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IEC 60952-2

Aircraft batteries – Part 2: Design and construction requirements

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Organization: IEC
Publication Date: 1 July 2013
Status: active
Page Count: 78
ICS Code (Aerospace electric equipment and systems): 49.060
ICS Code (Acid secondary cells and batteries): 29.220.20
scope:

This part of IEC 60952 series defines the physical design, construction and material requirements for nickel-cadmium and lead-acid aircraft batteries containing vented or valveregulated cells or monoblocs.

The batteries are used for both general purposes and specific aerospace applications. The specific topics addressed in this part serve to establish acceptable quality standards required to qualify a battery as airworthy as defined in Clause 3 of IEC 60952-1:2013.

A preferred range of aircraft batteries is specified in Annex A, but this part of IEC 60952 series may be used for other battery sizes, arrangements and ratings. For particular applications, other design requirements may be stipulated. These will be in addition to the requirements of this part and will be covered by specific documents.

It is recognised that additional data may be required by other organisations (national standards bodies, AECMA, SAE, etc.). The present standard can be used as a framework to devise tests for generation of the required data

Document History

IEC 60952-2
July 1, 2013
Aircraft batteries – Part 2: Design and construction requirements
This part of IEC 60952 series defines the physical design, construction and material requirements for nickel-cadmium and lead-acid aircraft batteries containing vented or valveregulated cells or...
September 1, 2004
Aircraft Batteries Part 2: Design and Construction Requirements
A description is not available for this item.
January 1, 1991
Aircraft Batteries Part 2: Design and Construction Requirements; (CENELEC EN 60952-2: 1993)
A description is not available for this item.

References

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