System und Verfahren zur Pilot-In-Control-Steuerung in einem Drehflügelflugzeug

Details

Veröffentlichungs-Nr.

EP3489134

Aktenzeichen

EP18183759

Anmeldetag

16. Juli 2018

Veröffentlichung

13. Mai 2020

Erteilung

13. Mai 2020

Rechtsraum

EP

IPC

B64C13/10B64C27/56B64C13/50

Abstract

A rotorcraft (101) including a control element, a control sensor connected to the control element, where the control sensor is operable to generate trim data indicating a displacement of the control element in relation to a trim position of the control element, and a flight control computer (FCC) operable to monitor the trim data and determine an active detent state of the control element. The active detent state is one of an in-detent state (803), an out-of-detent state (813), and an in-transition state (807). The FCC is operable to buffer a transition of the active detent state from the in-detent state (803) to the out-of-detent state (813) using the in-transition state (807). The FCC provides a first flight management function when the active detent state is the in-detent state or the in-transition state, and provides a second flight management function when the active detent state is the out-of-detent state.

Anmelder

Firma

Bell Helicopter Textron Inc.

Land

🇺🇸 USA

Fachgebiete