Project planning data for a rotor and control system procurement and testing program for modifications to the XV-15 tilt-rotor research demonstrator aircraft is presented. The design, fabrication, and installation of advanced composite blades compatible with the existing hub, an advanced composite hub, and a nonmechanical control system are required.


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    Title :

    Preliminary Design Study of Advanced Composite Blade and Hub and Nonmechanical Control System for the Tilt-Rotor Aircraft. Volume 2: Project Planning Data


    Publication date :

    1980


    Size :

    65 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English