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


    Author / Creator :

    Type of media :

    Conference paper


    Type of material :

    Print



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