Invention Grant
- Patent Title: Method and device for detecting oscillatory failures in an automatic position control chain of an aircraft control surface
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Application No.: US15284989Application Date: 2016-10-04
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Publication No.: US10049511B2Publication Date: 2018-08-14
- Inventor: Philippe Goupil , Rémy Dayre , Simone Urbano
- Applicant: Airbus Operations SAS
- Applicant Address: FR Toulouse
- Assignee: AIRBUS OPERATIONS SAS
- Current Assignee: AIRBUS OPERATIONS SAS
- Current Assignee Address: FR Toulouse
- Agency: Greer, Burns & Crain, Ltd.
- Priority: FR1559755 20151014
- Main IPC: B64C23/02
- IPC: B64C23/02 ; G07C5/08 ; B64D45/00 ; G05B23/02 ; B64C13/50

Abstract:
A detection device comprising a first data processing unit configured to determine a first trend of the control surface control order as a function of time, the first trend being defined according to a reference parameter, a second data processing unit configured to determine at least one second trend of the control surface position value as a function of time, the second trend being also defined according to the reference parameter, and a monitoring unit configured to compare the first and second trends in order to verify the existence of a correlation between these first and second trends so as to detect an oscillatory failure as soon as a loss of correlation between the first and second trends appears, if necessary.
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Information query