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    • 3. 发明申请
    • Missile launcher
    • 导弹发射器
    • US20090188382A1
    • 2009-07-30
    • US11802030
    • 2007-05-18
    • Emanuel Hallgren
    • Emanuel Hallgren
    • F41F3/04
    • F41F3/052
    • A missile launcher comprising a forward support (501) for supporting a forward portion of a missile, and an aft support (505) for supporting an aft portion of the missile where the forward support (501) is arranged to swing clear of the aft portion of the missile during the initial period of its launching run where the forward support comprises a roll member (501) being in the shape of a segment of a circle and pivoted at the circle centre, where the perimeter of said member (501) is arranged to make frictional contact to the missile fuselage in order to confer mechanical energy to the roll member (501) to make said member to swing clear of the aft portion of the missile during the initial period of said missiles launching run.
    • 一种导弹发射器,包括用于支撑导弹的前部的前部支撑件(501)和用于支撑导弹的后部的后部支撑件(505),其中所述前部支撑件(501)布置成摆动离开所述后部部分 的导弹在其发射运行的初始阶段期间,其中前部支撑件包括卷状构件(501),该滚动构件(501)呈圆形的形状并且在圆心处枢转,所述构件(501)的周边布置 以使所述导弹机身摩擦接触,以便向所述滚动部件(501)赋予机械能,以使所述部件在所述导弹发射运行的初始阶段期间远离所述导弹的后部摆动。