公开(公告)号：US20180319479A1

公开(公告)日：2018-11-08

申请号：US15773221

申请日：2016-11-02

申请人： LATECOERE

发明人： Cyrille BESSETTES ,  Damien BUCHET

IPC分类号： B64C1/14 ,  E05C3/16 ,  E05C17/00

CPC分类号： B64C1/143 ,  E05C3/162 ,  E05C17/025 ,  E05Y2900/502 ,  E05Y2900/531

摘要： An aircraft emergency exit door (10) with opening mechanisms integrated by a grouping of the mechanisms into a door beam (3) located on a given side of a window (16) of standard dimensions. In the beam, an inner handle (1) is mounted on a main shaft (102) connected with a locking shaft (8A) on which there is mounted, against return springs (83), a door blocking/locking mechanism (8) comprising a lock (81). A mechanism for conditionally opening the door (100) includes a vent flap (110), a pivot connection (12) for coupling the flap (110) to the inner handle (1), and a blocking shaft (120) that has, at each end, a pressure lever (121) equipped with supports for blocking (122) and unblocking (123) the flap (110). Return springs (32) mounted against the conditional opening mechanism (100) are calibrated to allow the opening of the flap (110) by exerting reduced pressure in residual pressure variation conditions, and to prevent it from opening in overpressure conditions.

公开(公告)号：US20150292254A1

公开(公告)日：2015-10-15

申请号：US14443080

申请日：2013-11-14

申请人： LATECOERE

发明人： Cyrille Bessettes ,  Damien Buchet ,  Nicolas Lutzi ,  Renaud Othomene

IPC分类号： E05F15/70 ,  E05F15/60 ,  E05F15/40 ,  E05F11/54 ,  B64C1/14

CPC分类号： E05F15/70 ,  B64C1/1407 ,  B64C1/1423 ,  B64C1/1446 ,  E05F11/54 ,  E05F15/40 ,  E05F15/60 ,  E05Y2900/502

摘要： The invention aims to integrate the activation of the opening/closing phases around a single electric motor, including the treatment of the external window that may be present. An airplane electric door according to the invention has a locking system provided with means for locking a safety catch and a system (200) for coordinating door movements having a single actuating electric motor (2), a cylindrical support (501) having a vertical rotation axis (Z′Z), said support (501) being intended to be rotated by the motor (2), and a fixed guide (91). The support (501) has at least one guideway (511) connected to the arm (6), this guideway (511) being at least partially helical along the vertical axis (Z′Z) of the support (501). The fixed guide (9), which is likewise cylindrical with a vertical axis (Z′Z), possesses at least one double, vertical (91v) and horizontal (91h), camway for guiding the arm (6) successively in these two directions in a manner connected to the arm (6) in order to prevent it from lifting vertically and then to pivot it.

摘要翻译： 本发明旨在将打开/关闭阶段的激活集成在单个电动机周围，包括处理可能存在的外部窗口。 根据本发明的飞机电动门具有锁定系统，其具有用于锁定安全锁扣的装置和用于协调具有单个致动电动机（2）的门运动的系统（200），具有垂直旋转的圆柱形支撑件（501） 轴（Z'Z），所述支撑件（501）旨在由马达（2）旋转，以及固定引导件（91）。 支撑件（501）具有连接到臂（6）的至少一个导轨（511），该导轨（511）沿支撑件（501）的垂直轴线（Z'Z）至少部分地是螺旋形的。 同样圆柱形的具有垂直轴线（Z'Z）的固定引导件（9）具有至少一个用于在这两个方向上连续地引导臂（6）的双垂直（91v）和水平（91h） 以与臂（6）连接的方式，以防止其垂直提升然后使其枢转。