Apparatus and method for providing a suspended agent
    1.
    发明授权
    Apparatus and method for providing a suspended agent 失效
    用于提供悬浮剂的装置和方法

    公开(公告)号:US06387077B1

    公开(公告)日:2002-05-14

    申请号:US09687323

    申请日:2000-10-13

    Abstract: Apparatus and methods for maintaining the suspension of an agent suspended in a suspending medium in which a container holding the agent is revolved about an axis to create and maintain the suspension and the agent is selectively provided from the container. The agent may be selectively provided from the container while the container is simultaneously or intermittently revolved in a planetary orbit about an axis of rotation generally parallel to an axis of the container for maintaining the suspension. Alternatively, the container may be rotated about its longitudinal axis by a source of rotation to create and maintain the suspension while the agent is provided from the container due to a force imparted by the source of rotation.

    Abstract translation: 用于保持悬浮在悬挂介质中的试剂的悬浮液的装置和方法,其中容纳所述试剂的容器围绕轴旋转以产生并保持所述悬浮液,并且所述试剂从所述容器中选择性地提供。 当容器围绕围绕容器的轴线的旋转轴线以行星轨道同时或间歇地旋转时,容器可以选择性地提供,用于维持悬架。 或者,容器可以通过旋转源围绕其纵向轴线旋转以产生并保持悬架,同时由于由旋转源施加的力而从容器提供试剂。

    Filter systems for air intakes of aircraft engines and related methods
    2.
    发明授权
    Filter systems for air intakes of aircraft engines and related methods 有权
    飞机发动机进气过滤系统及相关方法

    公开(公告)号:US08961634B2

    公开(公告)日:2015-02-24

    申请号:US13274965

    申请日:2011-10-17

    Abstract: A filter system includes a filter assembly having an interior, an end defining a bypass opening, and another end for coupling to an air intake of an aircraft engine to permit intake air from the interior to enter the air intake. The filter system includes a bypass closure movable relative to the filter assembly between at least a first position and a second position. The bypass closure substantially covers the bypass opening in the first position to inhibit intake air from entering the interior through the bypass opening. The filter system includes an actuator coupled to at least one of the filter assembly and the bypass member to cause relative movement of the bypass closure between the first and second positions.

    Abstract translation: 过滤器系统包括具有内部的过滤器组件,限定旁路开口的端部,以及用于联接到飞行器发动机的进气口的另一端,以允许来自内部的进气进入进气口。 过滤器系统包括在至少第一位置和第二位置之间相对于过滤器组件可移动的旁路封闭件。 旁路盖基本上覆盖在第一位置的旁路开口,以阻止进气通过旁路开口进入内部。 过滤器系统包括联接到过滤器组件和旁路构件中的至少一个的致动器,以引起旁路闭合件在第一和第二位置之间的相对运动。

    Filter Systems For Air Intakes Of Aircraft Engines and Related Methods
    3.
    发明申请
    Filter Systems For Air Intakes Of Aircraft Engines and Related Methods 有权
    飞机发动机进气过滤系统及相关方法

    公开(公告)号:US20130092798A1

    公开(公告)日:2013-04-18

    申请号:US13274965

    申请日:2011-10-17

    Abstract: A filter system includes a filter assembly having an interior, an end defining a bypass opening, and another end for coupling to an air intake of an aircraft engine to permit intake air from the interior to enter the air intake. The filter system includes a bypass closure movable relative to the filter assembly between at least a first position and a second position. The bypass closure substantially covers the bypass opening in the first position to inhibit intake air from entering the interior through the bypass opening. The filter system includes an actuator coupled to at least one of the filter assembly and the bypass member to cause relative movement of the bypass closure between the first and second positions.

    Abstract translation: 过滤器系统包括具有内部的过滤器组件,限定旁路开口的端部,以及用于联接到飞行器发动机的进气口的另一端,以允许来自内部的进气进入进气口。 过滤器系统包括在至少第一位置和第二位置之间相对于过滤器组件可移动的旁路封闭件。 旁路盖基本上覆盖在第一位置的旁路开口,以阻止进气通过旁路开口进入内部。 过滤器系统包括联接到过滤器组件和旁路构件中的至少一个的致动器,以在第一和第二位置之间引起旁路闭合件的相对运动。

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