Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Interior hinge arm of boarding gate of airplane
The invention discloses an aircraft boarding gate interior hinge arm which comprises a support, a connecting rod mechanism A, a connecting rod mechanism B and an adjusting rotary sleeve, one end of the connecting rod mechanism B is telescopically connected with the adjusting rotary sleeve, the other end of the connecting rod mechanism B is provided with the support rotationally connected with the connecting rod mechanism B, and one end of the connecting rod mechanism A is arranged in the adjusting rotary sleeve and movably connected with the adjusting rotary sleeve. One support is installed on an interior trim, the other support is installed on a door, the length between the connecting rod mechanism B and the adjusting rotary sleeve is adjusted according to the installation space, when the door is opened, the connecting rod mechanism A and the adjusting rotary sleeve are separated, when the door is loosened, the connecting rod mechanism A restores to the original position, and when the door is opened, the connecting rod mechanism B restores to the original position. By arranging the connecting rod mechanism A and the connecting rod mechanism B, the length of the hinge arm can be adjusted and the hinge arm can be rebounded and reset by adjusting the rotating sleeve, so that the hinge arm has an automatic reset function, and the use scene of the hinge arm is improved.
本发明公开了一种飞机登机门内饰铰链臂，包括支架、连杆机构A、连杆机构B、调节旋转套，所述连杆机构B一端和所述调节旋转套可伸缩连接，另一端设有和其转动连接的所述支架，所述连杆机构A一端设于所述调节旋转套内和其活动连接，另一端设有和其转动连接的所述支架，将一个所述支架安装于内饰上，另一个安装于门上，根据安装空间调节所述连杆机构B和所述调节旋转套之间的长度，打开门时，所述连杆机构A和所述调节旋转套分离，松开门时，所述连杆机构A恢复原位，通过设置连杆机构A、连杆机构B、调节旋转套使铰链臂能调节长度且能回弹复位，使其具有自动复位功能，提升了铰链臂使用场景。
Interior hinge arm of boarding gate of airplane
The invention discloses an aircraft boarding gate interior hinge arm which comprises a support, a connecting rod mechanism A, a connecting rod mechanism B and an adjusting rotary sleeve, one end of the connecting rod mechanism B is telescopically connected with the adjusting rotary sleeve, the other end of the connecting rod mechanism B is provided with the support rotationally connected with the connecting rod mechanism B, and one end of the connecting rod mechanism A is arranged in the adjusting rotary sleeve and movably connected with the adjusting rotary sleeve. One support is installed on an interior trim, the other support is installed on a door, the length between the connecting rod mechanism B and the adjusting rotary sleeve is adjusted according to the installation space, when the door is opened, the connecting rod mechanism A and the adjusting rotary sleeve are separated, when the door is loosened, the connecting rod mechanism A restores to the original position, and when the door is opened, the connecting rod mechanism B restores to the original position. By arranging the connecting rod mechanism A and the connecting rod mechanism B, the length of the hinge arm can be adjusted and the hinge arm can be rebounded and reset by adjusting the rotating sleeve, so that the hinge arm has an automatic reset function, and the use scene of the hinge arm is improved.
本发明公开了一种飞机登机门内饰铰链臂，包括支架、连杆机构A、连杆机构B、调节旋转套，所述连杆机构B一端和所述调节旋转套可伸缩连接，另一端设有和其转动连接的所述支架，所述连杆机构A一端设于所述调节旋转套内和其活动连接，另一端设有和其转动连接的所述支架，将一个所述支架安装于内饰上，另一个安装于门上，根据安装空间调节所述连杆机构B和所述调节旋转套之间的长度，打开门时，所述连杆机构A和所述调节旋转套分离，松开门时，所述连杆机构A恢复原位，通过设置连杆机构A、连杆机构B、调节旋转套使铰链臂能调节长度且能回弹复位，使其具有自动复位功能，提升了铰链臂使用场景。
Interior hinge arm of boarding gate of airplane
一种飞机登机门内饰铰链臂
FENG QINGXIAO (Autor:in) / MIAO PENG (Autor:in) / CAI LIN (Autor:in) / WANG LEI (Autor:in) / CHEN ZHE (Autor:in) / YIN YANJIAO (Autor:in)
23.01.2024
Patent
Elektronische Ressource
Chinesisch
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