发明名称 ROTARY BLADE RETENTION SYSTEM
摘要 1530366 Securing propeller blades to hubs LORD CORP 15 July 1976 [18 July 1975] 29462/76 Heading B7V A propeller-blade retention system comprises a frictionless thrust bearing 34 and a laminated elastomeric thrust bearing 38 connected in series. The laminations of the elastomeric bearing are frusto conical and define an effective elastic centre which is located outboard of the thrust bearings. The thrust bearings are preloaded by means of a resilient pad 66 which frictionally engages the surface 64 of the hub 10 during static conditions to resist drooping. The pad moves away from the surface 64 during centrifugal loading.
申请公布号 GB1530366(A) 申请公布日期 1978.10.25
申请号 GB19760029462 申请日期 1976.07.15
申请人 LORD CORP 发明人
分类号 B64C11/06;B64C27/35;B64C27/48;(IPC1-7):64C11/06 主分类号 B64C11/06
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