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    PIVOT BIN ASSEMBLY
    52.
    发明公开
    PIVOT BIN ASSEMBLY 审中-公开

    公开(公告)号：EP3590836A1

    公开(公告)日：2020-01-08

    申请号：EP19194309.1

    申请日：2015-07-10

    Applicant: C&D Zodiac, Inc.

    Inventor： Savian, Scott

    IPC: B64D11/00

    Abstract: An aircraft storage bin comprises 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. 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.

    PIVOT BIN ASSEMBLY
    57.
    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
    58.
    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.

    INTEGRATED CENTERLINE LAVATORY GALLEY MONUMENT
    59.
    发明公开
    INTEGRATED CENTERLINE LAVATORY GALLEY MONUMENT 审中-公开

    公开(公告)号：EP3197776A4

    公开(公告)日：2018-03-28

    申请号：EP15844241

    申请日：2015-09-22

    Applicant: C&D ZODIAC INC

    Inventor： SAVIAN SCOTT ,  JIN ZHAO

    IPC: B64D11/02 ,  B64D11/04

    CPC classification number: B64D11/02 ,  B64D11/04

    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.

    DESIGN OPTIMIZER SYSTEM AND METHODS
    60.
    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.

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