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    • 94. 发明公开
    • PIVOT BIN ASSEMBLY
    • SCHWENKBEHÄLTERANORDNUNG
    • EP2956360A1
    • 2015-12-23
    • EP14751181.0
    • 2014-02-13
    • C&D Zodiac, Inc.
    • SAVIAN, ScottKEARSEY, StephenWILLIAMS, Corey
    • B64D11/00
    • B64D11/003B64D2011/0038B64D2011/0053Y02T50/46
    • A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated with the first side panel and the bucket, and a second pivot mechanism operatively associated with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.
    • 枢轴箱组件,其构造成接收行李并定位在飞行器的内部。 所述枢轴箱组件包括上壳体,所述上壳体包括强力和第一和第二侧板,与所述上壳体配合以限定箱体内部的铲斗,与所述第一侧板和所述铲斗可操作地相关联的第一枢转机构,以及 第二枢转机构可操作地与第二侧板和铲斗相关联。 第一和第二枢转机构沿着枢转轴线轴向对准,使得所述铲斗围绕所述枢转轴线相对于所述上壳体在打开位置和关闭位置之间枢转。
    • 95. 发明公开
    • AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS
    • 带有声学材料的飞机内部面板
    • EP2870066A2
    • 2015-05-13
    • EP13812870.7
    • 2013-07-08
    • C&D Zodiac, Inc.
    • SAVIAN, ScottLONG, EricDE BOTTON, Jordan
    • 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。 第二面板包括多个形成于其中的向内延伸的肋构件。 肋构件包括内表面和外表面。 多个肋部件之间限定多个面板部分。 面板部分包括内表面和外表面。 肋构件的内表面固定至第一面板的内表面,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腔和第二腔。
    • 97. 发明公开
    • PSU POD ASSEMBLY AND METHOD FOR USING SAME
    • PSU-POD-ANORDNUNG UND VERWENDUNGSVERFAHRENDAFÜR
    • EP2815285A1
    • 2014-12-24
    • EP13748536.3
    • 2013-02-13
    • C&D Zodiac, Inc.
    • SAVIAN, Scott
    • G05F1/00
    • 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。 面板包括被配置成将PSU盒组件固定到飞行器内的部件的连接器。