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    PIVOT BIN ASSEMBLY
    21.
    发明公开
    PIVOT BIN ASSEMBLY 审中-公开

    公开(公告)号：EP3412571A1

    公开(公告)日：2018-12-12

    申请号：EP18185347.4

    申请日：2015-07-10

    Applicant: C&D Zodiac, Inc.

    Inventor： SAVIAN, Scott

    IPC: B64D11/00

    CPC classification number: B64D11/003 ,  Y02T50/46

    Abstract: An aircraft storage bin comprising: 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. The bucket 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. The aircraft storage bin further comprises a first pivot mechanism operatively associated with the first side wall of the bucket and a second pivot mechanism operatively associated with the second side wall of the bucket. The first side wall of the bucket defines a first arcuate slot therein and the second side wall of the bucket defines a second arcuate slot therein. The first arcuate slot receives the first pivot mechanism and the second arcuate slot receives the second pivot mechanism. The first and second arcuate slots are open to a top edge of the first and second side walls of the bucket.

    COMPACT CABIN ATTENDANT SEAT STOWAGE
    22.
    发明授权
    COMPACT CABIN ATTENDANT SEAT STOWAGE 有权

    公开(公告)号：EP2991899B1

    公开(公告)日：2018-06-06

    申请号：EP14791218.2

    申请日：2014-04-29

    Applicant: C&D Zodiac, Inc.

    Inventor： NABIH, Najd ,  REAMS, Edward ,  SAVIAN, Scott ,  ZARROUATI, Olivier

    IPC: B64D11/06

    CPC classification number: B64D11/02 ,  B60N2/3018 ,  B60N2/3029 ,  B60N2/3031 ,  B60N2/3047 ,  B60N2/856 ,  B64D11/0691

    Abstract: An aircraft monument that includes an enclosure with an enclosure interior, a compartment with a compartment interior positioned in the enclosure interior, and a stowable seat assembly disposed in the compartment. The compartment includes at least a first vertically oriented wall. The seat assembly includes a chair assembly with a back portion and a seat portion pivotably connected to the back portion along a seat pivot axis such that the seat is pivotable between closed and open positions. The chair assembly is movable between a stowed position where the seat pivot axis extends generally parallel to the first wall and the chair assembly is positioned in the compartment interior, and a deployed position where the seat pivot axis extends generally perpendicular to the first wall and the chair assembly is positioned outside of the compartment interior.

    DESIGN OPTIMIZER SYSTEM AND METHODS
    23.
    发明公开
    DESIGN OPTIMIZER SYSTEM AND METHODS 审中-公开
    设计优化器系统和方法

    公开(公告)号：EP3265338A1

    公开(公告)日：2018-01-10

    申请号：EP16759442.3

    申请日：2016-03-02

    Applicant: C&D Zodiac, Inc.

    Inventor： SAVIAN, Scott ,  SHETTY, Sandesh ,  SANDBERG, Roy, Benjamin

    IPC: B60N2/00 ,  B64D11/06 ,  G06F17/50

    CPC classification number: G06F17/5095 ,  B64D11/06

    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.

    DESIGN OPTIMIZER SYSTEM
    24.
    发明公开
    DESIGN OPTIMIZER SYSTEM 审中-公开
    设计优化器系统

    公开(公告)号：EP2969754A1

    公开(公告)日：2016-01-20

    申请号：EP13877481.5

    申请日：2013-05-28

    Applicant: C&D Zodiac, Inc.

