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BS G 248:1993

BS G 248:1993

$102.76

Specification for hybrid remote power controllers. General requirements

Published By Publication Date Number of Pages
BSI 1993 16
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This International Standard specifies the general design and performance requirements of hybrid remote power controllers for aircraft. They consist of an electromagnetic device or a combined electromagnetic/solid-state device, for load switching, and a solid-state control circuit for control of the load-switching devices.

On aircraft, remote power controllers are used to close and open the electrical circuit and to protect wiring and equipment in the event of overload or short-circuit conditions.

The load-switching device and solid-state control circuit may be mounted in a common enclosure or may be discrete inter-connected units.

NOTE 1 This International Standard recognizes the need to have hybrid units which are, as far as practical, interface-compatible with fully solid-state power controllers.

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BS G 248:1993
$102.76