MODULAR LAVATORY WITH ALCOVE
    31.
    发明专利

    公开(公告)号:CA2900394C

    公开(公告)日:2018-05-15

    申请号:CA2900394

    申请日:2014-02-19

    Applicant: C&D ZODIAC INC

    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.

    PIVOT BIN ASSEMBLY
    32.
    发明专利

    公开(公告)号:CA2859823C

    公开(公告)日:2017-01-17

    申请号:CA2859823

    申请日:2013-02-13

    Applicant: C&D ZODIAC INC

    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.

    DESIGN OPTIMIZER SYSTEM
    33.
    发明专利

    公开(公告)号:CA2903719A1

    公开(公告)日:2014-09-18

    申请号:CA2903719

    申请日:2013-05-28

    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.

    MODULAR LAVATORY WITH ALCOVE
    34.
    发明专利

    公开(公告)号:CA2997127A1

    公开(公告)日:2014-08-28

    申请号:CA2997127

    申请日:2014-02-19

    Applicant: C&D ZODIAC INC

    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.

    AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS

    公开(公告)号:CA2878487A1

    公开(公告)日:2014-01-09

    申请号:CA2878487

    申请日:2013-07-08

    Abstract: 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.

    СИСТЕМА И СПОСОБЫ РАБОТЫ ОПТИМИЗАТОРА КОНСТРУКЦИИ

    公开(公告)号:RU2717049C2

    公开(公告)日:2020-03-17

    申请号:RU2017133946

    申请日:2016-03-02

    Applicant: C&D ZODIAC INC

    Abstract: Компьютеризированнаясистемадляопределениякомпоновкиэлементоввоздушногосудна. Системавключаетв себямодульввода, выполненныйс возможностьюприниматьпервыевходныеданные, указывающиепервоезначениепервогопараметра, первуюбазуданныхпризнаков, котораявключаетв себямножествонастроекпризнаков, модульпоискапризнаков, выполненныйс возможностьювыполнятьпоискв первойбазеданныхпризнакови выбиратьнастройкупризнаканаосновепервогозначенияпервогопараметра, центральнуюбазуданных, котораявключаетв себямножествоправил, регулирующихконструктивнуюкомпоновкуфюзеляжа, имодульоптимизации, поддерживающийсвязьс центральнойбазойданныхи выполненныйс возможностьюформироватьоптимальнуюкомпоновкунаосновевыбраннойнастройкипризнака. 4 н. и 5 з.п. ф-лы, 40 ил.

    СИСТЕМА ЗАЩЕЛОК ВЕРХНЕГО БАГАЖНОГО ОТСЕКА

    公开(公告)号:RU2669496C1

    公开(公告)日:2018-10-11

    申请号:RU2017118331

    申请日:2015-10-27

    Applicant: C&D ZODIAC INC

    Abstract: Изобретение, вобщем, относитсяк системезащелок, аболееконкретнок системезащелокдляверхнегобагажногоотсекав воздушномсудне. Системазащелоквключаетв себяузелкнопки-лопатки, узелпервойзащелкии первыйкабель. Узелкнопки-лопаткисодержиткнопку, подвижнуюмеждуисходнойпозициейи позициейдляприведенияв действие. Перваязащелкавключаетв себяузелпервогоязычкаи узелпервогокрюка. Первыйкабельпроходитмеждуузломкнопки-лопаткии узломпервойзащелки. Приэтомузлыкнопки-лопаткии первогокрюкасвязаныс однимизполкии верхнегокорпуса, аузелпервогоязычкасвязанс другимизполкии верхнегокорпуса. Перемещениекнопкиизисходнойпозициив позициюдляприведенияв действиеперемещаетпервыйкабель, расцепляязасчетэтогоузелпервогокрюкаи узелпервогоязычка. Техническимрезультатомявляетсяповышениебезопасностиприиспользовании. 3 н. и 21 з.п. ф-лы, 11 ил.

    STORAGE BIN WITH LUGGAGE POSITIONING PROTRUSIONS

    公开(公告)号:CA3003753A1

    公开(公告)日:2017-06-15

    申请号:CA3003753

    申请日:2016-11-18

    Applicant: C&D ZODIAC INC

    Abstract: An aircraft storage bin that includes an upper housing, and a bucket movable with respect to the upper housing between a closed position and an open position. The upper housing and the bucket cooperate to define a bin interior. The bucket includes a bottom and first and second opposing side walls. The bottom of the bucket includes an outer surface, an inner surface, a front edge, and first and second protrusions protruding into the bin interior. The first protrusion defines a first luggage engaging surface and the second protrusion defines a second luggage engaging surface.

    PIVOT BIN ASSEMBLY WITH MINIMAL FORCE REQUIRED FOR CLOSING

    公开(公告)号:CA2973070A1

    公开(公告)日:2016-08-04

    申请号:CA2973070

    申请日:2015-10-27

    Applicant: C&D ZODIAC INC

    Inventor: SAVIAN SCOTT

    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.

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