公开(公告)号：US20160222654A1

公开(公告)日：2016-08-04

申请号：US15011215

申请日：2016-01-29

Applicant: C&D ZODIAC, INC.

Inventor： Bruce Shimizu ,  Scott Savian

IPC: E04B9/00 ,  B64D11/02 ,  B64C1/06 ,  F16M13/02

CPC classification number: E04B9/006 ,  B64C1/066 ,  B64D11/02 ,  E04B9/003

Abstract: A module for mounting within a ceiling panel assembly. The module includes an upper mounting frame that includes a main body portion that defines a central opening, a lower mounting frame that is at least partially received in the central opening of the upper mounting frame, and a latch assembly. The main body portion of the upper mounting frame includes a flange extending outwardly therefrom. The lower mounting frame is pivotable with respect to the upper mounting frame between a first position and a second position. The latch assembly is associated with a first end of the upper mounting frame and the lower mounting frame. When the latch assembly is released the lower mounting frame pivots from the first position to the second position.

Abstract translation: 用于安装在天花板面板组件内的模块。 模块包括上部安装框架，其包括限定中心开口的主体部分，至少部分地容纳在上部安装框架的中心开口中的下部安装框架和闩锁组件。 上安装框架的主体部分包括从其向外延伸的凸缘。 下安装框架可相对于上安装框架在第一位置和第二位置之间枢转。 闩锁组件与上安装框架和下安装框架的第一端相关联。 当闩锁组件被释放时，下安装框架从第一位置枢转到第二位置。

公开(公告)号：US09260189B2

公开(公告)日：2016-02-16

申请号：US14794732

申请日：2015-07-08

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Ian Geoffrey Scoley

IPC: B64D11/02 ,  A47K4/00 ,  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.

公开(公告)号：US09174734B2

公开(公告)日：2015-11-03

申请号：US14622377

申请日：2015-02-13

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  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.

公开(公告)号：US20150151839A1

公开(公告)日：2015-06-04

申请号：US14622377

申请日：2015-02-13

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Corey Williams

IPC: B64D11/00

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：US09045230B2

公开(公告)日：2015-06-02

申请号：US13765612

申请日：2013-02-12

Applicant: C&D ZODIAC, INC.

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

IPC: B64D11/02

CPC classification number: B64D11/02 ,  B64D11/0691

Abstract: A lavatory monument assembly configured to be positioned in the interior of an aircraft that includes a first wall and a second wall that are generally parallel to one another, and the second wall is longer than the first wall. The lavatory monument assembly further includes a third wall and a fourth wall, and the third wall and the fourth wall generally are perpendicular to the first wall and the second wall, and the third wall and the fourth wall connect to the first wall and the second wall to form a lavatory interior. The first portion of the fourth wall generally is parallel to the third wall, and a second portion of the fourth wall angles inwardly along generally straight lines into the lavatory interior, such that the area in the lavatory interior proximate the first wall is less than the area proximate the second wall. The lavatory monument assembly farther includes a toilet in the lavatory interior proximate the first wall, and it further includes a door positioned on one of the first, second, third, or fourth walls.

Abstract translation: 一种构造成定位在飞行器内部的卫生间纪念碑组件，其包括大致彼此平行的第一壁和第二壁，并且第二壁比第一壁长。 卫生间纪念碑组件还包括第三壁和第四壁，第三壁和第四壁通常垂直于第一壁和第二壁，第三壁和第四壁连接到第一壁，第二壁连接到第一壁 墙壁形成盥洗室内部。 第四壁的第一部分通常平行于第三壁，并且第四壁的第二部分沿大致直线向内倾斜进入盥洗室内部，使得靠近第一壁的盥洗室内部的区域小于 靠近第二个墙的区域。 卫生间纪念碑组件还包括靠近第一墙壁的盥洗室内部的卫生间，并且还包括位于第一，第二，第三或第四壁之一上的门。

公开(公告)号：US20140278270A1

公开(公告)日：2014-09-18

申请号：US13841840

申请日：2013-03-15

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian ,  Sandesh Shetty ,  Adam Sbeglia

IPC: G06F17/50

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行器内部布局配置的所有可能组合的列表。 第六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占据最少座位空间的一个配置的输出，至少重量，并且包含 大多数飞机机舱的存储空间。 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：US20140009950A1

公开(公告)日：2014-01-09

申请号：US13895075

申请日：2013-05-15

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian

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

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。

公开(公告)号：US20200298976A1

公开(公告)日：2020-09-24

申请号：US16899491

申请日：2020-06-11

Applicant: C&D Zodiac, Inc.

Inventor： Scott Savian

IPC: B64D11/06

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.

公开(公告)号：US10647430B2

公开(公告)日：2020-05-12

申请号：US15674342

申请日：2017-08-10

Applicant: C&D ZODIAC, INC.

Inventor： Eric Long ,  Stephen Kearsey ,  Scott Savian

IPC: B64D11/00 ,  E05B53/00 ,  E05C9/00 ,  E05C3/24 ,  E05B41/00 ,  E05B5/00 ,  E05B65/00 ,  E05C1/12 ,  E05C19/00 ,  E05B7/00 ,  E05C9/04 ,  E05B1/00

Abstract: A latch system that includes a paddle button assembly having a button that is movable between home and actuation positions, a latch assembly that includes a striker assembly with a striker and a hook assembly, and a cable that extends between the paddle button and latch assembly. The hook assembly includes a hook, a pivotal trigger arm, and a manual override switch that is movable between first and second positions when the trigger arm is moved from an engaged position to a disengaged position. Movement of the button from the home position to the actuation position pushes or pulls the cable, thereby pivoting the trigger arm from the engaged to the disengaged position and disengaging the hook from the striker. Pivotal movement of the trigger arm from the engaged to the disengaged position results in linear movement of the manual override switch from the first to the second position.

公开(公告)号：US10301025B2

公开(公告)日：2019-05-28

申请号：US15257611

申请日：2016-09-06

Applicant: C&D ZODIAC, INC.

Inventor： Scott Savian

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

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.