Assembly for controlling solid-state switching elements in an aircraft
Disclosed herein is an assembly for controlling solid-state switching elements in an aircraft having at least one power pathway (1a, 1b) comprising at least one power line (6a, 6b) supplying power toat least one item of equipment on board an aircraft from at least one electrical power source via a p...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | Disclosed herein is an assembly for controlling solid-state switching elements in an aircraft having at least one power pathway (1a, 1b) comprising at least one power line (6a, 6b) supplying power toat least one item of equipment on board an aircraft from at least one electrical power source via a power switch (7a, 7b), and at least one control member (9a, 9b) controlling at least one power switch (7a, 7b) according to control signals arising from a control means (10a, 10b). The control assembly comprises a single power supply (3) supplying power to the control members (9a, 9b).
本公开涉及种用于控制航空器中固态开关元件的组件,该组件具有:至少个供电路径(1a、1b),该供电路径包括:至少个电源线(6a、6b),用于从至少个电源通过电源开关(7a、7b)向航空器机载的至少个设备项供电;以及至少个控制机构(9a、9b),所述控制机构根据控制装置(10a、10b)产生的控制信号控制至少个电源开关(7a、7b),控制组件包括向控制机构(9a、9b)供电的单个电源(3)。 |
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