Rotor blade shaft integrity monitoring system,申请号US19820388299-传众专利搜索

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发明名称	Rotor blade shaft integrity monitoring system
摘要	A helicopter rotor blade to hub arm attachment configured to react centrifugal loads from the blade through a blade cuff, spindle, and elastomeric bearings utilizes a bolt in the bore of the spindle for secondary load path operation and a spindle integrity monitoring indicator to provide a visual showing of a deviation from the normal load path.
申请公布号	US4439106(A)	申请公布日期	1984.03.27
申请号	US19820388299	申请日期	1982.06.14
申请人	UNITED TECHNOLOGIES CORPORATION	发明人	FERRIS, DONALD L.;OLSTER, ELLIOT F.;MARCHITTO, MICHAEL J.
分类号	B64C27/00;B64C27/48;B64D45/00;(IPC1-7):B64C27/48	主分类号	B64C27/00
代理机构		代理人
主权项
地址

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