Aircraft Hybrid remote power controllers General requirements

Available format(s)

Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users

Language(s)

English, French

Published date

07-23-1992

Publisher

International Organization for Standardization

Specifies the general design and performance requirements. The controllers 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, they are used to close and open the electrical circuit and to protect wiring and equipment in the event of overload or short-circuit conditions.

DevelopmentNote	Also numbered as BS G248(1993). (06/2005)
DocumentType	Standard
Pages	11
PublisherName	International Organization for Standardization
Status	Current

18/30334464 DC : 0

BS ISO 20949 - AIRCRAFT - SMART CONTACTOR - GENERAL REQUIREMENTS

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