OVERHEAD STORAGE BIN LATCH SYSTEM
    2.
    发明公开

    公开(公告)号:EP3212501A4

    公开(公告)日:2018-06-06

    申请号:EP15855175

    申请日:2015-10-27

    Applicant: C&D ZODIAC INC

    CPC classification number: B64D11/003 E05B41/00 E05B53/005 E05C3/24 E05C9/00

    Abstract: A latch system that includes a paddle button assembly having a button that is movable between a home position and an actuation position, a first latch assembly that includes a first striker assembly and a first hook assembly, and a first cable that extends between the paddle button assembly and the first latch assembly. Movement of the button from the home position to the actuation position moves the first cable, thereby disengaging the first hook assembly and the first striker assembly.

    TOILET MODULE
    4.
    发明公开
    TOILET MODULE 审中-公开

    公开(公告)号:EP3122222A4

    公开(公告)日:2017-11-15

    申请号:EP15768248

    申请日:2015-03-25

    Applicant: C&D ZODIAC INC

    CPC classification number: B64D11/02

    Abstract: A toilet module attachment assembly that includes a retainer member that is adapted to be secured to a wall and a seal member. The retainer member includes a wall attachment flange and a press fit portion extending generally inwardly from the wall attachment flange. When the retainer member is secured to a wall a channel is defined between the wall and the press fit portion. The seal member includes a receiving portion having a groove defined therein and a bulge portion that is received in the channel of the retainer member.

    DOOR FOR AN AIRCRAFT
    5.
    发明专利

    公开(公告)号:CA2917564C

    公开(公告)日:2021-07-20

    申请号:CA2917564

    申请日:2014-07-11

    Abstract: A door for an aircraft includes a first panel (58) divisible into at least two first slats (64-70) that are releasable connected to one another, a first tensioning cable (100) attached between the at least two first slats, and a first tensioner (124) 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.

    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.

    AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS
    7.
    发明申请
    AIRCRAFT INTERIOR PANEL WITH ACOUSTIC MATERIALS 审中-公开
    具有声学材料的飞机内部面板

    公开(公告)号:WO2014008507A2

    公开(公告)日:2014-01-09

    申请号:PCT/US2013049597

    申请日:2013-07-08

    CPC classification number: B64C1/40 B64C1/066

    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.

    Abstract translation: 一种面板组件,其包括具有内表面和外表面的第一面板,以及具有内表面和外表面的第二面板。 第二面板包括在其中形成的多个肋构件,其向内延伸。 肋构件包括内表面和外表面。 在多个肋构件之间限定多个面板部。 面板部分包括内表面和外表面。 肋构件的内表面固定到第一面板的内表面,并且面板部分的内表面与第一面板的内表面间隔开以限定至少第一和第二空腔。

    DOOR FOR AN AIRCRAFT
    8.
    发明申请
    DOOR FOR AN AIRCRAFT 审中-公开
    飞机门

    公开(公告)号:WO2015006678A2

    公开(公告)日:2015-01-15

    申请号:PCT/US2014046327

    申请日:2014-07-11

    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。

    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.

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