Device for supplying electrical power to an aircraft on the ground
View Patent ↗A device for supplying electrical power to an aircraft on the ground, including two electric generators driven by an auxiliary power unit. The first generator is connected by a connection/disconnection mechanism to an aircraft network and to an electric taxiing network, to supply either an AC voltage to the aircraft network when it is connected to the aircraft network, or an AC voltage or a power to the taxiing network when it is connected to the taxiing network. The second generator is connected by the connection/disconnection mechanism to the aircraft or taxiing networks to supply the AC voltage to one of those networks.
1. A device for supplying electrical power to an aircraft on the ground, comprising:
two electric generators driven by an auxiliary power unit, the first generator configured to supply an electric taxiing network that comprises electric motors for driving wheels of the aircraft, and the second generator configured to supply an electric aircraft network;
wherein the first generator is connected by selective connection/disconnection means to the aircraft network and the taxiing network, said first generator being configured to supply a first AC voltage to the aircraft network when said first generator is connected to the aircraft network, and wherein said first generator is configured to supply a higher AC voltage or a power to the taxiing network when said first generator is connected to the taxiing network; and
wherein the second generator is connected by selective connection/disconnection means to the aircraft and taxiing networks, said second generator being configured to supply the first AC voltage to the aircraft network when said second generator is connected to said aircraft network, and wherein said second generator is configured to supply the first AC voltage to the taxing network when said second generator is connected to said taxiing network.
2. A device according to claim 1 , wherein one of the generators is a starter/generator configured to start the auxiliary power unit.
3. A device according to claim 2 , further comprising a motor control unit connected to the starter/generator for controlling starting of the auxiliary power unit.
4. A device according to claim 1 , wherein the first generator is a three-stage synchronous generator with wound rotor excitation.
5. A device according to claim 1 , wherein the first generator supplies a voltage of 115 Vac at 400 Hz and a power of 90 kVA when it is connected to the aircraft network.
6. A device according to claim 1 , wherein the first generator provides a power of 150 kW when it is connected to the taxiing network.
7. A device according to claim 1 , wherein the second generator supplies an electric power for supplying electric charges to an aircraft on the ground, and a voltage of 115 Vac at 400 Hz.
8. A method for supplying electrical power to an aircraft on ground by a device according to claim 1 , the method comprising:
supplying the taxiing network by the first generator and the aircraft network by the second generator; and
supplying the aircraft network by the first generator when the taxiing function is not used, with the second generator then being out of service.
9. A method according to claim 8 , wherein the first generator is a three-stage synchronous generator with wound rotor excitation, and the excitation of the first generator is controlled by a motor control unit to switch from a voltage generator to a voltage generator or from a generator of power to a voltage generator.
10. A method according to claim 8 , further comprising supplying the taxiing network by the second generator when the first generator is defective.