Patent · US Active

Assembly and method for on-wing thrust measurement of aircraft engines

US11067461B2 · kind B2 · utility

0Cited by
2References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 7, 2017
Grant dateJul 20, 2021
Priority date
Expiry dateApr 3, 2038

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01L25/00
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

A method determines a thrust force of an aircraft engine that is attached to an aircraft by a force transferring element having a strain gauge for determining its strain state and a temperature sensor for measuring a surface temperature of the force transferring element adjacent to the strain gauge. The method includes: determining the surface temperature; determining a strain of the force transferring element; determining the strain state of the force transferring element based on the determined strain and compensating for temperature effects by taking into account the surface temperature, the compensation of the temperature effects taking into account both static and transient influences; and calculating the thrust force of the aircraft engine from the determined strain state.

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