发明名称 Blade lock system for variable diameter rotor systems
摘要 A VDR blade lock system includes a set of blade pins that are rigidly mounted into the outboard blade section and a set of mount pins that are rigidly mounted to a rotor mount assembly. A resilient bushing at least partially surrounds each pin to provide high-energy absorption, impact resistance and low compressive modules. Should the outboard rotor blade section become free, centrifugal force will cause the outboard rotor blade section to rapidly telescope radially outward over the inboard blade section. The lock system prevents full extension of the outboard rotor blade section while the bushings act as a series of springs to reduce the deceleration rate of the outboard rotor blade section to minimize an impact force experienced by the VDR system.
申请公布号 US6398497(B1) 申请公布日期 2002.06.04
申请号 US20010788822 申请日期 2001.02.20
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 FEDERICI FRANCIS D.;BYRNES FRANCIS E.
分类号 B64C11/28;B64C27/473;B64C29/00;(IPC1-7):B64C11/28 主分类号 B64C11/28
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