Patent · US Active

Capacitance based wear indicator

US10731506B2 · kind B2 · utility

2Cited by
11References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateDec 19, 2017
Grant dateAug 4, 2020
Priority date
Expiry dateApr 25, 2038

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF05D2260/83
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

A wear indicator for detecting blade clearance in a gas turbine engine includes a capacitor connected to a first conductor and a second conductor. The capacitor includes a multiple of layers arranged transverse to a rub direction, each layer separated by an insulator and including a first plate, a second plate, and a dielectric between the first plate and the second plate. A method of detecting blade clearance in a gas turbine engine, includes determining a change in capacitance between the first and second capacitance and determining an amount of material removed from the wear indicator by the blade corresponding to the change in capacitance.

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