    Inventor： SAVIAN, Scott ,  SHETTY, Sandesh ,  SBEGLIA, Adam

    IPC: B64D11/06

    CPC classification number: G06F17/5095 ,  B64D11/00 ,  B64D11/06 ,  G06F2217/02 ,  G06F2217/46

    Abstract: A computerized system for optimizing the design layout of an aircraft configured to execute, by at least one processor, the instructions of one or more software modules stored on a nonvolatile computer readable medium, the system comprising a first software module configured to receive input from a user regarding number of seats; a second software module configured to receive input from a user regarding seat pitch; a third software module configured to receive input from a user regarding meal service; a fourth software module configured to receive input from a user regarding beverage service; a fifth software module configured to comprise a listing of all possible combinations of all aircraft interior layout configurations for an aircraft. The sixth software module uses the inputs from one or more of the first, second, third, or fourth software modules to determine and create an output of the one configuration that takes up the least amount of seat space, weighs the least, and contains the most amount of aircraft cabin storage space. A seventh software module graphically displays the output of the sixth software module.

    Abstract translation: 一种用于优化飞机的设计布局的计算机化系统，所述飞机的设计布局被配置为由至少一个处理器执行存储在非易失性计算机可读介质上的一个或多个软件模块的指令，所述系统包括第一软件模块，所述第一软件模块被配置为接收来自 用户关于座位数量; 第二软件模块，其被配置为从用户接收关于座位间距的输入; 第三软件模块，其被配置为从用户接收关于膳食服务的输入; 第四软件模块，被配置为从用户接收关于饮料服务的输入; 第五软件模块，其被配置为包括航空器的所有飞机内部布局配置的所有可能组合的列表。 第六软件模块使用来自第一，第二，第三或第四软件模块中的一个或多个的输入来确定并创建占用最少量座位空间的一个配置的输出，其重量最小并包含 最多的飞机机舱存储空间。 第七个软件模块以图形方式显示第六个软件模块的输出。

    PIVOT BIN ASSEMBLY
    25.
    发明公开
    PIVOT BIN ASSEMBLY 有权

    公开(公告)号：EP2814737A1

    公开(公告)日：2014-12-24

    申请号：EP13749848.1

    申请日：2013-02-13

    Applicant: C&D Zodiac, Inc.

    Inventor： SAVIAN, Scott ,  KEARSEY, Stephen

    IPC: B64D11/00

    CPC classification number: B64D13/00 ,  B60Q3/225 ,  B60Q3/43 ,  B64D11/0015 ,  B64D11/003 ,  B64D2011/0038 ,  Y02T50/46 ,  Y10T29/49002

    Abstract: 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 and are rotatable about 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.

    Abstract translation: 枢转仓组件被配置为接收行李并被定位在飞机的内部。 枢转仓组件包括：上部壳体，其包括强力背板以及第一和第二侧板;与上部壳体协作以限定仓内部的铲斗;与第一侧板和铲斗可操作地关联的第一枢转机构;以及 与第二侧板和铲斗可操作地相关联的第二枢转机构。 第一枢转机构和第二枢转机构沿枢转轴线轴向对齐并且可围绕枢转轴线旋转，使得桶在打开位置与关闭位置之间围绕枢转轴线相对于上部壳体枢转。

    PIVOT BIN ASSEMBLY
    28.
    发明公开
    PIVOT BIN ASSEMBLY 有权
    飞机的回转行李架安排

    公开(公告)号：EP2560874A1

    公开(公告)日：2013-02-27

    申请号：EP11772659.6

    申请日：2011-04-20

    Applicant: C&D Zodiac, Inc.

    Inventor： LEE, Nick ,  SAVIAN, Scott

    IPC: B64D11/00

    CPC classification number: B64D11/003 ,  Y02T50/46 ,  Y10T29/49826

    Abstract: A bin assembly that includes a bin housing and a bin that is pivotal between an open and a closed position within the bin housing. The bin housing includes a forward bulkhead panel, aft bulkhead panel and an aft housing panel that includes a rigid valence panel having one of a latch striker or a latch assembly secured thereto. The rigid valence panel has opposite ends that are secured to the forward and aft bulkhead panels. The bin includes an aft wall, a forward wall, a bin bottom and the other of a latch striker or a latch assembly secured to the bin bottom, thereby defining a latching location. A downward load in the bin is distributed from the latching location, along the rigid valence panel and to the aft and forward bulkhead panels.

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