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...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MARTIN ANDREW, RUHAN DESMOND, ZIOLKOWSKI CRAIG, ABLER TODD
Format: Patent
Sprache:chi ; eng
Schlagworte:
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Beschreibung
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。