The mechanical timer or clock provides control functions according to elapsed time while a high-speed aircraft, missile, or artillery shell, travels between two points in its flight or trajectory. The escapement assembly is of the type having a rotary escapement wheel and a pivoted escapement lever with oscillating masses and two bladed escapement pallets, arranged in balanced relation about the pivot axis of an operating arbor, in a generally conventional manner, to control the step-bystep rotary movement of the escapement wheel. The latter is connected through a gear train with the controlled mechanism and the driving spring or other energy source for the escapement mechanism and timer.


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    Titel :

    Timing Escapement Mechanism


    Beteiligte:
    D. Popovitch (Autor:in)

    Erscheinungsdatum :

    1965


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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