The invention belongs to the technical field of electromechanical management, and relates to a helicopter fuel transfer control method. The method comprises the following steps: when a transfer pump switch acquired by an electromechanical management computer is in an on state and a transfer direction input by a user through an electromechanical parameter display is not received, determining that a condition for entering automatic transfer control is already met at present; when 1-3 fuel quantities meet the automatic transfer requirement, entering an automatic transfer state, and controlling the transfer direction to be converted according to an automatic transfer control flow; in the automatic transmission state, receiving an automatic transmission stopping instruction input by a user through the electromechanical parameter display; according to the instruction of stopping automatic transmission, exiting the automatic transmission state, and determining that the condition of entering manual transmission control is already met at present; and receiving the transmission direction input by the user through the electromechanical parameter display, entering a manual transmission state, responding to the operation of the user on the manual transmission interface, and converting the transmission direction.
本发明属于机电管理技术领域,涉及一种直升机燃油转输控制方法。方法包括:当机电管理计算机采集的转输泵开关为接通状态,且未接收到用户通过机电参数显示器输入的转输方向时,确定当前已具备了进入自动转输控制的条件;当1‑3发燃油量满足自动转输要求时,进入自动转输状态,按照自动转输控制流程控制转输方向发生转换;在自动转输状态时,接收用户通过机电参数显示器输入的“停止自动转输”指令;根据“停止自动转输”指令,退出自动转输状态,确定当前已具备了进入手动转输控制的条件;接收用户通过机电参数显示器输入的转输方向,进入手动转输状态,响应用户在手动转输界面的操作,转换转输方向。
Helicopter fuel transfer control method
一种直升机燃油转输控制方法
2023-03-07
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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