Initial examination of projected effects of increased fluid temperature on operational life of pumping equipment discloses life gap existing between present high temperature development and anticipated equipment life for SST; approach of centralized distribution is represented, i.e., hydraulic power generated by engine driven pumps and distributed to all required services through continuous tubing networks; composite system or power substation concept is based on tieing in intermittently scheduled loads and short duration peak power demands to other sources of power for driving pumps; recommendations made.


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    Title :

    New look at supersonic aircraft hydraulic requirements


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1963 Hydraulic equipment



    Publication date :

    1963


    Size :

    11 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    A NEW LOOK AT SUPERSONIC AIRCRAFT HYDRAULIC REQUIREMENTS

    Williams, R. E. | SAE Technical Papers | 1963


    Supersonic transport aircraft hydraulic systems

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




    Hydraulic Power Units for Supersonic Aircraft

    Lambeck, R. P. | SAE Technical Papers | 1967