发明名称 PROPELLER HUB AND BLADE CRACK DETECTION
摘要 <p>Propeller hubs and the hollow inner ends of propeller blades are filled or substantially filled with a liquid so that cracks in the hub wall or the blade wall leading from the interior to the exterior surface provide a pathway for the liquid to flow out to the exterior thereof, thus providing a visual indication of the presence of a crack prior to a catastrophic failure of the part. The liquid may be sealed in the blade or hub or may be carried within the hub as a lubricating fluid, partially or substantially filling the hub. The liquid may contain a dye to enhance visibility even of very small amounts which flow to the surface when the propeller is subjected to centrifugal force. Maintenance personnel and/or operators may then periodically inspect the exterior of the hub and/or blade to check for any evidence of the indicator liquid on the exterior surfaces or on the adjacent aircraft surfaces as a warning of possible incipient crack or fatigue failure.</p>
申请公布号 CA1078358(A) 申请公布日期 1980.05.27
申请号 CA19770270909 申请日期 1977.02.02
申请人 CESSNA AIRCRAFT COMPANY (THE) 发明人 VOISARD, WALTER B.
分类号 B64C11/00;(IPC1-7):64C11/38 主分类号 B64C11/00
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