Patent · US Active

Method and device for detecting oscillatory failures in an automatic position control chain of an aircraft control surface

US10049511B2 · kind B2 · utility

1Cited by
1References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 4, 2016
Grant dateAug 14, 2018
Priority date
Expiry dateDec 17, 2036

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05B23/0235
  • WIPO fieldControl
  • WIPO sectorInstruments

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.