公开(公告)号：US20170008630A1

公开(公告)日：2017-01-12

申请号：US15257611

申请日：2016-09-06

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian

IPC: B64D11/02

CPC classification number: B64D11/02 ,  A47K4/00 ,  B64D11/003 ,  B64D11/0641 ,  B64D11/0691 ,  B64D2011/0046 ,  B64D2231/025 ,  Y10T29/49826

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.

Abstract translation: 一个模块化的盥洗室纪念碑组件，被配置为定位在飞行器的内部。 模块化盥洗室纪念碑集合包括第一，第二，第三和第四墙壁，其协作形成限定盥洗室内部的外壳。 第四壁包括从其向外延伸的壁龛。 组件还包括定位在凹室中的水槽模块，位于凹室中的水槽模块上方的反射镜模块以及位于第二或第三壁之一上的门。

公开(公告)号：US09527591B2

公开(公告)日：2016-12-27

申请号：US14184653

申请日：2014-02-19

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian ,  Ian Geoffrey Scoley

IPC: B64D11/02 ,  A47K4/00 ,  B64D11/06 ,  B64D11/00

CPC classification number: B64D11/02 ,  A47K4/00 ,  B64D11/003 ,  B64D11/0641 ,  B64D11/0691 ,  B64D2011/0046 ,  B64D2231/025 ,  Y10T29/49826

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.

Abstract translation: 一个模块化的盥洗室纪念碑组件，被配置为定位在飞行器的内部。 模块化盥洗室纪念碑集合包括第一，第二，第三和第四墙壁，其协作形成限定盥洗室内部的外壳。 第四壁包括从其向外延伸的壁龛。 组件还包括定位在凹室中的水槽模块，位于凹室中的水槽模块上方的反射镜模块以及位于第二或第三壁之一上的门。

公开(公告)号：US20160176527A1

公开(公告)日：2016-06-23

申请号：US15058907

申请日：2016-03-02

Applicant: C&D Zodiac, Inc.

Inventor： Gary Tien Le ,  Aram Aris Krikorian

IPC: B64D11/06

CPC classification number: B64D11/0648 ,  B60N2/68 ,  B60R21/026 ,  B64D11/06 ,  B64D11/0649 ,  B64D11/0696

Abstract: Tubular bodies for use in frames for seats of vehicles such as aircraft are described. A tube can include a sidewall that has a variable thickness along the length of the tube. The variable thickness of the sidewalls can result in the tube having a variable inner diameter along the length of the tube. The tube may also include a variable outer diameter.

公开(公告)号：US20160122021A1

公开(公告)日：2016-05-05

申请号：US14993929

申请日：2016-01-12

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Ian Geoffrey Scoley ,  Ralph Burrows ,  Christoph Goeschel ,  John Higgins ,  Thomas Lee ,  Herman Schotte

IPC: B64D11/02 ,  B64D11/06

CPC classification number: B64D11/02 ,  A47K4/00 ,  B64D11/003 ,  B64D11/0641 ,  B64D11/0691 ,  B64D2011/0046 ,  B64D2231/025 ,  Y10T29/49826

Abstract: A 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 enclosure that defines a lavatory interior, a door positioned on one of the first, second, third, or fourth walls, and an opening on the fourth side that is open to an exterior of the enclosure. A seat is at least partially positioned in the opening. The seat includes a seat back and a seat portion that is pivotal between a storage position and a deployed position. In the deployed position the seat portion extends outside of the opening.

Abstract translation: 构造成定位在飞机内部的盥洗室纪念碑组件。 模块化盥洗室纪念碑装置包括第一，第二，第三和第四墙壁，其协作形成限定盥洗室内部的外壳，位于第一，第二，第三或第四壁之一上的门，以及第四侧上的开口 这是通向外壳的外部。 座椅至少部分地位于开口中。 该座椅包括座椅靠背和在存放位置和展开位置之间枢转的座椅部分。 在展开位置，座部分延伸到开口的外侧。

公开(公告)号：US20160114889A1

公开(公告)日：2016-04-28

申请号：US14923905

申请日：2015-10-27

Applicant: C&D ZODIAC, INC.

