Patent · US Active

Method and device for estimating the forces exerted on a control surface of an aircraft

US8165729B2 · kind B2 · utility

1Cited by
9References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 2, 2007
Grant dateApr 24, 2012
Priority date
Expiry dateFeb 22, 2031

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05B13/04
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

Disclosed is a method and device for estimating forces exerted on at least one aircraft control surface. The method includes steps of, and the device includes components that carry out steps that include: generating current aircraft flight data; determining, from the generated aircraft flight data, a value Bl based on current deflection data and geometrical characteristics of a lever arm actuator of the at least one aircraft control surface; calculating, from the determined value Bl, at least one hinge moment; summing each calculated hinge moment; and dividing the sum by the value Bl to obtain an estimate of the forces exerted on the least one aircraft control surface.

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