Device and method for emergency electricity supply on board an aircraft
View Patent ↗A device and a method for emergency electricity supply on board an aircraft, able to supply a part of the aircraft's electrical power circuit. The device includes a synchronous machine with separate excitation, associated with a flywheel, and an auxiliary device to set the flywheel in rotation and to maintain rotation of the flywheel.
1. A device for supplying emergency electricity to at least a part of an electrical power circuit on board an aircraft, comprising:
a first synchronous machine associated with a first excitation and a flywheel;
an auxiliary device that sets the flywheel in rotation and maintains the rotation of the flywheel; and
a second synchronous machine associated with a second excitation that is separate from the first excitation, the second synchronous machine being associated with a ram air turbine, wherein
the auxiliary device is connectable to a bus bar via a first three-phase contactor, and
the first synchronous machine is connectable:
to the auxiliary device,
to the bus bar via a second three-phase contactor, and
to the second synchronous machine via the second three-phase contactor and a third three-phase contactor.
2. The device according to claim 1 , wherein the auxiliary device includes two static converters.
3. The device according to claim 2 , wherein the first converter is a three-phase rectifier used to obtain direct voltage.
4. The device according to claim 2 , wherein
the second converter is a three-phase inverter, and
the auxiliary device is configured to self-pilot the first synchronous machine.
5. The device according to claim 1 , wherein the aircraft is an airplane.
6. The device according to claim 5 , wherein the airplane is an all-electric airplane.
7. An aircraft comprising the device according to claim 1 .
8. A method to provide an emergency electricity supply on board an aircraft, comprising:
supplying, by a first synchronous machine associated with a first excitation and a flywheel, emergency electricity to at least a part of an electrical power circuit in event of total failure of electricity generation;
setting, by an auxiliary device, the flywheel in rotation;
maintaining, by the auxiliary device, the rotation of the flywheel;
supplying, by a second synchronous machine associated with a second excitation that is separate from the first excitation, the second synchronous machine being associated with a ram air turbine, electricity to the electrical power circuit of the aircraft;
coupling the flywheel to the part of the electrical power circuit instantly in the event of total failure of electricity generation; and
uncoupling the flywheel from the electrical power circuit after a time needed for deployment and setting in rotation of the ram air turbine, wherein
the auxiliary device is connectable to a bus bar via a first three-phase contactor.
9. The method according to claim 8 , further comprising a step of recharging, via the auxiliary device, the flywheel using the part of the electrical power circuit.
10. The method according to claim 8 , further comprising a step of coupling the flywheel to the part of the electrical power circuit during landing of the aircraft when the ram air turbine becomes inactive to supply the necessary power for braking of the airplane.