The patent application relates to a retractable nose landing gear for a high performance aircraft. It includes a structure which is pivoted into the fuselage of the aircraft and which positions the wheel mechanically relative to the landing gear structures to provide stowage of the wheel in a horizontal position directly behind the retracted landing gear structure. It provides a minimum of storage space in the aircraft while maximizing space for an engine air duct above the landing gear wheel well and helping to reduce aircraft frontal area. (Author)


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    Titel :

    Retractable Nose Landing Gear


    Beteiligte:

    Erscheinungsdatum :

    1979


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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