A platform for research: civil engineering, architecture and urbanism
A platform for research: civil engineering, architecture and urbanism
Cabin door locking device, aircraft or spacecraft cabin door and aircraft or spacecraft
The invention provides a cabin door locking device, an aircraft or spacecraft cabin door and an aircraft or spacecraft. In one aspect, a door locking device for an aircraft or spacecraft door is described, the door locking device comprising: a drivable spindle drive extending along a longitudinal axis and fixed along the longitudinal axis relative to a door frame of the aircraft or spacecraft door; at least one locking bolt driven by the drivable spindle drive and guided along a longitudinal axis; and at least one adjustment bushing assembly mounted on the fuselage frame and comprising a first eccentric bushing having a bolt receptacle centrally oriented along the longitudinal axis for receiving at least one locking bolt, the cabin door locking device can form a shape matching locking connection on two shafts which are perpendicular to the longitudinal axis.
本发明提供一种舱门锁定装置、飞行器或航天器舱门以及飞行器或航天器。在一个方面中，描述了一种用于飞行器或航天器舱门的舱门锁定装置，舱门锁定装置包括：可驱动主轴驱动器，其沿着纵向轴线延伸并且沿着纵向轴线相对于飞行器或航天器舱门的舱门框架固定；至少一个锁定螺栓，其由可驱动主轴驱动器驱动并且沿着纵向轴线被导引；以及至少一个调节衬套组件，其安装在机身框架上并且包括第一偏心衬套，该第一偏心衬套具有沿着纵向轴线居中地定向的螺栓接纳部，以用于接纳至少一个锁定螺栓，使得舱门锁定装置能够在均与纵向轴线垂直的两个轴上形成形状配合锁定连接。
Cabin door locking device, aircraft or spacecraft cabin door and aircraft or spacecraft
The invention provides a cabin door locking device, an aircraft or spacecraft cabin door and an aircraft or spacecraft. In one aspect, a door locking device for an aircraft or spacecraft door is described, the door locking device comprising: a drivable spindle drive extending along a longitudinal axis and fixed along the longitudinal axis relative to a door frame of the aircraft or spacecraft door; at least one locking bolt driven by the drivable spindle drive and guided along a longitudinal axis; and at least one adjustment bushing assembly mounted on the fuselage frame and comprising a first eccentric bushing having a bolt receptacle centrally oriented along the longitudinal axis for receiving at least one locking bolt, the cabin door locking device can form a shape matching locking connection on two shafts which are perpendicular to the longitudinal axis.
本发明提供一种舱门锁定装置、飞行器或航天器舱门以及飞行器或航天器。在一个方面中，描述了一种用于飞行器或航天器舱门的舱门锁定装置，舱门锁定装置包括：可驱动主轴驱动器，其沿着纵向轴线延伸并且沿着纵向轴线相对于飞行器或航天器舱门的舱门框架固定；至少一个锁定螺栓，其由可驱动主轴驱动器驱动并且沿着纵向轴线被导引；以及至少一个调节衬套组件，其安装在机身框架上并且包括第一偏心衬套，该第一偏心衬套具有沿着纵向轴线居中地定向的螺栓接纳部，以用于接纳至少一个锁定螺栓，使得舱门锁定装置能够在均与纵向轴线垂直的两个轴上形成形状配合锁定连接。
Cabin door locking device, aircraft or spacecraft cabin door and aircraft or spacecraft
舱门锁定装置、飞行器或航天器舱门以及飞行器或航天器
OHLER SU REN (author)
2024-06-21
Patent
Electronic Resource
Chinese
IPC:
E05B
LOCKS
,
Schlösser