Power distribution arrangement especially in an aircraft
AssigneeDaimlerChrysler Aerospace Airbus GmbH
InventorsWerner Weiler, Michael Krumbholz
Life of this patent
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AssigneeDaimlerChrysler Aerospace Airbus GmbH
InventorsWerner Weiler, Michael Krumbholz
Estimating the term…
A power distribution arrangement, especially in an aircraft, includes plural power sources, a power line having plural power supply strands connected to the power sources, plural power consumer groups each including plural power consuming devices, and branch lines respectively connecting the power line with the power consumer groups. A respective allocation unit selectively interconnects the power consuming devices of each group with selected individual branch line strands of the branch lines. A status unit acquires information regarding the respective operating status of the power sources and the power line strands, and conveys corresponding information regarding a power failure on any power line strand to a central power control unit, which correspondingly transmits control commands over a control bus to the respective allocation units. In response to the control commands, each allocation unit automatically disconnects power consuming devices from any power line strand that has failed and reconnects the devices to another power line strand that is still operating properly. In this manner, the allocation of power consuming devices to the several power line strands can be reconfigured automatically or by manual inputs without requiring a mechanical rearrangement of power system components, and it is possible to a large extent to ensure that power will continue to be provided to important power consuming devices despite the failure of any one or more power supply circuits or branches.
A power distribution apparatus comprising:
An electrical power distribution system in an aircraft, said system comprising:
A method for controlling a power distribution system including a plurality of power sources, a plurality of power line strands respectively connected to said power sources, a plurality of branch line strands respectively connected to said power line strands, a plurality of power consuming devices, a plurality of feeder lines respectively connected to said power consuming devices, a status evaluation unit adapted to evaluate an operating status of at least one of said power sources, said power line strands and said branch line strands, and a selective interconnection switching junction interposed and connected between said feeder lines and said branch line strands and adapted to selectively interconnect one or more respective ones of said feeder lines with respective selected ones of said branch line strands, said method comprising the following steps:
Dependencies are inferred from the claim text.