Vorder- und Hinterkantenvorrichtungswinkeln während des Sinkfluges eines Flugzeuges

Details

Veröffentlichungs-Nr.

EP2851289

Aktenzeichen

EP14186027

Anmeldetag

23. September 2014

Veröffentlichung

9. Mai 2018

Erteilung

9. Mai 2018

Rechtsraum

EP

IPC

B64C9/32B64C13/16B64C19/02G05D1/00G05D1/06

Abstract

A system (300) for increasing the descent rate of an aircraft may include a flight control computer(450), an edge control system (460), and a speedbrake control device (532). The flight control computer may be configured to compute a first setting for a leading edge device (150) and/or a trailing edge device (240) of an aircraft wing. The edge control system may be communicatively coupled to the flight control computer and may include an edge control device (453) having a plurality of control device positions (458) including a cruise position (462). The speedbrake control device may include a plurality of speedbrake detents (536) including a flight detent (542). The edge control system (460) may be configured to automatically command the leading edge device (150), the trailing edge device (240), or both, to a deflection angle corresponding to the first setting if the edge control device is in the cruise position and the speedbrake control device is in the flight detent.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete