TERTIARY LOCKING ASSEMBLY FOR A THRUST REVERSER
    2.
    发明申请
    TERTIARY LOCKING ASSEMBLY FOR A THRUST REVERSER 有权
    紧急锁定装置

    公开(公告)号:US20140076999A1

    公开(公告)日:2014-03-20

    申请号:US14060823

    申请日:2013-10-23

    Applicant: Aircelle

    Abstract: A tertiary locking assembly for a thrust reverser includes a tertiary lock, a primary control line associated with the tertiary lock, and a secondary control line. The primary control line includes a primary electromechanical valve and a primary power supply line connected to the primary electromechanical valve. In addition, the secondary control line has a secondary electromechanical control valve and a secondary power supply line connected to the secondary electromechanical control valve. In particular, the secondary control line is provided with at least one manually controlled switch.

    Abstract translation: 用于推力反向器的三级锁定组件包括三级锁,与第三级锁相关联的主控制线和辅助控制线。 主控制线包括主机电阀和连接到主机电阀的主电源线。 另外,二次控制线具有二次机电控制阀和与二次机电控制阀连接的二次供电线。 特别地,辅助控制线设置有至少一个手动控制开关。

    Tertiary locking assembly for a thrust reverser
    4.
    发明授权
    Tertiary locking assembly for a thrust reverser 有权
    用于推力反向器的三级锁定组件

    公开(公告)号:US09458794B2

    公开(公告)日:2016-10-04

    申请号:US14060823

    申请日:2013-10-23

    Applicant: AIRCELLE

    Abstract: A tertiary locking assembly for a thrust reverser includes a tertiary lock, a primary control line associated with the tertiary lock, and a secondary control line. The primary control line includes a primary electromechanical valve and a primary power supply line connected to the primary electromechanical valve. In addition, the secondary control line has a secondary electromechanical control valve and a secondary power supply line connected to the secondary electromechanical control valve. In particular, the secondary control line is provided with at least one manually controlled switch.

    Abstract translation: 用于推力反向器的三级锁定组件包括三级锁,与第三级锁相关联的主控制线和辅助控制线。 主控制线包括主机电阀和连接到主机电阀的主电源线。 另外,二次控制线具有二次机电控制阀和与二次机电控制阀连接的二次供电线。 特别地,辅助控制线设置有至少一个手动控制开关。

    ACUTATOR FOR AIRCRAFT TURBINE ENGINE NACELLE WITH NOTABLY ONE-PIECE ANNULAR REAR PART
    5.
    发明申请
    ACUTATOR FOR AIRCRAFT TURBINE ENGINE NACELLE WITH NOTABLY ONE-PIECE ANNULAR REAR PART 审中-公开
    航空发动机发动机与非常一个单独的后端零件

    公开(公告)号:US20140271163A1

    公开(公告)日:2014-09-18

    申请号:US14287845

    申请日:2014-05-27

    Applicant: AIRCELLE

    Abstract: An actuator for an aircraft turbine engine nacelle with a one-piece annular rear part, includes an engine assembly having a nut which is capable of rotating but not of translational movement, and a shaft for turning this nut. The actuator also includes a screw assembly having a screw capable of translational movement without rotating, in mesh with the nut, and a ball joint at one end of this screw intended to be fixed to the annular rear part.

    Abstract translation: 具有一体式环形后部部分的用于飞机涡轮发动机机舱的致动器包括具有能够旋转但不能平移运动的螺母的发动机组件和用于转动该螺母的轴。 致动器还包括螺钉组件,其具有能够平移运动而不旋转的螺钉,与螺母啮合,并且在该螺钉的一端的球形接头用于固定到环形后部。

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