Inventor： Stephen Kearsey ,  Eric Long ,  Scott Savian

IPC: B64D11/00 ,  E05C9/00 ,  E05C1/12 ,  A47B46/00 ,  E05C19/00

CPC classification number: B64D11/003 ,  A47B46/005 ,  B64D11/0015 ,  B64D2011/0038 ,  E05B41/00 ,  E05B53/00 ,  E05B53/003 ,  E05B53/005 ,  E05C1/12 ,  E05C3/24 ,  E05C9/00 ,  E05C19/00 ,  Y02T50/46 ,  Y10S292/37

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：US09279438B2

公开(公告)日：2016-03-08

申请号：US14540195

申请日：2014-11-13

Applicant: C&D ZODIAC, INC.

Inventor： Darmo Tandjung ,  Tyler Smithson

IPC: F16B5/06 ,  F16B11/00

CPC classification number: F16B5/0614 ,  F16B11/006 ,  Y10T29/49895 ,  Y10T29/49966

Abstract: A bracket that includes a main body portion having a first portion and a second portion that form a first angle therebetween. The first portion includes opposing front and rear surfaces and the second portion includes opposing upper and lower surfaces. The first portion includes a fastener opening defined therethrough, the second portion includes an insert feature extending from the lower surface, and the second portion includes at least one adhesive opening defined therethrough.

Abstract translation: 一种支架，其包括具有第一部分的主体部分和在它们之间形成第一角度的第二部分。 第一部分包括相对的前表面和后表面，而第二部分包括相对的上表面和下表面。 第一部分包括限定在其中的紧固件开口，第二部分包括从下表面延伸的插入件，并且第二部分包括至少一个通过其限定的粘合剂开口。

公开(公告)号：US20150354610A1

公开(公告)日：2015-12-10

申请号：US14668627

申请日：2015-03-25

Applicant: C&D ZODIAC, INC.

Inventor： Richard McClure

IPC: F16B2/12 ,  F16B5/06 ,  F16B2/10

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：US09162617B2

公开(公告)日：2015-10-20

申请号：US13765652

申请日：2013-02-12

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Stephen Kearsey

IPC: B64D11/00 ,  B60Q3/02 ,  A47B46/00 ,  B64D13/00

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: 枢轴箱组件，其构造成接收行李并定位在飞行器的内部。 所述枢轴箱组件包括上壳体，所述上壳体包括强力和第一和第二侧板，与所述上壳体配合以限定箱体内部的铲斗，与所述第一侧板和所述铲斗可操作地相关联的第一枢转机构，以及 第二枢转机构可操作地与第二侧板和铲斗相关联。 第一枢转机构和第二枢转机构沿着枢轴对准并且可以围绕枢转轴线旋转，使得所述挖斗围绕枢转轴线相对于上壳体在打开位置和关闭位置之间枢转。

公开(公告)号：US20150210393A1

公开(公告)日：2015-07-30

申请号：US14677865

申请日：2015-04-02

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian

IPC: B64D11/06 ,  B64D11/00

CPC classification number: B64D11/0601 ,  B64D11/0015 ,  B64D11/003 ,  B64D11/0606 ,  B64D11/0641 ,  Y10T29/49826

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：US09079528B2

公开(公告)日：2015-07-14

申请号：US13765646

申请日：2013-02-12

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian

IPC: B60Q3/02 ,  B64D11/00 ,  A47B46/00 ,  B64D13/00

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

Abstract: A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.

Abstract translation: 被配置为定位在飞行器内部的PSU舱组件。 PSU盒组件包括PSU盒，其包括壳体，壳体包括顶部，底部以及第一，第二，第三和第四侧，其协作以限定荚内部和位于PSU荚上方并连接到PSU荚的面板。 PSU舱包括至少位于舱内部的第一和第二读取灯，其被配置成将光照射在壳体下方，并且定位在壳体上或壳体中的舱灯，该灯被配置为在壳体上方照射光。 该面板包括被配置为将PSU盒组件固定到飞行器内的组件的连接器。