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    • 8. 发明申请
    • INTEGRATED BEARING ASSEMBLIES FOR GUIDED ATTACK ROCKETS
    • 集成轴承组件用于引导攻击轴
    • US20160010685A1
    • 2016-01-14
    • US14468677
    • 2014-08-26
    • ROLLER BEARING COMPANY OF AMERICA, INC.
    • Alex Habibvand
    • F16C25/06F42B15/01F16C19/54
    • F16C25/06F16C19/163F16C19/548F16C2226/60F16C2240/14F42B15/01F42B15/36
    • A guide mechanism, configured for use with a guided attack rocket, includes an inner housing partially disposed in an outer housing. The inner and outer housings each define a forward end and an aft end. A first angular contact bearing is positioned between the outer housing forward end and the inner housing forward end. A second angular contact bearing is positioned between the outer housing aft end and the inner housing aft end. A retaining nut is received over the inner housing forward end. The retaining nut preloads the first and second angular contact bearings. Each of the angular contact bearings includes an inner member disposed within an outer member. The outer member defines an outer raceway and the inner member defines an inner raceway. A plurality of rolling elements is disposed between the outer raceway and the inner raceway.
    • 构造成与引导式攻击火箭一起使用的引导机构包括部分地设置在外壳中的内壳。 内壳体和外壳体每个限定前端和后端。 第一角接触轴承定位在外壳前端和内壳前端之间。 第二角接触轴承位于外壳体后端和内壳体后端之间。 保持螺母容纳在内壳前端上。 保持螺母预加载第一和第二角接触轴承。 每个角接触轴承包括设置在外部构件内部的内部构件。 外部构件限定外部滚道,并且内部构件限定内部滚道。 多个滚动元件设置在外滚道和内滚道之间。