CONTROL WHEEL FOR AERONAUTICS
    2.
    发明申请
    CONTROL WHEEL FOR AERONAUTICS 有权
    航空控制轮

    公开(公告)号:US20130255436A1

    公开(公告)日:2013-10-03

    申请号:US13834263

    申请日:2013-03-15

    CPC classification number: G05G1/10 B64C13/04 Y10T74/20256 Y10T74/20834

    Abstract: The invention concerns a control wheel (100) for aeronautics constituted of at least two half-shells (10) assembled one to the other, said half-shells comprising reinforcing ribs (11) on their internal surface, positioning and fixing means (12) and locating holes (13) to allow the passage of electrical wires connecting electrical actuating means (20) to a control unit. The control wheel (100) includes a central opening (15) intended to be connected to a control shaft/hub. The wheel comprises an intermediate guide part (50) disposed between the half-shells (10) and positioned inside the control wheel (100), said part including at least one guide conduit (51) adapted to connect on the one hand a locating hole (13) to the central opening (15) of the control wheel (100).

    Abstract translation: 本发明涉及一种用于航空的控制轮(100),该控制轮由至少两个彼此组装的半壳(10)组成,所述半壳在其内表面上包括加强肋(11),定位和固定装置(12) 以及定位孔(13)以允许将电致动装置(20)连接到控制单元的电线通过。 控制轮(100)包括旨在连接到控制轴/轮毂的中心开口(15)。 所述车轮包括设置在所述半壳体(10)之间并且位于所述控制轮(100)内部的中间引导部件(50),所述部件包括至少一个导向管道(51),所述至少一个引导管道一方面连接定位孔 (13)连接到控制轮(100)的中心开口(15)。

    Control wheel for aeronautics
    4.
    发明授权
    Control wheel for aeronautics 有权
    航空控制轮

    公开(公告)号:US08997598B2

    公开(公告)日:2015-04-07

    申请号:US13834263

    申请日:2013-03-15

    CPC classification number: G05G1/10 B64C13/04 Y10T74/20256 Y10T74/20834

    Abstract: The invention concerns a control wheel (100) for aeronautics constituted of at least two half-shells (10) assembled one to the other, said half-shells comprising reinforcing ribs (11) on their internal surface, positioning and fixing means (12) and locating holes (13) to allow the passage of electrical wires connecting electrical actuating means (20) to a control unit. The control wheel (100) includes a central opening (15) intended to be connected to a control shaft/hub. The wheel comprises an intermediate guide part (50) disposed between the half-shells (10) and positioned inside the control wheel (100), said part including at least one guide conduit (51) adapted to connect on the one hand a locating hole (13) to the central opening (15) of the control wheel (100).

    Abstract translation: 本发明涉及一种用于航空的控制轮(100),该控制轮由至少两个彼此组装的半壳(10)组成,所述半壳在其内表面上包括加强肋(11),定位和固定装置(12) 以及定位孔(13)以允许将电致动装置(20)连接到控制单元的电线通过。 控制轮(100)包括旨在连接到控制轴/轮毂的中心开口(15)。 所述车轮包括设置在所述半壳体(10)之间并且位于所述控制轮(100)内部的中间引导部件(50),所述部件包括至少一个导向管道(51),所述至少一个引导管道一方面连接定位孔 (13)连接到控制轮(100)的中心开口(15)。

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