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    INTEGRATED CENTERLINE LAVATORY MONUMENT
    41.
    发明申请
    INTEGRATED CENTERLINE LAVATORY MONUMENT 审中-公开

    公开(公告)号：US20180148175A1

    公开(公告)日：2018-05-31

    申请号：US15878220

    申请日：2018-01-23

    Applicant: C&D Zodiac, Inc.

    Inventor： Scott SAVIAN ,  Zhao JIN

    IPC: B64D11/02 ,  B64D11/04 ,  B64D11/00

    CPC classification number: B64D11/02 ,  B64D11/04 ,  B64D2011/0046 ,  Y10T29/49826

    Abstract: A monument configured to be positioned in the interior of an aircraft that includes first, second, third and fourth sides and first and second lavatories spaced apart from one another by at least a portion of a galley storage section that is open to the first side. The first and second sides are opposite to one another and the third and fourth sides are opposite to one another. The first lavatory defines a first lavatory interior and includes a first toilet therein and the second lavatory defines a second lavatory interior and includes a second toilet therein.

    PIVOT BIN ASSEMBLY WITH TWO PART PIVOT AXLE
    42.
    发明申请
    PIVOT BIN ASSEMBLY WITH TWO PART PIVOT AXLE 审中-公开

    公开(公告)号：US20180044022A1

    公开(公告)日：2018-02-15

    申请号：US15727467

    申请日：2017-10-06

    Applicant: C&D ZODIAC, INC.

    Inventor： Scott Savian

    IPC: B64D11/00

    CPC classification number: B64D11/003 ,  B60Q3/43 ,  B64D11/0015 ,  B64D2011/0038 ,  Y02T50/46

    Abstract: An aircraft storage bin that includes an upper housing with first and second side panels, a bucket that includes a bottom and first and second sides, a first clevis assembly that includes a first inner plate and a first outer plate that extend between the first side panel and the first side wall, and a second clevis assembly that includes a second inner plate and a second outer plate that extend between the second side panel and the second side wall. The first inner plate includes a first outer protrusion and the first outer plate includes first inner protrusion that cooperate to form a first pivot axle. The second inner plate includes a second outer protrusion and the second outer plate includes second inner protrusion that cooperate to form a second pivot axle.

    Pivot bin assembly with minimal force required for closing
    43.
    发明授权
    Pivot bin assembly with minimal force required for closing 有权

    公开(公告)号：US09789963B2

    公开(公告)日：2017-10-17

    申请号：US14924607

    申请日：2015-10-27

    Applicant: C&D ZODIAC, INC.

    Inventor： Scott Savian

    IPC: B64D11/00 ,  B60Q3/43

    CPC classification number: B64D11/003 ,  B60Q3/43 ,  B64D11/0015 ,  B64D2011/0038 ,  Y02T50/46

    Abstract: 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, first and second opposing side walls extending upwardly from the bottom and a center of gravity. The bucket pivots about a pivot axis with respect to the upper housing between an open position and a closed position. The center of gravity of the bucket is positioned below the pivot axis when the bucket is in the closed position.

    QUAD MODULAR LAVATORY WITH ALCOVES
    46.
    发明申请
    QUAD MODULAR LAVATORY WITH ALCOVES 有权
    QUAD模块化装置与ALCOVES

    公开(公告)号：US20170001729A1

    公开(公告)日：2017-01-05

    申请号：US15257626

    申请日：2016-09-06

    Applicant: C&D ZODIAC, INC.

    Inventor： Scott Savian

    IPC: B64D11/02 ,  A47K4/00

    CPC classification number: B64D11/02 ,  A47K4/00 ,  B64D11/003 ,  B64D11/0641 ,  B64D11/0691 ,  B64D2011/0046 ,  B64D2231/025 ,  Y10T29/49826

    Abstract: A modular lavatory monument assembly configured to be positioned in the interior of an aircraft. The modular lavatory monument assembly includes first, second, third and fourth walls that cooperate to form an outer shell that defines a lavatory interior. The fourth wall includes an alcove extending outwardly therefrom. The assembly also includes a sink module positioned in the alcove, a mirror module positioned above the sink module in the alcove, and a door positioned on one of the second or third walls.

