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A platform for research: civil engineering, architecture and urbanism
Electromechanical integrated cargo hold door actuating system
The invention relates to a mechanical-electrical integration cargo hold door actuating system, and belongs to the field of mechanical transmission. Comprising a linear actuator, a control panel, a transmission flexible shaft and an electric tool. Wherein the linear actuator is mounted between an aircraft cargo hold door and a fuselage structure to open and close the cargo hold door; the control panel is installed on an aircraft skin structure and used for controlling the linear actuator to open and close the cargo hold door and displaying relevant state information of the cargo hold door. The linear actuator and the control panel are connected through a transmission flexible shaft, and transmission of mechanical force between the linear actuator and the control panel is achieved. During power failure, the transmission flexible shaft is manually driven through an electric tool, and the linear actuator is driven to open and close the cargo hold door; the linear actuator comprises a control driver and an electromechanical actuator; relevant state information of the cargo hold door is fed back to the control panel by controlling the driver; the electromechanical actuator is connected with the control panel through a transmission flexible shaft; electric or manual control over opening and closing of the cargo hold door is achieved.
本发明涉及一种机电一体化货舱门作动系统，属于机械传动领域；包括线性作动器、控制面板、传动软轴和电动工具；其中，线性作动器安装在飞机货舱门和机身结构之间，实现开启和关闭货舱门；控制面板安装在飞机蒙皮结构上，用于操控线性作动器开启和关闭货舱门，并显示货舱门相关状态信息；线性作动器和控制面板通过传动软轴连接，实现线性作动器和控制面板之间机械力的传递；断电时，手动通过电动工具驱动传动软轴，带动线性作动器开启和关闭货舱门；线性作动器包括控制驱动器和机电作动器；通过控制驱动器实现将货舱门相关状态信息反馈至控制面板；机电作动器与控制面板通过传动软轴连接；本发明实现货舱门开关的电动或手动控制。
Electromechanical integrated cargo hold door actuating system
The invention relates to a mechanical-electrical integration cargo hold door actuating system, and belongs to the field of mechanical transmission. Comprising a linear actuator, a control panel, a transmission flexible shaft and an electric tool. Wherein the linear actuator is mounted between an aircraft cargo hold door and a fuselage structure to open and close the cargo hold door; the control panel is installed on an aircraft skin structure and used for controlling the linear actuator to open and close the cargo hold door and displaying relevant state information of the cargo hold door. The linear actuator and the control panel are connected through a transmission flexible shaft, and transmission of mechanical force between the linear actuator and the control panel is achieved. During power failure, the transmission flexible shaft is manually driven through an electric tool, and the linear actuator is driven to open and close the cargo hold door; the linear actuator comprises a control driver and an electromechanical actuator; relevant state information of the cargo hold door is fed back to the control panel by controlling the driver; the electromechanical actuator is connected with the control panel through a transmission flexible shaft; electric or manual control over opening and closing of the cargo hold door is achieved.
本发明涉及一种机电一体化货舱门作动系统，属于机械传动领域；包括线性作动器、控制面板、传动软轴和电动工具；其中，线性作动器安装在飞机货舱门和机身结构之间，实现开启和关闭货舱门；控制面板安装在飞机蒙皮结构上，用于操控线性作动器开启和关闭货舱门，并显示货舱门相关状态信息；线性作动器和控制面板通过传动软轴连接，实现线性作动器和控制面板之间机械力的传递；断电时，手动通过电动工具驱动传动软轴，带动线性作动器开启和关闭货舱门；线性作动器包括控制驱动器和机电作动器；通过控制驱动器实现将货舱门相关状态信息反馈至控制面板；机电作动器与控制面板通过传动软轴连接；本发明实现货舱门开关的电动或手动控制。
Electromechanical integrated cargo hold door actuating system
一种机电一体化货舱门作动系统
NIE ZHENJIN (author) / GUO PENG (author) / WU HAO (author) / WANG XIN (author) / WANG XIAOLU (author) / ZHAO SHOUJUN (author)
2024-02-02
Patent
Electronic Resource
Chinese
IPC:
E05F
DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION
,
Vorrichtungen zum Bewegen der Flügel in die Offen- oder Schließstellung
Electromechanical integrated passenger car cabin door actuating system
| European Patent Office | 2024