The invention discloses a flight control method and system of an aircraft and an aircraft accelerator platform. The flight control method of the aircraft comprises the steps that the real-time position of a throttle lever on an active accelerator platform is obtained; judging whether the throttle lever exceeds an automatic working area of an active throttle table or not according to the real-time position; if yes, the stroke of the throttle lever exceeding the automatic working area is obtained; judging whether the travel reaches a preset TOGA * position or not; and if the TOGA * position is reached, activating a re-flight mode, otherwise, keeping the rotating speed and the thrust of the TOGA gear unchanged. According to the technical scheme, the technical problems that in the prior art, in the key stage of re-flight of an airplane, the operation burden and the mistaken touch risk of a pilot are increased, the step that the pilot needs to operate a throttle lever is increased, certain safety risks exist, and therefore the potential safety hazards of flight of the airplane and passengers are increased can be solved.
本发明公开了一种飞机的飞行控制方法、系统及飞机油门台,飞机的飞行控制方法包括:获取油门杆在主动式油门台的实时位置;根据所述实时位置判断所述油门杆是否超过主动式油门台的自动工作区域;若超过,则获取所述油门杆超过所述自动工作区域的行程;判断所述行程是否到达预设的TOGA*位置;若到达所述TOGA*位置,则激活复飞模式,否则保持TOGA档位的转速和推力不变。本发明所提供的技术方案能够解决现有技术中飞机在复飞的关键阶段,增加了飞行员的操作负担和误触风险,并增加了飞行员需要操作油门杆的步骤,存在一定的安全风险,从而增加飞机的飞行以及乘客安全隐患的技术问题。
Flight control method and system of aircraft and aircraft accelerator platform
一种飞机的飞行控制方法、系统及飞机油门台
2024-02-06
Patent
Elektronische Ressource
Chinesisch
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