Herein provided are methods and systems for a method for controlling autothrottle of an engine. A digital power request is obtained from an autothrottle controller, the digital power request based onan autothrottle input to the autothrottle controller. A manual input mode for the engine is terminated, the manual input mode based on a second power request obtained from a manual input associated with the engine. An autothrottle mode for the engine is engaged to control the engine based on the digital power request.

    本文中提供了用于控制发动机的自动油门的方法的方法和系统。从自动油门控制器获得数字功率请求,该数字功率请求是基于至自动油门控制器的自动油门输入。终止发动机的手动输入模式,该手动输入模式是基于从与发动机相关联的手动输入获得的第二功率请求。启用发动机的自动油门模式以基于数字功率请求来控制发动机。


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    Title :

    Autothrottle control system on turbopropeller-powered aircraft


    Additional title:

    以涡轮螺旋桨为动力的飞行器上的自动油门控制系统


    Contributors:

    Publication date :

    2020-05-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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