公开(公告)号：WO2017099977A1

公开(公告)日：2017-06-15

申请号：PCT/US2016/062890

申请日：2016-11-18

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott ,  LONG, Eric ,  HEIMBACH, Eric

IPC: B64D11/00 ,  A47B46/00

CPC classification number: B64D11/003

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.

Abstract translation: 飞行器存储箱，其包括上部壳体和相对于上部壳体在关闭位置和打开位置之间可移动的铲斗。 上部壳体和桶配合以限定仓室内部。 该桶包括底部以及相对的第一和第二侧壁。 桶的底部包括外表面，内表面，前边缘以及突出到箱内部的第一和第二突起。 第一突起限定第一行李箱接合表面，第二突起限定第二行李箱接合表面。

公开(公告)号：WO2016122737A1

公开(公告)日：2016-08-04

申请号：PCT/US2015/057655

申请日：2015-10-27

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott

IPC: A47B46/00 ,  B64D11/00 ,  B64D13/00

CPC classification number: B64D11/003 ,  B64D2011/0053 ,  B64D2013/0625 ,  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.

Abstract translation: 一种包括上部壳体的飞行器存储箱，以及与上壳体枢转连接的铲斗，该铲斗与上壳体配合以限定箱体内部。 铲斗包括底部，前缘，从底部向上延伸的第一和第二相对的侧壁和重心。 斗在相对于上壳体的枢转轴线在打开位置和关闭位置之间枢转。 当铲斗处于关闭位置时，铲斗的重心位于枢转轴线的下方。

公开(公告)号：WO2016069558A1

公开(公告)日：2016-05-06

申请号：PCT/US2015/057513

申请日：2015-10-27

Applicant: C&D ZODIAC, INC.

Inventor： KEARSEY, Stephen ,  LONG, Eric ,  SAVIAN, Scott

IPC: B64D11/00

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.

Abstract translation: 一种闩锁系统，其包括具有可在原始位置和致动位置之间移动的按钮的桨按钮组件，包括第一撞击器组件和第一钩组件的第一闩锁组件以及在所述桨按钮之间延伸的第一线缆 组件和第一闩锁组件。 按钮从原位移动到致动位置移动第一缆线，从而使第一钩组件和第一撞针组件脱离接合。

公开(公告)号：WO2016004096A3

公开(公告)日：2016-02-18

申请号：PCT/US2015038650

申请日：2015-06-30

Applicant: C&D ZODIAC INC

Inventor： SMITHSON TYLER ,  ISLAM RAKIBUL ,  MORRISON RICHARD ,  LE ROUX MONIQUE ,  JAFRI AAMIR

IPC: B32B3/26 ,  B32B3/30 ,  B64D25/00

CPC classification number: B64C1/066 ,  B32B1/00 ,  B32B3/12 ,  B32B3/266 ,  B32B3/30 ,  B32B5/024 ,  B32B5/22 ,  B32B5/24 ,  B32B5/26 ,  B32B29/02 ,  B32B2255/26 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/101 ,  B32B2307/554 ,  B32B2307/56 ,  B32B2307/58 ,  B32B2307/5825 ,  B32B2307/72 ,  B32B2605/00 ,  B32B2605/003 ,  B32B2605/18 ,  B64D11/00 ,  B64D11/0023

Abstract: A panel assembly that includes a front skin having a front surface, a back surface and at least one crush section portion, a core assembly that includes first, second, third, fourth and fifth layers laminated together, and at least a first crush section. The first, second, third, fourth and fifth layers each include a front surface, a back surface and at least one crush section portion. The front surface of the first layer of the core assembly includes a plurality of scores defined therein. The second layer includes a plurality of elongated voids defined therein and the fourth layer includes a plurality of elongated voids defined therein.

Abstract translation: 一种面板组件，其包括具有前表面，后表面和至少一个挤压部分部分的前表皮，包括层压在一起的第一层，第二层，第三层，第四层和第五层以及至少第一挤压部分的芯组件。 第一，第二，第三，第四和第五层各自包括前表面，后表面和至少一个挤压部分部分。 芯组件的第一层的前表面包括在其中限定的多个刻痕。 第二层包括限定在其中的多个细长空隙，并且第四层包括限定在其中的多个细长空隙。

公开(公告)号：WO2015153923A1

公开(公告)日：2015-10-08

申请号：PCT/US2015/024171

申请日：2015-04-02

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott

IPC: B64D11/06

CPC classification number: B64D11/0605 ,  B64D11/0015 ,  B64D11/003 ,  B64D11/0604 ,  B64D11/0606 ,  B64D11/0624 ,  B64D11/0627

Abstract: An aircraft lounge assembly that includes an enclosure having a rear wall, first and second side walls and a forward wall that cooperate to define a seating area. The lounge assembly also includes first and second seats positioned in the seating area, and a first dividing wall positioned between the first and second seats. The first dividing wall divides the seating area into a first seat section and a second seat section. The front wall includes a shared entrance space defined therein. A first seat path is defined between the shared entrance space and the first seat section and a second seat path is defined between the shared entrance space and the second seat section.

