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Inward opening type helicopter cabin door control device and method
The invention provides an inward-opening type helicopter cabin door control method. The inward-opening type helicopter cabin door control method comprises the steps that a first closing signal is sent to a controller unit; the controller unit receives the first closing signal and judges the state of the cabin door; if the cabin door is in the opening and locking state, the locking actuation system opens an'opening position lock ', generates a feedback signal and sends the feedback signal to the controller unit; the controller unit receives the feedback signal, generates a second closing signal and sends the second closing signal to the cabin door actuating system; the cabin door actuating system receives the second closing signal, starts to close the cabin door and enables the cabin door to move to a closing position, and the cabin door locking system generates an in-place signal and feeds back the in-place signal to the controller unit; the controller unit receives the in-place signal, generates a third closing signal and sends the third closing signal to the locking actuation system, and the locking actuation system closes the'closing position lock 'and generates a locking signal.
本申请提供了一种内开式直升机舱门控制方法,包括:发送第一关闭信号给控制器单元;控制器单元接收第一关闭信号,判断舱门的状态;若舱门处于打开锁定状态,锁闭作动系统打开“打开位置锁”,并生成反馈信号发送给控制器单元;控制器单元接收所述反馈信号,生成第二关闭信号,发送第二关闭信号给舱门作动系统;舱门作动系统接收到所述第二关闭信号,开始关闭舱门,并使舱门运动到关闭位置,舱门锁闭系统生成到位信号反馈给控制器单元;控制器单元接收到所述到位信号,生成第三关闭信号发送给锁闭作动系统,所述锁闭作动系统关闭“关闭位置锁”,并生成锁定信号。
Inward opening type helicopter cabin door control device and method
The invention provides an inward-opening type helicopter cabin door control method. The inward-opening type helicopter cabin door control method comprises the steps that a first closing signal is sent to a controller unit; the controller unit receives the first closing signal and judges the state of the cabin door; if the cabin door is in the opening and locking state, the locking actuation system opens an'opening position lock ', generates a feedback signal and sends the feedback signal to the controller unit; the controller unit receives the feedback signal, generates a second closing signal and sends the second closing signal to the cabin door actuating system; the cabin door actuating system receives the second closing signal, starts to close the cabin door and enables the cabin door to move to a closing position, and the cabin door locking system generates an in-place signal and feeds back the in-place signal to the controller unit; the controller unit receives the in-place signal, generates a third closing signal and sends the third closing signal to the locking actuation system, and the locking actuation system closes the'closing position lock 'and generates a locking signal.
本申请提供了一种内开式直升机舱门控制方法,包括:发送第一关闭信号给控制器单元;控制器单元接收第一关闭信号,判断舱门的状态;若舱门处于打开锁定状态,锁闭作动系统打开“打开位置锁”,并生成反馈信号发送给控制器单元;控制器单元接收所述反馈信号,生成第二关闭信号,发送第二关闭信号给舱门作动系统;舱门作动系统接收到所述第二关闭信号,开始关闭舱门,并使舱门运动到关闭位置,舱门锁闭系统生成到位信号反馈给控制器单元;控制器单元接收到所述到位信号,生成第三关闭信号发送给锁闭作动系统,所述锁闭作动系统关闭“关闭位置锁”,并生成锁定信号。
Inward opening type helicopter cabin door control device and method
一种内开式直升机舱门控制装置和方法
XI JIASHENG (Autor:in) / ZOU MENG (Autor:in) / ZHAO SHIHAO (Autor:in) / PENG HAIFENG (Autor:in) / FENG SHENGQUAN (Autor:in)
06.02.2024
Patent
Elektronische Ressource
Chinesisch
Inward opening type opening mechanism of airplane cabin door
Europäisches Patentamt | 2024
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