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    • 51. 发明申请
    • PIVOT BIN ASSEMBLY
    • PIVOT BIN总成
    • US20150307192A1
    • 2015-10-29
    • US14796829
    • 2015-07-10
    • C&D Zodiac, Inc.
    • Scott Savian
    • B64D11/00
    • B64D11/003B60Q3/43B64D11/0015B64D2011/0038B64D2011/0046B64D2011/0053Y02T50/46
    • An aircraft storage bin that includes an upper housing, and a bucket pivotally connected to the upper housing that cooperates with the upper housing to define a bin interior. The bucket includes a bottom, a front edge and first and second opposing side walls extending upwardly from the bottom and pivots about a pivot axis with respect to the upper housing between an open position and a closed position. When the storage bin is installed in an aircraft, a first horizontal distance is defined between a first vertical line that extends through the pivot axis and the front edge of the bucket when the bucket is in the closed position, and a second horizontal distance is defined between the first vertical line and the front edge of the bucket when the bucket is in the open position. The first horizontal distance is greater than the second horizontal distance.
    • 一种包括上部壳体的飞行器存储箱,以及与上壳体枢转连接的铲斗,该铲斗与上壳体配合以限定箱体内部。 铲斗包括底部,前边缘以及从底部向上延伸的第一和第二相对侧壁,并且在打开位置和关闭位置之间相对于上壳体枢转枢转。 当存储箱安装在飞行器中时,当铲斗处于关闭位置时,在通过枢转轴线延伸的第一垂直线和铲斗的前边缘之间限定第一水平距离,并且定义第二水平距离 当铲斗处于打开位置时,在第一垂直线和铲斗的前边缘之间。 第一个水平距离大于第二个水平距离。
    • 54. 发明授权
    • Freewheeling rotary damping mechanism
    • 续流旋转阻尼机构
    • US08899390B2
    • 2014-12-02
    • US13765358
    • 2013-02-12
    • C&D Zodiac, Inc.
    • Stephen KearseyRichard McClure
    • F16D57/02F16F9/32A47B46/00F16F9/14B64D11/00
    • F16F9/3207A47B46/00B64D11/003F16F9/145
    • A damping mechanism that includes a housing with an inner circumferential surface defined by an assembly outer race, an axle shaft that is rotatable with respect to the housing, and a transmission assembly operatively associated with the axle shaft and disposed within the housing. The transmission assembly includes an assembly intermediate race. A fluid space that includes fluid therein is defined between the assembly intermediate race and the inner circumferential surface of the assembly outer race. A vane is disposed between the assembly intermediate race and the inner circumferential surface of the assembly outer race. The vane includes a restriction space defined therein. When the axle shaft rotates in the first direction, the transmission assembly transmits rotation from the axle shaft to the vane, and when the axle shaft rotates in the second direction, the transmission assembly transmits less rotation to the first vane than when the axle shaft rotates in the first direction.
    • 一种阻尼机构,包括具有由组件外座圈限定的内圆周表面的壳体,可相对于所述壳体旋转的车轴,以及与所述车轴一起操作地配置并设置在所述壳体内的变速器组件。 传动组件包括组合中间座圈。 在组件中间座圈和组件外圈的内圆周表面之间限定包括流体的流体空间。 叶片设置在组装中间座圈和组件外圈的内周面之间。 叶片包括其中限定的限制空间。 当车轴沿第一方向旋转时,传动组件将转轴从轴轴传递到叶片,并且当车轴沿第二方向旋转时,传动组件相对于第一叶片的旋转少于当车轴旋转时 在第一个方向。
    • 58. 发明申请
    • HIGH PRIVACY PASSENGER AIRCRAFT CABIN ARRANGEMENT
    • 高保密乘客飞机仓库安排
    • US20130105627A1
    • 2013-05-02
    • US13665476
    • 2012-10-31
    • C&D ZODIAC, INC.
    • Ben OrsonElijah Dobrusin
    • B64D11/00
    • B64D11/00B64D11/0601
    • An aircraft that includes a cabin that has a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough, a first door positioned fore of the first class section, an economy class section positioned in the interior and aft of the first class section, and a longitudinally extending second aisle that extends parallel to the first aisle and that does not extend through the first class section. An economy class passenger that enters through the first door travels down the second aisle to enter the economy class section and never enters the first class section.
    • 一种飞机,其包括具有地板,侧壁,天花板和内部的舱室,位于内部的第一类部分,其包括延伸穿过其中的纵向延伸的第一通道,位于第一类部分前方的第一门, 经济舱部分位于第一类部分的内部和后部,以及纵向延伸的第二通道,其平行于第一通道延伸并且不延伸穿过第一类部分。 通过第一个门进入的经济舱乘客从第二个通道行进,进入经济舱,不得进入第一类。