SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN
Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving, via a fuel switch, a first control signal indicative of an off position on a fuel switch, determining a throttle resolver angle of a throttle controller in response t...
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | chi ; eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving, via a fuel switch, a first control signal indicative of an off position on a fuel switch, determining a throttle resolver angle of a throttle controller in response to the first control signal, comparing the throttle resolver angle to a threshold throttle angle, and generating a pilot warning in response to the first control signal and the throttle resolver angle exceeding the threshold throttle angle.
提供了飞行控制系统、飞行控制方法和飞机。一种飞机,包括系统和方法,用于经由燃料开关接收指示燃料开关上的关闭位置的第一控制信号;响应于第一控制信号,确定油门控制器的油门解算器角度;将油门解算器角度与阈值油门角度进行比较;以及响应于第一控制信号以及油门解算器角度超过阈值油门角度,生成飞行员警告。 |
---|