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    • 2. 发明申请
    • LOW COST DEPLOYMENT SYSTEM AND METHOD FOR AIRBORNE OBJECT
    • 低成本部署系统和空中客车对象的方法
    • WO2010129290A1
    • 2010-11-11
    • PCT/US2010/032594
    • 2010-04-27
    • RAYTHEON COMPANYGESWENDER, Chris, E.
    • GESWENDER, Chris, E.
    • F42B10/16F42B10/14
    • F42B10/14F42B10/16F42B10/50F42B10/54F42C15/23
    • A deployment system is provided for utilization onboard an airborne object including a deployable element (12). In one embodiment, the deployment system includes a circumferential restraint (34) and a release mechanism (32) mounted to the airborne object. The circumferential restraint (34) is disposed at least partially around the airborne object in a constraining position wherein the circumferential restraint (32) prevents deployment of the deployable element. The release mechanism normally resides in a first position in which the release mechanism maintains the circumferential restraint in the constraining position. The release mechanism (32) is movable to a second position to release the circumferential restraint (34) from the constraining position and permit deployment of the deployable element (12).
    • 提供了一种部署系统,用于在包括可部署元件(12)的机载对象上使用。 在一个实施例中,展开系统包括安装在机载物体上的圆周限制器(34)和释放机构(32)。 周向约束(34)至少部分地围绕机身物体设置在限制位置,其中周向约束(32)防止展开元件的展开。 释放机构通常位于第一位置,其中释放机构将周向约束保持在约束位置。 释放机构(32)可移动到第二位置以将周向约束(34)从限制位置释放并允许展开元件(12)的展开。