公开(公告)号：US20150375844A1

公开(公告)日：2015-12-31

申请号：US14788255

申请日：2015-06-30

Applicant: C&D ZODIAC, INC.

Inventor： Tyler Smithson ,  Rakibul Islam ,  Richard Morrison ,  Monique Le Roux ,  Aamir Jafri

IPC: B64C1/12

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，包括具有前表面，后表面和至少一个挤压部分的前表皮，包括层压在一起的第一，第二，第三，第四和第五层的芯组件以及至少第一挤压部分。 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。 芯组件的第一层的前表面包括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，第四层包括限定在其中的多个细长空隙。

公开(公告)号：US09174722B2

公开(公告)日：2015-11-03

申请号：US14589906

申请日：2015-01-05

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian ,  Eric Long ,  Jordan De Botton

IPC: G10K11/168 ,  B64C1/40 ,  B64C1/12 ,  B64C1/06 ,  G10K11/16

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向内延伸的肋构件。 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。

公开(公告)号：US20150307193A1

公开(公告)日：2015-10-29

申请号：US14794732

申请日：2015-07-08

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Ian Geoffrey Scoley

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：US20150274297A1

公开(公告)日：2015-10-01

申请号：US14668770

申请日：2015-03-25

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Ian Geoffrey Scoley ,  Eric Long

IPC: 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：US08955805B2

公开(公告)日：2015-02-17

申请号：US14179494

申请日：2014-02-12

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian ,  Stephen Kearsey ,  Corey Williams

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

CPC classification number: B64D11/003 ,  B60Q3/43 ,  B64D11/0015 ,  B64D2011/0038 ,  Y02T50/46

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 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。 第一和第二枢转机构沿着枢转轴线轴向对齐，使得该斗围绕上部壳体的枢转轴线在打开位置和关闭位置之间枢转。

公开(公告)号：US20140197721A1

公开(公告)日：2014-07-17

申请号：US14179494

申请日：2014-02-12

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian ,  Stephen Kearsey ,  Corey Williams

IPC: B64D11/00 ,  A47B46/00

CPC classification number: B64D11/003 ,  B60Q3/43 ,  B64D11/0015 ,  B64D2011/0038 ,  Y02T50/46

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 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，所述上壳体包括强背和第一和第二侧板，与所述上壳体协作以限定仓室内部的桶，与所述第一侧板和所述桶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。 第一和第二枢转机构沿着枢转轴线轴向对齐，使得该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：USD706706S1

公开(公告)日：2014-06-10

申请号：US29464727

申请日：2013-08-20

Applicant: C&D Zodiac, Inc.

Designer： Chris Schutterra ,  Bruce Shimizu

公开(公告)号：US20140123383A1

公开(公告)日：2014-05-08

申请号：US14072749

申请日：2013-11-05

Applicant: C&D Zodiac, Inc.

Inventor： Peter Detjen ,  Edward Reams ,  Christoph Goeschel

IPC: B64D11/02 ,  B64D11/04

CPC classification number: B64D11/02 ,  B64D11/04 ,  B64D2011/0046

Abstract: A modular monument assembly configured to be positioned in an aircraft that includes an enclosure that includes a first module and a second module, and a circulation system that is adapted to receive water from a water source. The circulation system includes a circulation line for circulating water, a water heater, a circulation pump, first and second faucets and first and second lines that are in fluid communication with the first and second faucets. The first faucet is positioned in the first module and the second faucet is positioned in the second module.

Abstract translation: 一种模块化纪念碑组件，其被配置为定位在包括第一模块和第二模块的外壳的飞行器中，以及适于从水源接收水的循环系统。 循环系统包括用于循环水的循环管线，热水器，循环泵，第一和第二水龙头以及与第一和第二水龙头流体连通的第一和第二管线。 第一个水龙头位于第一个模块中，第二个水龙头位于第二个模块中。

公开(公告)号：US20140014773A1

公开(公告)日：2014-01-16

申请号：US14028424

申请日：2013-09-16

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian

IPC: B64D11/00 ,  B64D11/06

CPC classification number: B64D11/003 ,  B64D11/06 ,  B64D11/0606 ,  B64D11/0641 ,  Y10T29/49826

Abstract: A lounge assembly configured to be positioned in the interior of an aircraft. The lounge assembly includes a first seat shell configured to at least partially surround a passenger seat, and an overhead storage bin assembly. The overhead storage bin assembly includes first and second posts configured to be secured to a floor of the aircraft, and an overhead bin housing supported by the first and second posts. The overhead bin housing includes at least a first overhead storage bin that is positioned generally above the first seat shell.

Abstract translation: 配置为定位在飞机内部的休息室组件。 休息室组件包括构造成至少部分地围绕乘客座椅的第一座椅外壳和顶置存储箱组件。 架空存储箱组件包括构造成固定到飞行器的地板上的第一和第二柱以及由第一和第二柱支撑的架空仓壳体。 架空仓壳体包括至少第一架空存储箱，其大致位于第一座椅壳体的上方。

公开(公告)号：US20130207529A1

公开(公告)日：2013-08-15

申请号：US13765358

申请日：2013-02-12

Applicant: C&D ZODIAC, INC.

Inventor： Stephen Kearsey ,  Richard McClure

IPC: F16F9/32 ,  A47B46/00

CPC classification number: F16F9/3207 ,  A47B46/00 ,  B64D11/003 ,  F16F9/145

Abstract: A damping mechanism that includes a housing with an inner circumferential surface defined by an assembly outer race, an axle shaft that is rotatable with respect to the housing, and a transmission assembly operatively associated with the axle shaft and disposed within the housing. The transmission assembly includes an assembly intermediate race. A fluid space that includes fluid therein is defined between the assembly intermediate race and the inner circumferential surface of the assembly outer race. A vane is disposed between the assembly intermediate race and the inner circumferential surface of the assembly outer race. The vane includes a restriction space defined therein. When the axle shaft rotates in the first direction, the transmission assembly transmits rotation from the axle shaft to the vane, and when the axle shaft rotates in the second direction, the transmission assembly transmits less rotation to the first vane than when the axle shaft rotates in the first direction.

Abstract translation: 一种阻尼机构，包括具有由组件外座圈限定的内圆周表面的壳体，可相对于所述壳体旋转的车轴;以及传动组件，其可操作地与所述车轴相关联并且设置在所述壳体内。 传动组件包括组合中间座圈。 在组件中间座圈和组件外圈的内圆周表面之间限定包括流体的流体空间。 叶片设置在组装中间座圈和组件外圈的内周面之间。 叶片包括其中限定的限制空间。 当车轴沿第一方向旋转时，传动组件将转轴从轴轴传递到叶片，并且当车轴沿第二方向旋转时，传动组件相对于第一叶片的旋转少于当车轴旋转时 在第一个方向。