Method for mounting an aircraft component and aircraft assembly
    2.
    发明授权
    Method for mounting an aircraft component and aircraft assembly 有权
    安装飞机部件和飞机组件的方法

    公开(公告)号:US08944382B2

    公开(公告)日:2015-02-03

    申请号:US13601485

    申请日:2012-08-31

    IPC分类号: B64C1/14 B64F5/00 B64C25/10

    摘要: A method for mounting an aircraft component, which in the mounted state is movable between a first and a second operating position and is taken up in its first operating position in a mounting area, comprises the measuring of the mounting area, in order to obtain data characteristic of the shape and/or the dimensions of the mounting area. The data characteristic of the shape and/or the dimensions of the mounting area are projected onto the aircraft component arranged in its second operating position. Finally, the aircraft component arranged in its second operating position is adjusted with reference to the projection of the data characteristic of the shape and/or the dimensions of the mounting area.

    摘要翻译: 一种用于安装飞行器部件的方法,其在安装状态下可在第一和第二操作位置之间移动并且在其安装区域中的第一操作位置被吸收,包括测量安装区域,以便获得数据 安装区域的形状和/或尺寸的特征。 安装区域的形状和/或尺寸的数据特征被投影到布置在其第二操作位置的飞行器部件上。 最后,参照投影形状的数据特征和/或安装区域的尺寸来调整布置在其第二操作位置的飞行器部件。

    CENTRIFUGE AND CENTRIFUGE ROTOR FOR THE SAME
    3.
    发明申请
    CENTRIFUGE AND CENTRIFUGE ROTOR FOR THE SAME 有权
    离心机和离心机相同

    公开(公告)号:US20110183830A1

    公开(公告)日:2011-07-28

    申请号:US13059320

    申请日:2009-08-17

    IPC分类号: B04B9/00 B04B15/00

    摘要: A centrifuge for separating solids from a liquid including a centrifuge rotor with a rotor shaft, partially formed as a hollow shaft, and a centrifuging drum, being rotatable with the rotor shaft, wherein the liquid to be separated can be supplied via the cavity of the hollow shaft. To ease emptying of the drum, the centrifuging drum includes a drum lower part and a drum upper part, which bears loosely against the drum lower part. The upper part is guided in an axially movable manner on the shaft and is movable by means of a disengagement mechanism parallel to the rotor axis into an open position in which, for self-emptying of the interior space, the drum parts are spaced apart from one another while they still rotate with the rotor shaft.

    摘要翻译: 一种用于从包括离心机转子的液体的液体中分离固体的离心机,其具有转子轴,部分地形成为空心轴,以及离心鼓,其可与转子轴一起旋转,其中待分离的液体可以经由 中空轴。 为了减轻鼓的排空,离心鼓包括鼓下部和鼓上部,其松动地抵靠滚筒下部。 上部在轴上以可轴向方式被引导,并且可通过平行于转子轴线的分离机构移动到打开位置,在该打开位置中,为了自动排空内部空间,鼓部分与 而它们仍然随着转子轴旋转。

    Centrifuge for separating solid matter from a liquid and centrifuge rotor for the same
    4.
    发明授权
    Centrifuge for separating solid matter from a liquid and centrifuge rotor for the same 有权
    用于从液体中分离固体物质并离心转子用于离心机

    公开(公告)号:US09144807B2

    公开(公告)日:2015-09-29

    申请号:US13059320

    申请日:2009-08-17

    摘要: A centrifuge for separating solids from a liquid including a centrifuge rotor with a rotor shaft, partially formed as a hollow shaft, and a centrifuging drum, being rotatable with the rotor shaft, wherein the liquid to be separated can be supplied via the cavity of the hollow shaft. To ease emptying of the drum, the centrifuging drum includes a drum lower part and a drum upper part, which bears loosely against the drum lower part. The upper part is guided in an axially movable manner on the shaft and is movable by means of a disengagement mechanism parallel to the rotor axis into an open position in which, for self-emptying of the interior space, the drum parts are spaced apart from one another while they still rotate with the rotor shaft.

    摘要翻译: 一种用于从包括离心机转子的液体的液体中分离固体的离心机,其具有转子轴,部分地形成为空心轴,以及离心鼓,其可与转子轴一起旋转,其中待分离的液体可以经由 中空轴。 为了减轻鼓的排空,离心鼓包括鼓下部和鼓上部,其松动地抵靠滚筒下部。 上部在轴上以可轴向方式被引导,并且可通过平行于转子轴线的分离机构移动到打开位置,在该打开位置中,为了自动排空内部空间,鼓部分与 而它们仍然随着转子轴旋转。

    METHOD FOR MOUNTING AN AIRCRAFT COMPONENT AND AIRCRAFT ASSEMBLY
    5.
    发明申请
    METHOD FOR MOUNTING AN AIRCRAFT COMPONENT AND AIRCRAFT ASSEMBLY 有权
    安装飞机组件和飞机装配的方法

    公开(公告)号:US20130056584A1

    公开(公告)日:2013-03-07

    申请号:US13601485

    申请日:2012-08-31

    摘要: A method for mounting an aircraft component, which in the mounted state is movable between a first and a second operating position and is taken up in its first operating position in a mounting area, comprises the measuring of the mounting area, in order to obtain data characteristic of the shape and/or the dimensions of the mounting area. The data characteristic of the shape and/or the dimensions of the mounting area are projected onto the aircraft component arranged in its second operating position. Finally, the aircraft component arranged in its second operating position is adjusted with reference to the projection of the data characteristic of the shape and/or the dimensions of the mounting area.

    摘要翻译: 一种用于安装飞行器部件的方法,其在安装状态下可在第一和第二操作位置之间移动并且在其安装区域中的第一操作位置被吸收,包括测量安装区域,以便获得数据 安装区域的形状和/或尺寸的特征。 安装区域的形状和/或尺寸的数据特征被投影到布置在其第二操作位置的飞行器部件上。 最后,参照投影形状的数据特征和/或安装区域的尺寸来调整布置在其第二操作位置的飞行器部件。