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公开(公告)号：US4127201A
公开(公告)日：1978-11-28
申请号：US741978
申请日：1976-11-15
申请人： Emil Baumann
发明人： Emil Baumann
CPC分类号： B65G69/30 , B60P1/43 , B65G69/287
摘要： A collapsible loading and unloading ramp comprising two substantially parallel spaced longitudinal supports intended to be secured to a vehicle component, for instance a vehicle platform. Each of the longitudinal supports comprises a ramp portion which can be adjusted and locked in position with respect to the plane of the platform and an on-loading portion hingedly connected therewith. The ramp portion comprises three interconnected partial elements, the first partial element provided with a suspension means is hingedly, lockably secured at the second partial element and the second partial element together with the first partial element is secured to be laterally pivotable and fixable at the third partial element. Between both of the longitudinal supports, preferably however only at the region of the third partial element as well as at the on-loading portion, there are provided transverse supports arranged in spaced relationship from one another. The on-loading portion can be fixed in angled relationship to the ramp portion by means of a tension element, such as a chain which can be varied in length.
摘要翻译： 一种可折叠的装载和卸载斜坡，包括两个基本上平行的间隔开的纵向支撑件，用于固定到车辆部件，例如车辆平台。 每个纵向支撑件包括可相对于平台的平面调节和锁定在适当位置的斜坡部分和与其平行连接的上载部分。 斜坡部分包括三个互连的部分元件，设置有悬挂装置的第一部分元件被铰接地锁定地固定在第二部分元件处，并且第二部分元件与第一部分元件一起被固定成横向可枢转并可固定在第三部分元件 部分元素 在两个纵向支撑件之间，优选仅在第三部分元件的区域以及在装载部分处，设置有彼此间隔开的横向支撑件。 通过诸如可以在长度上变化的链条的张紧元件，上载部分可以以与斜面部分成角度的关系固定。
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公开(公告)号：US3946640A
公开(公告)日：1976-03-30
申请号：US418615
申请日：1973-11-23
申请人： Emil Baumann
发明人： Emil Baumann
摘要： A mobile anti-aircraft weapon incorporating a housing rotatable about a substantially vertical axis with respect to the chassis of a support vehicle. The housing is equipped with side doors which can be pivoted about hinges and a respective rocket launcher accommodating a plurality of rockets mounted at the outside of each side door and serving as weapons.
摘要翻译： 一种移动式防空武器，其包括相对于支撑车辆的底盘围绕基本垂直的轴线旋转的壳体。 该壳体配备有可围绕铰链枢转的侧门和容纳安装在每个侧门外侧并用作武器的多个火箭的相应火箭发射器。
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