发明名称 Aircraft structural fatigue monitor
摘要 The present invention is a system for monitoring, storing, and reporting the accumulation of fatigue occurrences experienced by an aircraft. The system according to the present invention uses existing aircraft instrumentation to monitor fatigue occurrences. Data is collected on the magnitude and cycles of any turbulence encounters; magnitude and number of gloading accrued by aircraft maneuvering; the number of pressurization cycles that the aircraft has experienced; and the number of takeoffs/landing cycles that have occurred. These data are stored in electronic memory for later review by the flight crew or maintenance personnel. Additionally, the number of accumulated wing flap cycles and landing extensions/retractions may also be monitored to facilitate the maintenance operations of these two critical flight controls.
申请公布号 US6289289(B1) 申请公布日期 2001.09.11
申请号 US19980209169 申请日期 1998.12.10
申请人 HONEYWELL INTERNATIONAL INC. 发明人 ZWEIFEL TERRY L.
分类号 B64F5/00;G01M5/00;G07C3/00;(IPC1-7):G06F19/00;G08B23/00 主分类号 B64F5/00
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