Patent · US Active

System and method for measuring fatigue for mechanical components of an aircraft and aircraft maintenance method

US8600611B2 · kind B2 · utility

87Cited by
14References
12Claims
0Family size

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Inventor

Key dates

Filing dateNov 15, 2010
Grant dateDec 3, 2013
Priority date
Expiry dateNov 15, 2030

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG07C5/006
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

A system for measuring fatigue of a component of an aircraft subject to mechanical stresses includes: a plurality of stress sensors mounted on the component, each sensor being configured to detect a predetermined mechanical stress threshold and to deliver a data signal representative of exceeding of the threshold; and a mechanism for recording the data and the sensors configured to detect different stress thresholds so as to make it possible to calculate, on the basis of the data recorded by the system, an estimation of fatigue of the component due to the mechanical stresses. It is thus possible to optimize overhaul of the components.

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