The patent application relates to an invention that pertains to lifting and propulsion systems in vertical and short takeoff and landing type aircraft. More particularly, this invention pertains to such systems wherein the power source is a bypass turbofan engine and where remote lifting fans are powered by turbojet exhaust while bypass fan efflux is vectored to provide lift or thrust.


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    Title :

    Fan Lift-Cruise V/STOL Aircraft


    Contributors:

    Publication date :

    1976


    Size :

    13 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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    Review of V/STOL lift/cruise fan technology

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