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    • 11. 发明授权
    • PSU pod assembly and method for using same
    • PSU荚组件及其使用方法
    • US09079528B2
    • 2015-07-14
    • US13765646
    • 2013-02-12
    • C&D ZODIAC, INC.
    • Scott Savian
    • B60Q3/02B64D11/00A47B46/00B64D13/00
    • B64D13/00B60Q3/225B60Q3/43B64D11/0015B64D11/003B64D2011/0038Y02T50/46Y10T29/49002
    • A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.
    • 被配置为定位在飞行器内部的PSU舱组件。 PSU盒组件包括PSU盒,其包括壳体,壳体包括顶部,底部以及第一,第二,第三和第四侧,其协作以限定荚内部和位于PSU荚上方并连接到PSU荚的面板。 PSU舱包括至少位于舱内部的第一和第二读取灯,其被配置成将光照射在壳体下方,并且定位在壳体上或壳体中的舱灯,该灯被配置为在壳体上方照射光。 该面板包括被配置为将PSU盒组件固定到飞行器内的组件的连接器。
    • 12. 发明申请
    • AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS
    • 具有声学材料的飞机内部面板
    • US20150144734A1
    • 2015-05-28
    • US14589906
    • 2015-01-05
    • C&D Zodiac, Inc.
    • Scott SavianEric LongJordan De Botton
    • B64C1/40
    • B64C1/40B64C1/066
    • A panel assembly that includes a first panel having an inner surface and an outer surface, and a second panel having an inner surface and an outer surface. The second panel includes a plurality of rib members formed therein that extend inwardly. The rib members include an inner surface and an outer surface. A plurality of panel portions are defined between the plurality of rib members. The panel portions include an inner surface and an outer surface. The inner surface of the rib members are secured to the inner surface of the first panel, and the inner surface of the panel portions is spaced apart from the inner surface of the first panel to define at least first and second cavities.
    • 一种面板组件,其包括具有内表面和外表面的第一面板,以及具有内表面和外表面的第二面板。 第二面板包括在其中形成的多个向内延伸的肋构件。 肋构件包括内表面和外表面。 在多个肋构件之间限定多个面板部。 面板部分包括内表面和外表面。 肋构件的内表面固定到第一面板的内表面,并且面板部分的内表面与第一面板的内表面间隔开以限定至少第一和第二空腔。
    • 13. 发明申请
    • PSU POD ASSEMBLY AND METHOD FOR USING SAME
    • PSU POD组装及其使用方法
    • US20130208490A1
    • 2013-08-15
    • US13765646
    • 2013-02-12
    • C&D ZODIAC, INC.
    • Scott Savian
    • B60Q3/02A47B46/00
    • B64D13/00B60Q3/225B60Q3/43B64D11/0015B64D11/003B64D2011/0038Y02T50/46Y10T29/49002
    • A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.
    • 被配置为定位在飞行器内部的PSU舱组件。 PSU盒组件包括PSU盒,其包括壳体,壳体包括顶部,底部以及第一,第二,第三和第四侧,其协作以限定荚内部和位于PSU荚上方并连接到PSU荚的面板。 PSU舱包括至少位于舱内部的第一和第二读取灯,其被配置成将光照射在壳体下方,并且定位在壳体上或壳体中的舱灯,该灯被配置为在壳体上方照射光。 该面板包括被配置为将PSU盒组件固定到飞行器内的组件的连接器。