By substituting aluminum forgings for steel, weight of flexible engine suspension for Pratt and Whitney R-4360 engine was reduced from 134 to 71.5 lb; mounting described; endurance life of link; conclusions from fatigue tests on 26 assemblies; redesign of link explained; it incorporates antifretting corrosion reliefs and chromic acid anodizing.


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    Title :

    Fatigue life of aircraft engine mounting components


    Additional title:

    Soc Automotive Engrs -- J


    Contributors:


    Publication date :

    1950


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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