ACTUATOR BOX ASSEMBLY
    1.
    发明公开
    ACTUATOR BOX ASSEMBLY 审中-公开
    致动器箱组件

    公开(公告)号:EP1989102A2

    公开(公告)日:2008-11-12

    申请号:EP07751365.3

    申请日:2007-02-22

    IPC分类号: B63B43/02 B63B43/14 F16K31/05

    摘要: An emergency floatation system for an aircraft includes an actuator box assembly that activates the floatation system either electrically or manually. The actuator box assembly is separated from a valve assembly of an inflation reservoir and provides an interface between an electromechanical trigger system and a redundant mechanical trigger system. The actuator box includes a pivot member that provides an interface for the redundant trigger systems and an output actuator. For normal operation a button in the cockpit is pressed which sends an electrical signal to an electromechanical actuator in the actuator box assembly. The electromechanical actuator rotates the pivot member, which operates the output actuator and opens the valve assembly. Alternatively, should the electrical system of the aircraft fail, the pilot or other occupant may activate the mechanical trigger system, thereby rotating the pivot member and activating the output actuator to open the valve assembly.

    摘要翻译: 用于飞机的应急浮动系统包括致动器箱组件,其通过电动或手动来激活浮动系统。 致动器箱组件与充气储存器的阀组件分开并提供机电触发系统和冗余机械触发系统之间的接口。 致动器盒包括为冗余触发器系统和输出致动器提供接口的枢轴构件。 对于正常操作,驾驶舱中的按钮被按下,其将电信号发送到致动器箱组件中的机电致动器。 机电致动器旋转枢转构件,该枢转构件操作输出致动器并打开阀组件。 或者,如果飞机的电气系统发生故障,飞行员或其他乘员可启动机械触发系统,由此旋转枢轴构件并启动输出致动器以打开阀组件。

    FLOATATION SYSTEM INCLUDING LIFE RAFT
    10.
    发明授权
    FLOATATION SYSTEM INCLUDING LIFE RAFT 有权
    随着生活木筏漂浮

    公开(公告)号:EP1429958B1

    公开(公告)日:2007-05-16

    申请号:EP02761719.0

    申请日:2002-09-18

    IPC分类号: B64C25/56

    摘要: An emergency floatation system includes at least one inflatable float and an inflatable emergency life raft contained within a single cover, wherein the system is adapted to be converted from a packed configuration to a partially deployed configuration by use of a first actuating member, and wherein the system is adapted to be converted from the partially deployed configuration into a fully deployed configuration by use of a second actuating member.