发明名称 IN SITU FLAP AND SLAT WING TIP BRAKE RESPONSE TESTER
摘要 A method, apparatus and computer-readable medium for measuring a determining a validity of an estimate of a response time of a brake is disclosed. A sensor obtains a waveform of a parameter related to the engagement of the brake during engagement of the brake. A processor analyzes the obtained waveform, determines inflection points in the waveform within a selected time period, validates the signal integrity of the waveform and provides an indicator when the number of determined inflection points is greater than a pre-specified count value.
申请公布号 CA2844166(A1) 申请公布日期 2014.09.06
申请号 CA20142844166 申请日期 2014.02.26
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 KREIENHEDER, JASON B.
分类号 F16D66/00;B64C9/32;B64C13/24;B64F5/00 主分类号 F16D66/00
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