发明名称 Cable for detecting a misalignment of adjacent airfoils
摘要 <p>The present invention relates to an apparatus (10) for detecting and signaling a misalignment of adjacent auxiliary airfoil elements comprising a cable (12) that is guided through the airfoil elements (1-6) and means for detecting an excessive movement of the cable and generating an error signal in response thereto. The apparatus further comprises a spring system (58) consisting of dual concentric compression springs attached to the cable for tensioning thereof. The means for detecting an excessive movement of the cable comprises a proximity sensor system attached to a housing of the spring system. The apparatus also comprises a latch means for locking the spring system with respect to the housing when a predetermined cable loading is reached. automatically moves the spring system away from said proximity sensor system (26) and locks said spring system against movement. &lt;IMAGE&gt;</p>
申请公布号 EP0726201(A1) 申请公布日期 1996.08.14
申请号 EP19950202998 申请日期 1995.11.06
申请人 THE BOEING COMPANY 发明人 CAFERRO, JOSEPH S.;TOMASSI, HECTOR V.
分类号 B64C9/02;B64D45/00;(IPC1-7):B64D45/00 主分类号 B64C9/02
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