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? aircraft emergency exit door, and method for opening / closing an aircraft emergency exit door?

机译:?飞机紧急出口门,以及打开/关闭飞机紧急出口门的方法?

摘要

an aircraft emergency exit door (10) with opening mechanisms integrated by a grouping of said mechanisms in a door bar (3) positioned on one side of a standard sized window (16). In said bar an inner handle (1) is mounted on a mainshaft (102) connected to a locking shaft (8a) on which a locking / locking door mechanism (83) is mounted against return springs (83). 8) comprising a lock (81). a conditional door opening mechanism (100) comprises a vent flap (110), a pivot connection (12) for coupling flap (110) to the inner handle (1), and a locking shaft (120) having , at each end, a pressure lever (121) equipped with brackets for locking (122) and unlocking (123) the tab (110). return springs (32) mounted against the conditional opening mechanism (100) are calibrated to allow said flap (110) to open under reduced pressure under varying residual pressure conditions, and to prevent it from opening under overpressure conditions .
机译:一种飞机紧急出口门(10),其打开机构通过一组所述机构集成在位于标准尺寸窗户(16)一侧的门杆(3)中。在所述杆中,内部手柄(1)安装在主轴(102)上,主轴(102)连接至锁定轴(8a),锁定/锁定门机构(83)抵着复位弹簧(83)安装在锁定轴(8a)上。 8)包括锁(81)。一个有条件的门打开机构(100)包括一个排气门(110),一个将门(110)耦合到内部把手(1)的枢轴连接(12)和一个锁轴(120),锁轴的两端各有一个压力杆(121)配有用于锁定(122)和解锁(123)凸舌(110)的支架。校准抵靠有条件打开机构(100)安装的复位弹簧(32),以允许所述阀瓣(110)在变化的残余压力条件下在减压下打开,并防止其在过压条件下打开。

著录项

  • 公开/公告号BR112018008872A8

    专利类型

  • 公开/公告日2019-02-26

    原文格式PDF

  • 申请/专利权人 LATECOERE;

    申请/专利号BR20181108872

  • 发明设计人 CYRILLE BESSETTES;DAMIEN BUCHET;

    申请日2016-11-02

  • 分类号B64C1/14;

  • 国家 BR

  • 入库时间 2022-08-21 12:03:37

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