Patent · US Active

Irregularity detection in a structure of an aircraft

US8896329B2 · kind B2 · utility

0Cited by
6References
4Claims
0Family size

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Key dates

Filing dateMay 26, 2009
Grant dateNov 25, 2014
Priority date
Expiry dateMay 29, 2031

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01M5/0091
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

A device, a system and a method for detecting an irregularity in a structure of an aircraft are proposed. The device includes a resonant circuit with a resonance frequency and a probe for tuning the resonance frequency of the resonant circuit. The resonant circuit and the probe are operatively connected in such a way that the probe changes the resonance frequency of the resonant circuit if the structure changes due to a formation of an irregularity.

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