A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
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 (author) / ZOU MENG (author) / ZHAO SHIHAO (author) / PENG HAIFENG (author) / FENG SHENGQUAN (author)
2024-02-06
Patent
Electronic Resource
Chinese
Inward opening type opening mechanism of airplane cabin door
| European Patent Office | 2024