发明名称 ROTARY WING AIRCRAFT INSTRUMENTED MOTION CONTROL BEARINGS
摘要 Motion control bearings and methods making such with the capability to monitor properties therein is provided. Devices and methods for creating and using motion control bearings for rotary wing aircraft in particular are disclosed using wireless communication and monitoring of multiple load, motion and health related information items related to the bearing and blade at the wing hub. Static and dynamic blade orientation provides additional information on flight regime, thrust vectors, and gross vehicle weight. Power is provided using kinetic energy power harvesting.
申请公布号 WO2012138816(A2) 申请公布日期 2012.10.11
申请号 WO2012US32249 申请日期 2012.04.05
申请人 ALLRED, CHARLES;DOWNING, MARSHALL;FUHRER, ZACHARY;JOLLY, MARK;SMITH, MATTHEW;LORD CORPORATION 发明人 ALLRED, CHARLES;DOWNING, MARSHALL;FUHRER, ZACHARY;JOLLY, MARK;SMITH, MATTHEW
分类号 F16C27/06;B23P17/00 主分类号 F16C27/06
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