Two categories of controls advanced, one for system restricted to initiation during landing roll, other for initiation during flight; actuation system under development in relation to these requirements; its power transmission system is composed of variable displacement hydraulic pump designed as engine component; system believed to be adaptable to number of reverser systems, missions, and aircraft types. (see also abstract in SAE -- J n 7 v 66 July 1958 p 38-9)


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    Title :

    Control systems for thrust reversal


    Additional title:

    Soc Automotive Engrs -- Paper


    Contributors:
    Burnett, J. (author) / Moses, D. (author)

    Conference:

    SAE Meeting ; 1958 Reverse thrust



    Publication date :

    1958


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    CONTROL SYSTEMS FOR THRUST REVERSAL

    MOSES, DONALD / BURNETT, JOHN | SAE Technical Papers | 1958


    Control systems for thrust reversal

    Burnett, J. / Moses, D. | Engineering Index Backfile | 1958


    Thrust Reversal System

    J. P. Mertens | NTIS | 1965


    Thrust reversal for jet aircraft

    Colley, R.H. | Engineering Index Backfile | 1959


    Technical aspects of thrust reversal

    Curiel, G. | Engineering Index Backfile | 1954