This SAE Aerospace Standard (AS) establishes vibration and transmissibility test procedures which compare the relative strengths of various loop and saddle type support clamps. This procedure is intended for conducting fatigue testing which is standard throughout the aerospace industry thereby establishing a clamp strength comparison that can be used in an evaluation process. The testing required by this document ensures that clamps will meet adequate fatigue requirements only. It does not infer qualification of the clamp installation techniques or its ability to meet in-service environments or operating conditions. Separate qualification testing should be performed to ensure satisfactory service of the installed clamp. AS1974 has been reaffirmed to comply with the SAE five-year review policy.
Clamps, Support, Comparative Fatigue Strengths, Test Method
2013-01-02
Conference paper
English
Clamps, Support, Comparative Fatigue Strengths, Test Method
SAE Technical Papers | 2008
Clamps, Support, Comparative Fatigue Strengths, Test Method
SAE Technical Papers | 2007
Online Contents | 1997
SAE Technical Papers | 1971