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公开(公告)号:US20160117869A1
公开(公告)日:2016-04-28
申请号:US14989900
申请日:2016-01-07
Applicant: THE BOEING COMPANY
Inventor: Kevin L. Swearingen , Bradley J. Mitchell , Jeanne C. Maggiore , Stephen Gregory Dame , David A. Followell , Dane Joe Grgas
CPC classification number: G06F17/00 , B64C25/505 , B64D45/00 , B64D2045/0085 , B64F5/60 , G01M17/04 , G07C5/008
Abstract: A method for health monitoring of a damper associated with a landing gear is described which includes receiving sensor data from a pressure transducer and an accelerometer and optionally a thermal sensor operably mounted on or near the damper, a computer system, and applying, using the computer system, a diagnostic algorithm to the sensor data to induce and predict the health of the damper.
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公开(公告)号:US10073811B2
公开(公告)日:2018-09-11
申请号:US14989900
申请日:2016-01-07
Applicant: THE BOEING COMPANY
Inventor: Kevin L. Swearingen , Bradley J. Mitchell , Jeanne C. Maggiore , Stephen Gregory Dame , David A. Followell , Dane Joe Grgas
CPC classification number: G06F17/00 , B64C25/505 , B64D45/00 , B64D2045/0085 , B64F5/60 , G01M17/04 , G07C5/008
Abstract: A method for health monitoring of a damper associated with a landing gear is described which includes receiving sensor data from a pressure transducer and an accelerometer and optionally a thermal sensor operably mounted on or near the damper, a computer system, and applying, using the computer system, a diagnostic algorithm to the sensor data to induce and predict the health of the damper.
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