Patent · US Active

Assisted take-off method for aircraft

US8014910B2 · kind B2 · utility

11Cited by
11References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 4, 2006
Grant dateSep 6, 2011
Priority date
Expiry dateJan 6, 2029

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/0661
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A reference value is arbitrarily selected from a range of possible aircraft rotation speeds. A position of a trimmable horizontal stabilizer is angled in accordance with a centering of the reference value. A deviation between the reference value and an accelerating speed value of the aircraft is determined. Elevators or the horizontal stabilizer are controlled, prior to rotation, in accordance with the determined deviation.

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