Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Locking mechanism for rotary flight lock of hatch door
A locking mechanism for a flight lock for a hatch door, the flight lock being rotatable between a flight lock locking position and a flight lock unlocking position, the hatch door being provided with a handle shaft, the hatch door being opened by rotating a handle fixed at an end of the handle shaft in an opening direction, the locking mechanism comprising: a locking shaft mounted at the hatch door; the locking shaft rocker arm boss is provided with a protruding part and can be installed on the locking shaft in a relatively rotating mode. The first rocker arm is installed on the handle shaft in a relative rotation mode, the flight lock is connected to the locking shaft rocker arm boss in an operable mode, when the flight lock is located at the flight lock locking position, the locking shaft rocker arm boss is located at the locking shaft rocker arm boss locking position, the protruding part is contained in the concave part, and the first rocker arm is connected to the flight lock through the locking shaft rocker arm boss locking position. When the flight lock is located at the flight lock locking position, the handle is rotated in the opening direction so that the surface of the concave part can abut against the protruding part. The invention further provides an aircraft comprising the locking mechanism.
一种用于舱门的飞行锁的锁定机构，该飞行锁能在飞行锁锁定位置与飞行锁解锁位置之间转动，舱门安装有手柄轴，沿开启方向转动固定在手柄轴的端部处的手柄能打开舱门，锁定机构包括：安装于舱门处的锁定轴；具有凸出部的锁定轴摇臂凸台，其能相对旋转地安装在锁定轴上；具有凹入部的第一摇臂，其不能相对旋转地安装在手柄轴上，飞行锁可操作地连接于锁定轴摇臂凸台，其中，在飞行锁处于飞行锁锁定位置时，锁定轴摇臂凸台处于锁定轴摇臂凸台锁定位置中，凸出部被接纳在凹入部中，且凸出部与凹入部的表面之间相距一间隙，在飞行锁处于飞行锁锁定位置时，沿开启方向转动手柄使得凹入部的表面抵靠凸出部。本发明还提出了一种包括前述锁定机构的飞机。
Locking mechanism for rotary flight lock of hatch door
A locking mechanism for a flight lock for a hatch door, the flight lock being rotatable between a flight lock locking position and a flight lock unlocking position, the hatch door being provided with a handle shaft, the hatch door being opened by rotating a handle fixed at an end of the handle shaft in an opening direction, the locking mechanism comprising: a locking shaft mounted at the hatch door; the locking shaft rocker arm boss is provided with a protruding part and can be installed on the locking shaft in a relatively rotating mode. The first rocker arm is installed on the handle shaft in a relative rotation mode, the flight lock is connected to the locking shaft rocker arm boss in an operable mode, when the flight lock is located at the flight lock locking position, the locking shaft rocker arm boss is located at the locking shaft rocker arm boss locking position, the protruding part is contained in the concave part, and the first rocker arm is connected to the flight lock through the locking shaft rocker arm boss locking position. When the flight lock is located at the flight lock locking position, the handle is rotated in the opening direction so that the surface of the concave part can abut against the protruding part. The invention further provides an aircraft comprising the locking mechanism.
一种用于舱门的飞行锁的锁定机构，该飞行锁能在飞行锁锁定位置与飞行锁解锁位置之间转动，舱门安装有手柄轴，沿开启方向转动固定在手柄轴的端部处的手柄能打开舱门，锁定机构包括：安装于舱门处的锁定轴；具有凸出部的锁定轴摇臂凸台，其能相对旋转地安装在锁定轴上；具有凹入部的第一摇臂，其不能相对旋转地安装在手柄轴上，飞行锁可操作地连接于锁定轴摇臂凸台，其中，在飞行锁处于飞行锁锁定位置时，锁定轴摇臂凸台处于锁定轴摇臂凸台锁定位置中，凸出部被接纳在凹入部中，且凸出部与凹入部的表面之间相距一间隙，在飞行锁处于飞行锁锁定位置时，沿开启方向转动手柄使得凹入部的表面抵靠凸出部。本发明还提出了一种包括前述锁定机构的飞机。
Locking mechanism for rotary flight lock of hatch door
用于舱门的旋转飞行锁的锁定机构
JIANG CUNCUN (Autor:in) / ZHANG WENBIN (Autor:in) / YU JIANGCHENG (Autor:in) / CAI YUZHEN (Autor:in) / TENG QING (Autor:in) / DING HONGFEI (Autor:in)
21.07.2023
Patent
Elektronische Ressource
Chinesisch