LIGHTING ARRAY FOR AN AIRCRAFT
    2.
    发明申请
    LIGHTING ARRAY FOR AN AIRCRAFT 审中-公开
    照明阵列飞机

    公开(公告)号:WO2013181402A3

    公开(公告)日:2014-03-13

    申请号:PCT/US2013043382

    申请日:2013-05-30

    CPC classification number: B64D47/06 B64D47/02 B64D47/04 B64D2203/00

    Abstract: A lighting arrangement for an aircraft includes a navigational lighting group (42) disposed at a leading edge (36) of a wing (38) of the aircraft. The navigational lighting group includes at least one right of way light (50, 52). The lighting arrangement also includes a light bar (44) extending along at least a portion of the leading edge of the wing, adjacent to the navigational lighting group. The light bar is configured to emit light along a length thereof.

    Abstract translation: 用于飞行器的照明装置包括设置在飞机的翼(38)的前缘(36​​)处的导航照明组(42)。 导航照明组包括至少一个路灯(50,52)。 照明装置还包括沿着翼的前缘的至少一部分延伸的灯条(44),其邻近导航照明组。 光条被配置为沿其长度发光。

    LIGHTING ARRAY FOR AN AIRCRAFT
    3.
    发明申请
    LIGHTING ARRAY FOR AN AIRCRAFT 审中-公开
    照明阵列飞机

    公开(公告)号:WO2013181402A2

    公开(公告)日:2013-12-05

    申请号:PCT/US2013/043382

    申请日:2013-05-30

    CPC classification number: B64D47/06 B64D47/02 B64D47/04 B64D2203/00

    Abstract: A lighting arrangement for an aircraft includes a navigational lighting group disposed at a leading edge of a wing of the aircraft. The navigational lighting group includes at least one right of way light. The lighting arrangement also includes a light bar extending along at least a portion of the leading edge of the wing, adjacent to the navigational lighting group. The light bar is configured to emit light along a length thereof.

    Abstract translation: 用于飞机的照明装置包括设置在飞行器的翼的前缘的导航照明组。 导航照明组至少包括一个光照权。 照明装置还包括沿着翼的前缘的至少一部分延伸的灯条,与导航照明组相邻。 光条被配置为沿其长度发光。

    AIRCRAFT SIDEBOARD
    5.
    发明申请
    AIRCRAFT SIDEBOARD 审中-公开
    飞机侧栏

    公开(公告)号:WO2014051638A1

    公开(公告)日:2014-04-03

    申请号:PCT/US2012/059188

    申请日:2012-10-08

    Abstract: An aircraft sideboard (10) includes a first portion (26) with a first top surface (32) and a first panel (62). The first top surface (32) is disposed substantially horizontally at a first height and the first panel (62) is disposed substantially vertically adjacent to the first top surface (32). A second portion (28) is disposed adjacent to the first portion (26) at a first end of the first portion. The second portion (28) includes a second top surface (34) and a second panel (64). The second top surface (34) is disposed substantially horizontally at a second height and the second panel (64) is disposed substantially vertically adjacent to the second top surface (43). A table (76) is stowed interiorly to the first portion (26). The table (76) extends from the first portion when deployed. The first top surface (32) is immovable. The table (76) deploys by tilting the first panel (62) along a pivot axis defined adjacent to a bottom end thereof. The first height is greater than the second height.

    Abstract translation: 飞机侧板(10)包括具有第一顶表面(32)和第一面板(62)的第一部分(26)。 第一顶表面(32)基本上水平地设置在第一高度处,并且第一面板(62)基本上垂直地布置成与第一顶表面(32)相邻。 第二部分(28)在第一部分的第一端处邻近第一部分(26)设置。 第二部分(28)包括第二顶表面(34)和第二面板(64)。 第二顶表面(34)基本上水平地设置在第二高度处,并且第二面板(64)基本上垂直地布置成与第二顶表面(43)相邻。 桌子(76)内部收纳在第一部分(26)上。 当展开时,桌子(76)从第一部分延伸。 第一顶面(32)是不可移动的。 桌子(76)通过沿着与其底端相邻限定的枢转轴线倾斜第一面板(62)来部署。 第一个高度大于第二个高度。

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