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Norm

ÖNORM EN 4662

Issue date: 2010 10 01

Aerospace series - Test specification for vibration control components

This standard specifies the procedure and the parameter for testing static and dynamic stiffness of vibration control components (e.g. shock mounts with bushes). This s...
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Valid
Publisher:
Austrian Standards International
Format:
Digital | 12 Pages
Language:
German | English | Download GER/ENG
Optionally co-design standards:
Committee 237: Aerospace
ICS
49.035 17.160
Topics
Safety, Occupational safety, Vibrations, shock and vibration measurements Traffic & transport, Aircraft and space vehicle engineering, Components for aerospace construction
This standard specifies the procedure and the parameter for testing static and dynamic stiffness of vibration control components (e.g. shock mounts with bushes). This standard applies to vibration control components all installed for aircraft applications. It may be applied when referred to in the product standard or in a design specification.
ÖNORM EN 4662
2010 10 01
Aerospace series - Test specification for vibration control components
Norm
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