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Cabin door lock mechanism for intelligent low-altitude manned aircraft
The invention discloses a cabin door lock mechanism for an intelligent low-altitude manned aircraft, and relates to the field of intelligent low-altitude manned aircraft cabin door structural design.The cabin door lock mechanism comprises a first assembly arranged on the outer side of a cabin body and a second assembly arranged on the inner side of a cabin door; the first assembly comprises a first assembly support, a lock pin, a pull ring and a first reset spring, the lock pin is arranged in a guide hole of the first assembly support, the end of the lock pin is fixedly connected with the pull ring, and the first reset spring is arranged on the lock pin; the second assembly comprises a second assembly support, a lock hook, a hand plate, a transposition shaft and a second reset spring, thelock hook is connected with the second assembly support through the transposition shaft, the second reset spring is arranged on the transposition shaft, and the hand plate is arranged on the lock hook. The cabin door can be emergently opened and closed inside and outside the cabin, the environmental adaptability is high, external power sources such as electricity, gas and liquid are not needed, and the cabin door is convenient and reliable to open and close.
本发明公开了一种用于智能低空载人飞行器的舱门锁机构，涉及智能低空载人飞行器舱门结构设计领域，包括设置于舱体外侧的第一组件和设置于舱门内侧的第二组件；所述第一组件包括第一组件支座、锁销、拉环、第一复位弹簧，所述锁销设置于第一组件支座的导向孔中，所述锁销的端部与拉环固定连接，所述第一复位弹簧设置于锁销上；所述第二组件包括第二组件支座、锁钩、手板、转位轴和第二复位弹簧，所述锁钩通过转位轴与第二组件支座连接，所述第二复位弹簧设置于转位轴上，所述手板设置于锁钩上。本发明可在舱内和舱外紧急开、关舱门，环境适应性强，并且无需电、气、液等外部动力源，开关舱门操作方便、可靠。
Cabin door lock mechanism for intelligent low-altitude manned aircraft
The invention discloses a cabin door lock mechanism for an intelligent low-altitude manned aircraft, and relates to the field of intelligent low-altitude manned aircraft cabin door structural design.The cabin door lock mechanism comprises a first assembly arranged on the outer side of a cabin body and a second assembly arranged on the inner side of a cabin door; the first assembly comprises a first assembly support, a lock pin, a pull ring and a first reset spring, the lock pin is arranged in a guide hole of the first assembly support, the end of the lock pin is fixedly connected with the pull ring, and the first reset spring is arranged on the lock pin; the second assembly comprises a second assembly support, a lock hook, a hand plate, a transposition shaft and a second reset spring, thelock hook is connected with the second assembly support through the transposition shaft, the second reset spring is arranged on the transposition shaft, and the hand plate is arranged on the lock hook. The cabin door can be emergently opened and closed inside and outside the cabin, the environmental adaptability is high, external power sources such as electricity, gas and liquid are not needed, and the cabin door is convenient and reliable to open and close.
本发明公开了一种用于智能低空载人飞行器的舱门锁机构，涉及智能低空载人飞行器舱门结构设计领域，包括设置于舱体外侧的第一组件和设置于舱门内侧的第二组件；所述第一组件包括第一组件支座、锁销、拉环、第一复位弹簧，所述锁销设置于第一组件支座的导向孔中，所述锁销的端部与拉环固定连接，所述第一复位弹簧设置于锁销上；所述第二组件包括第二组件支座、锁钩、手板、转位轴和第二复位弹簧，所述锁钩通过转位轴与第二组件支座连接，所述第二复位弹簧设置于转位轴上，所述手板设置于锁钩上。本发明可在舱内和舱外紧急开、关舱门，环境适应性强，并且无需电、气、液等外部动力源，开关舱门操作方便、可靠。
Cabin door lock mechanism for intelligent low-altitude manned aircraft
一种用于智能低空载人飞行器的舱门锁机构
WANG XINLIN (author) / CAI JIANDONG (author) / XIE ANHUAN (author) / ZHANG DAN (author)
2021-02-09
Patent
Electronic Resource
Chinese
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