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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Clamps, Support, Comparative Fatigue Strengths, Test Method


    Publication date :

    2013-01-02



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English






    Clever clamps

    Online Contents | 1997


    WHEEL CLAMPS

    KAVANAGH CHRISTOPHER JOHN / BRYNE EIVIND / FURU HARALD et al. | European Patent Office | 2023

    Free access

    HOSE CLAMPS

    SAE Technical Papers | 1971