This project involved the detailed design of the aft fuselage and empennage structure, vertical stabilizer, rudder, horizontal stabilizer, and elevator for the Triton primary flight trainer. The main design goals under consideration were to illustrate the integration of the control systems devices used in the tail surfaces and their necessary structural supports as well as the elevator trim, navigational lighting system, electrical systems, tail-located ground tie, and fuselage/cabin interface structure. Accommodations for maintenance, lubrication, adjustment, and repairability were devised. Weight, fabrication, and (sub)assembly goals were addressed. All designs were in accordance with the FAR Part 23 stipulations for a normal category aircraft.


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    Titel :

    Aircraft Empennage Structural Detail Design


    Beteiligte:
    G. Meholic (Autor:in) / R. Brown (Autor:in) / M. Hall (Autor:in) / R. Harvey (Autor:in) / M. Singer (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    74 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Aircraft Empennage Structural Detail Design

    D. Lesnewski / R. M. Snow / L. M. Combs et al. | NTIS | 1993


    Aircraft empennage structural detail design

    Meholic, Greg / Brown, Rhonda / Hall, Melissa et al. | NTRS | 1993


    Aircraft empennage structural detail design

    Lesnewski, David / Snow, Russ M. / Combs, Lisa M. et al. | NTRS | 1993


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