Review of problem areas relating to system leakage, pump operational and fluid-induced problems, systems filtration assemblies, and system equipment installations; corrective action undertaken by Trans World Airlines, Inc, leading to improved reliability and operational safety; examples relate to development and adoption of teflon "slipper" seal combined with standard O-ring; flexible hose assemblies in Skydrol fluid systems incorporating butyl-rubber or teflon material liner, MS flareless type fitting, etc; system design details; pump operational reliability improvements.


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    Title :

    Improved reliability in transport aircraft hydraulic systems


    Additional title:

    SAE -- Paper


    Contributors:
    Moore, G.F. (author)

    Conference:

    SAE Meeting ; 1964 Hydraulic equipment



    Publication date :

    1964


    Size :

    6 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    Improved Reliability in Transport Aircraft Hydraulic Systems

    Moore, George F. | SAE Technical Papers | 1964


    Supersonic transport aircraft hydraulic systems

    Billet, A.B. | Engineering Index Backfile | 1964




    DESIGN FOR INCREASED RELIABILITY OF AIRCRAFT HYDRAULIC SYSTEMS

    CHATTLER, LEO MORSE | SAE Technical Papers | 1953