发明名称 NSMS flight laser detector system
摘要 A method includes rotating a rotor, measuring a rotor rotational time for the rotor to complete a revolution, determining a blade interval by dividing the rotor rotational time by a number of blades carried on the rotor, establishing an active hold-off time interval as a percentage of the blade interval time, directing a beam of light at the blades of the rotor using a laser, sensing light reflected from the blades, generating an output signal as a function of the sensed light, establishing a signal amplitude threshold, analyzing an amplitude of the output signal to trigger the active hold-off time interval when the amplitude reaches the signal amplitude threshold, and generating a blade arrival signal as a function of triggered active hold-off time intervals. The output signal is not analyzed within each active hold-off time interval.
申请公布号 US7984656(B2) 申请公布日期 2011.07.26
申请号 US20080220368 申请日期 2008.07.24
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 NICKLOUS ALLISON CLARK;DREGER EDWARD F.;CASWELL WILLIAM F.
分类号 G01L1/24 主分类号 G01L1/24
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