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Passenger cabin door
The invention relates to a passenger cabin door, and belongs to the technical field of helicopters. The locking mechanism at least comprises a lockset system, the lockset system comprises a plurality of locksets, the locksets are arranged on the sliding door body and the corresponding door frame of the sliding door body, the lockpins in the locksets are linked, and therefore linkage locking or unlocking of the locksets is achieved; and the blocking mechanism is arranged in at least one lock and is used for blocking and limiting a lock pin in the corresponding lock. After the lock is unlocked, the lock pin is kept at the unlocking position through blocking and limiting of the lock pin, and in the sliding closing process of the passenger cabin door, blocking and limiting of the lock pin are cancelled to achieve the locking action. Therefore, the lock pin does not need to collide with other parts to achieve the locking action, the possibility of abrasion and damage of the lock pin can be effectively reduced, and the service life of the lock pin can be greatly prolonged.
本发明涉及一种客舱门,属于直升机技术领域,包括:滑动门体;以及锁闭机构,其中,所述锁闭机构至少包括锁具系统,所述锁具系统包括:多个锁具,设置在所述滑动门体上及对应的所述滑动门体的门框处,多个所述锁具内的所述锁销联动,从而实现多个所述锁具的联动锁闭或解锁;以及阻挡机构,设置在至少一个所述锁具内,用于对应所述锁具内锁销的阻挡限位。本发明在锁具解锁后通过对锁销的阻挡限位使其保持在解锁位置,在客舱门滑动关闭的过程中撤销对锁销的阻挡限位来实现锁闭动作。因此,无需锁销与其它部件进行撞击来实现锁闭动作,能够有效降低锁销的磨损和锁销损坏的可能性,从而能够大大提升锁销的使用寿命。
Passenger cabin door
The invention relates to a passenger cabin door, and belongs to the technical field of helicopters. The locking mechanism at least comprises a lockset system, the lockset system comprises a plurality of locksets, the locksets are arranged on the sliding door body and the corresponding door frame of the sliding door body, the lockpins in the locksets are linked, and therefore linkage locking or unlocking of the locksets is achieved; and the blocking mechanism is arranged in at least one lock and is used for blocking and limiting a lock pin in the corresponding lock. After the lock is unlocked, the lock pin is kept at the unlocking position through blocking and limiting of the lock pin, and in the sliding closing process of the passenger cabin door, blocking and limiting of the lock pin are cancelled to achieve the locking action. Therefore, the lock pin does not need to collide with other parts to achieve the locking action, the possibility of abrasion and damage of the lock pin can be effectively reduced, and the service life of the lock pin can be greatly prolonged.
本发明涉及一种客舱门,属于直升机技术领域,包括:滑动门体;以及锁闭机构,其中,所述锁闭机构至少包括锁具系统,所述锁具系统包括:多个锁具,设置在所述滑动门体上及对应的所述滑动门体的门框处,多个所述锁具内的所述锁销联动,从而实现多个所述锁具的联动锁闭或解锁;以及阻挡机构,设置在至少一个所述锁具内,用于对应所述锁具内锁销的阻挡限位。本发明在锁具解锁后通过对锁销的阻挡限位使其保持在解锁位置,在客舱门滑动关闭的过程中撤销对锁销的阻挡限位来实现锁闭动作。因此,无需锁销与其它部件进行撞击来实现锁闭动作,能够有效降低锁销的磨损和锁销损坏的可能性,从而能够大大提升锁销的使用寿命。
Passenger cabin door
客舱门
LEE SUNG HAENG (Autor:in) / XIE DAN (Autor:in) / HE DONGSHENG (Autor:in) / ZHENG HUAN (Autor:in) / DU HANG (Autor:in)
26.03.2024
Patent
Elektronische Ressource
Chinesisch
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