Abstract translation: 一种飞机休息室组件，其包括具有后壁，第一和第二侧壁以及配合以限定休息区的前壁的外壳。 休息室组件还包括位于休息区中的第一和第二座位以及位于第一座椅和第二座椅之间的第一分隔壁。 第一分隔壁将休息区分为第一座椅区段和第二座椅区段。 前壁包括在其中限定的共享入口空间。 第一座位路径被限定在共享入口空间和第一座椅区段之间，并且第二座位路径被限定在共享入口空间和第二座椅区段之间。

公开(公告)号：WO2015148712A1

公开(公告)日：2015-10-01

申请号：PCT/US2015/022553

申请日：2015-03-25

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott ,  SCOLEY, Ian, Geoffrey ,  LONG, Eric

IPC: A47K11/00 ,  B64D11/00 ,  B64D11/02

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.

Abstract translation: 一种马桶模块附接组件，其包括适于固定在壁上的保持构件和密封构件。 保持器构件包括壁附接凸缘和从壁附接凸缘大致向内延伸的压配合部分。 当保持构件固定到壁上时，在壁和压配合部分之间限定通道。 密封构件包括具有限定在其中的凹槽的容纳部分和容纳在保持器构件的通道中的凸起部分。

公开(公告)号：WO2015148690A1

公开(公告)日：2015-10-01

申请号：PCT/US2015/022522

申请日：2015-03-25

Applicant: C&D ZODIAC, INC.

Inventor： MCCLURE, Richard

IPC: B64C1/00

CPC classification number: F16B2/12 ,  B64C1/066 ,  B64C1/403 ,  B64D11/02 ,  F16B2/10 ,  F16B2/185 ,  F16B5/0607 ,  F16B5/0621 ,  F16B21/065 ,  F16B21/09 ,  Y10T24/45707

Abstract: A fastener system that includes a female fastener assembly with a housing having a channel defined therein and a switch member movable within the channel between removing and fastening positions. The switch member includes a receiver portion having a post opening defined therein and a switch portion. The housing includes a lower opening. The post opening includes a removing portion that is aligned with the lower opening when the switch member is in the removing position and a fastening portion that is aligned with the post opening when the switch member is in the fastening position. The system also includes a male fastener assembly having a post with a slot therein. The post is received through the lower opening in the housing and the post opening so that the slot is aligned with the channel. The slot receives a portion of the receiver portion when the switch member is in the fastening position.

Abstract translation: 一种紧固件系统，其包括具有限定在其中的通道的壳体的阴紧固件组件和在移除和紧固位置之间的通道内可移动的开关构件。 开关构件包括具有限定在其中的柱形开口的接收器部分和开关部分。 壳体包括下开口。 后开口包括当开关构件处于移除位置时与下开口对准的移除部分和当开关构件处于紧固位置时与柱塞开口对准的紧固部分。 该系统还包括具有其中具有狭槽的柱的阳紧固件组件。 柱通过壳体中的下开口和柱开口接收，使得槽与通道对准。 当开关构件处于紧固位置时，狭槽接收接收器部分的一部分。

公开(公告)号：WO2015006678A3

公开(公告)日：2015-01-15

申请号：PCT/US2014/046327

申请日：2014-07-11

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

Inventor： GOINGS, William A. ,  LONG, Eric

IPC: B64D11/00 ,  B64C1/14

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.

公开(公告)号：WO2014143105A1

公开(公告)日：2014-09-18

申请号：PCT/US2013/042895

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的飞行器的设计布局的计算机化系统，所述系统包括第一软件模块，所述第一软件模块被配置为从 用户关于座位数; 第二软件模块，被配置为从用户接收关于座椅音高的输入; 第三软件模块，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; 第五软件模块被配置为包括用于飞行器的所有飞机内部布局配置的所有可能组合的列表。 第六个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和创建一个配置的输出，其占用最少量的座位空间，至少重量，并且包含 最大量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。

公开(公告)号：WO2014110286A1

公开(公告)日：2014-07-17

申请号：PCT/US2014/010919

申请日：2014-01-09

Applicant: C&D ZODIAC, INC.

Inventor： ORSON, Benjamin, Richard ,  JIN, Zhao ,  MECKE, Christian

IPC: B60Q3/02

CPC classification number: F21V15/012 ,  B64D11/00 ,  B64D47/02 ,  B64D2011/0053

Abstract: A lighting assembly that includes an outer housing defining an outer housing axis, an inner housing defining an inner housing axis and a light member positioned in the inner housing. The outer housing includes a front surface having a front opening and an inner surface that defines an adjustment cavity having a truncated spherical shape. The inner housing has a truncated spherical shape and is at least partially received within the adjustment cavity. The inner housing defines a light recess therein and includes a front cover having an aperture defined therein. The front cover at least partially defines the light recess. The light member defines a light axis. The light axis and the inner housing axis are not co-axial and not parallel and form an angle therebetween. The inner housing is adjustable between a home position and a plurality of adjustment positions.

Abstract translation: 一种照明组件，其包括限定外部壳体轴线的外部壳体，限定内部壳体轴线的内部壳体和定位在所述内部壳体中的轻型构件。 外壳包括具有前开口的前表面和限定具有截头球形的调节空腔的内表面。 内壳体具有截头球形并且至少部分地容纳在调节空腔内。 内壳体在其中限定一个光凹槽，并且包括其中限定有孔的前盖。 前盖至少部分地限定光凹部。 光构件限定光轴。 光轴和内壳体轴线不是同轴的并且不平行并且在它们之间形成一个角度。 内壳体在原位置和多个调节位置之间是可调节的。