    Abstract translation: 一个模块化的盥洗室纪念碑组件，被配置为定位在飞行器的内部。 模块化盥洗室纪念碑集合包括第一，第二，第三和第四墙壁，其协作形成限定盥洗室内部的外壳。 第四壁包括从其向外延伸的壁龛。 组件还包括定位在凹室中的水槽模块，位于凹室中的水槽模块上方的反射镜模块以及位于第二或第三壁之一上的门。

    DESIGN OPTIMIZER SYSTEM AND METHODS
    49.
    发明申请
    DESIGN OPTIMIZER SYSTEM AND METHODS 审中-公开
    设计优化系统和方法

    公开(公告)号：US20160180017A1

    公开(公告)日：2016-06-23

    申请号：US15059162

    申请日：2016-03-02

    Applicant: C&D ZODIAC, INC.

    Inventor： Scott Savian ,  Sandesh Shetty ,  Roy Benjamin Sandberg

    IPC: G06F17/50

    CPC classification number: G06F17/5095 ,  B64D11/00 ,  B64D11/06 ,  B64F5/00 ,  G06F2217/02

    Abstract: A computerized system for determining the design layout of an aircraft. The system includes an input module configured to receive a first input data indicating a first value of a first parameter, a first feature database that includes a plurality of feature settings, a feature search module configured to search the first feature database and select a feature setting based on the first value of the first parameter, a central database that includes a plurality of rules governing a design layout of a fuselage, and an optimizing module in communication with the central database and configured to generate an optimal design layout based on the selected feature setting.

    Abstract translation: 一种用于确定飞机设计布局的计算机化系统。 该系统包括：输入模块，被配置为接收指示第一参数的第一值的第一输入数据;包括多个特征设置的第一特征数据库;被配置为搜索第一特征数据库并选择特征设置的特征搜索模块 基于所述第一参数的第一值，包括控制机身的设计布局的多个规则的中央数据库，以及与所述中央数据库通信并被配置为基于所选择的特征生成最佳设计布局的优化模块 设置。

    DOOR FOR AN AIRCRAFT
    50.
    发明申请
    DOOR FOR AN AIRCRAFT 有权
    飞机门

    公开(公告)号：US20160144944A1

    公开(公告)日：2016-05-26

    申请号：US14900973

    申请日：2014-07-11

    Applicant: William A. GOINGS ,  Eric LONG ,  LEARJET INC. ,  C&D ZODIAC INC.

    Inventor： William A. GOINGS ,  Eric LONG

    IPC: B64C1/14 ,  E05F11/54 ,  B64D11/02

    CPC classification number: B64C1/14 ,  B64D11/0023 ,  B64D11/02 ,  E05F11/54 ,  E05Y2900/502

    Abstract: A door for an aircraft includes a first panel divisible into at least two first slats that are releasably connected to one another, a first tensioning cable attached between the at least two first slats, and a first tensioner connected to the first tensioning cable and being operative to apply a first tension thereto, thereby permitting the first tensioning cable to hold the at least two first slats together to form the first panel and to release the first tension in the first tensioning cable upon occurrence of a release action, thereby permitting the at least two first slats to dissociate from one another so that the first panel fragments.

    Abstract translation: 一种用于飞行器的门包括可分成至少两个彼此可释放地连接的第一板条的第一板，连接在所述至少两个第一板条之间的第一张紧绳索，以及连接到所述第一张紧绳索并且被操作的第一张紧器 以向其施加第一张力，从而允许第一张紧缆索将至少两个第一板条保持在一起以形成第一板，并且在出现释放动作时释放第一张紧缆索中的第一张力，从而允许至少 两个第一个板条彼此离解，使第一个面板碎片。

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