Patent · US Active

Failure analysis system

US9540117B2 · kind B2 · utility

2Cited by
0References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 18, 2014
Grant dateJan 10, 2017
Priority date
Expiry dateMar 25, 2035

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05B2219/45071
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A failure analysis system for monitoring sub-system failures in an aircraft that comprises a plurality of sub-systems, the aircraft having a plurality of functions, wherein each function is available when one or more associated sub-systems is operating correctly. The failure analysis system comprising: a plurality of monitors for monitoring the status of one or more sub-systems of the aircraft and determining if a failure has occurred; a memory arranged to store a list of a plurality of flight phases or operating modes to be completed by the monitored system and data associating one or more of the functions with each flight phase or operating mode; and a processor in communication with the monitors and the memory and arranged to model the response of the sub-systems to a failure determined by the monitors to identify which functions required by the flight phases or operating modes are degraded or are not available.

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