The invention belongs to the design technology of airplane cabin door structures, and particularly relates to a unit emergency parachuting cabin door and a mechanism thereof, the unit emergency parachuting cabin door is composed of a folding and unfolding mechanism, a door body structure, a lock mechanism, an electric switch mechanism and the like, the door body structure is fixed on a fuselage through the folding and unfolding mechanism, the lock mechanism locks the door body structure, and the electric switch mechanism is used for transmitting information of the door body structure. The air emergency evacuation device is installed on the lower portion of a cockpit, can be used for air emergency evacuation of crew crew under special conditions, and has the advantages of being large in opening envelope, good in reliability and high in personnel off-aircraft safety.
本申请属于飞机舱门结构机构设计技术,特别涉及一种机组应急跳伞舱门及其机构,由收放机构、门体结构、锁机构、电门机构等组成,门体结构由收放机构固定在机身上,锁机构将门体结构锁定,电门机构用于传递门体结构的信息,其安装在驾驶舱下部,可用于特殊情况下机组人员空中应急撤离使用,本发明具有开启包线大、可靠性好、人员离机安全性高的特点。
Unit emergency parachuting cabin door and mechanism thereof
一种机组应急跳伞舱门及其机构
2025-02-18
Patent
Electronic Resource
Chinese
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