Flight system and method for responding failure thereof
AssigneesHyundai Motor Company, Kia Corporation
InventorsHyun Ki Cho, Jin Soo Jang, Yoon Cheol Jeon, Jong Pil Kim
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Abstract
The present disclosure relates to a flight system and a failure responding method therefor. A flight system includes: a plurality of fuse boxes configured to control application of a voltage to at least one propulsion device; and an interlock control apparatus configured to control interlock lines between fuse boxes connected using the interlock lines among the fuse boxes to synchronize and control opening of the fuse boxes connected using the interlock lines.
Claims20
A flight system comprising:
- a plurality of fuse boxes, wherein each fuse box, of the plurality of fuse boxes, is configured to control application of a voltage to at least one propulsion device of a plurality of propulsion devices;
- and
- an interlock control apparatus configured to control connection of at least one interlock line between at least two fuse boxes, of the plurality of fuse boxes, connected via the at least one interlock line to synchronize control opening of the at least two fuse boxes,
- each of the plurality of fuse boxes is configured to be connected with a corresponding one of the plurality of propulsion devices, and fuse boxes of the plurality of fuse boxes are connected to an interlock line and synchronized with each other,
- wherein the interlock control apparatus comprises a switching device configured to be turned off based on a short-circuit of the at least one interlock line.
A method performed by a flight system, the method comprising:
- applying a voltage to at least one propulsion device of a plurality of propulsion devices, wherein each propulsion device of the plurality of propulsion devices is coupled to a fuse box of a plurality of fuse boxes, and wherein at least two fuse boxes of the plurality of fuse boxes are coupled via at least one interlock line between the at least two fuse boxes;
- synchronizing and controlling opening of the at least two fuse boxes by controlling opening of the at least one interlock line;
- and
- turning off a switching device based on a short-circuit of the at least one interlock line.
A flight system comprising:
- a plurality of fuse boxes, wherein each fuse box, of the plurality of fuse boxes, is configured to control application of a voltage to a propulsion device of a plurality of propulsion devices;
- and
- a controller circuit configured to control connection of an interlock line between paired fuse boxes, of the plurality of fuse boxes, connected via the interlock line to synchronize control opening of the paired fuse boxes,
- wherein, the paired fuse boxes comprises a first fuse box and a second fuse box,
- wherein the controller circuit comprises a switch configured to be:
- turned off based on a first state associated with the paired fuse boxes, and
- turned on based on a second state associated with at least one of the paired fuse boxes, to apply a control power to a driving controller of the first fuse box and a driving controller of the second fuse box.
Dependencies are inferred from the claim text.