Electrical system for an aircraft
AssigneeAirbus Operations GmbH
InventorsJens Schult, Henning Everth, Fabian Kraus
Life of this patent
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Abstract
An electrical system for an aircraft is provided. The system comprises an inverter for transforming a first alternating current from an on-board network having a variable frequency into a second alternating current, and at least a first electrical load and at least a second electrical load, which are configured to be operated simultaneously by the second alternating current.
Claims18
An electrical system for an aircraft, the electrical system comprising:
- an inverter for transforming a first alternating current from an on-board network having a variable frequency into a second alternating current;
- and
- at least a first electrical load and at least a second electrical load, which are operated simultaneously by the second alternating current.
An aircraft, comprising:
- a generator that is mechanically coupled with a drive of the aircraft to supply an on-board network of the aircraft with electrical energy;
- and
- an electrical system that includes an inverter that transforms a first alternating current from an on-board network having a variable frequency into a second alternating current, and at least a first electrical load and at least a second electrical load that are operable simultaneously by the second alternating current,
- wherein the electrical system is coupled with the on-board network via the inverter.
A method for operating an electrical system of an aircraft, comprising:
- transforming an alternating current from an on-board network having a variable first frequency into a second alternating current having a second frequency;
- and
- operating at least one first electrical load and at least one second electrical load with the second alternating current.
A computer program product, comprising:
- a non-volatile storage medium readable by a processor and storing instructions for execution by the processor for performing a method comprising:
- transforming an alternating current from an on-board network having a variable first frequency into a second alternating current having a second frequency;
- and
- operating at least one first electrical load and at least one second electrical load with the second alternating current.
A control unit for an electrical system of an aircraft, which is configured to carry out a method comprising:
- transforming an alternating current from an on-board network having a variable first frequency into a second alternating current having a second frequency;
- and
- operating at least one first electrical load and at least one second electrical load with the second alternating current.
Dependencies are inferred from the claim text.