Patent · US Active

Electric flight control system and method for an aircraft

US9315258B2 · kind B2 · utility

4Cited by
5References
12Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 9, 2014
Grant dateApr 19, 2016
Priority date
Expiry dateSep 17, 2034

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05D1/0833
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A flight control system includes at least one flight domain protection module intended at least for manual piloting and an auxiliary element configured to automatically transmit to the protection module, upon a detection of automatic piloting of the aircraft using an automatic piloting device, a predetermined auxiliary position, representing a control stick position equivalent, the protection module using the auxiliary position as a control stick position to implement a flight domain protection during the automatic piloting.

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