATOR WINDING FOR AN ELECTRICAL MACHINE
A novel method of manufacture and an improved construction of windings of a stator of an electrical machine are provided, which minimise
...Protection device for electrical cabinet in aircraft
A protection device for an electrical cabinet is divided into a plurality of compartments, the protection device including a rain guard
...SYSTEM FOR CONTROLLING AN AIRCRAFT ELECTRICAL NETWORK
SYSTEM FOR CONTROLLING AN AIRCRAFT ELECTRICAL NETWORK
System for controlling an aircraft electrical network comprising at least a first propulsion assembly having at least one left-hand
...Unit for generating non-propulsive electrical power
A unit (1′, 10′, 100′) for generating non-propulsive electrical power for use on board an aircraft, the unit (1′, 10′, 100′) comprising
...Electrical power distribution assembly for an aircraft
An electrical power distribution assembly for an airplane, the assembly including an electric switch device for placing in a Karman
...Method of controlling an electrical taxiing system
A control method for controlling an electrical taxiing system adapted to moving an aircraft while it is taxiing, the method comprising
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