公开(公告)号：WO2014008507A3

公开(公告)日：2014-01-09

申请号：PCT/US2013/049597

申请日：2013-07-08

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott ,  LONG, Eric ,  DE BOTTON, Jordan

IPC: B64C1/40

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.

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

Applicant: C & D ZODIAC INC

Inventor： SAVIAN SCOTT ,  LONG ERIC ,  DE BOTTON JORDAN

IPC: B64C1/40

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。

公开(公告)号：WO2013123064A1

公开(公告)日：2013-08-22

申请号：PCT/US2013/025956

申请日：2013-02-13

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott

IPC: G05F1/00

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。 位于PSU盒上方并连接到PSU盒的面板。 PSU舱包括至少第一和第二读取灯，其定位在舱内部，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，其配置为在壳体上方照射光。 面板包括被配置成将PSU盒组件固定到飞行器内的部件的连接器。

公开(公告)号：WO2013063599A1

公开(公告)日：2013-05-02

申请号：PCT/US2012/062474

申请日：2012-10-29

Applicant: C&D ZODIAC, INC.

Inventor： ORSON, Ben ,  JIN, Zhao

IPC: B64D11/06

CPC classification number: B64D11/06 ,  B64D11/0601 ,  B64D11/0606 ,  B64D11/0638 ,  B64D11/064 ,  B64D11/0641 ,  B64D11/0642 ,  B64D11/0643

Abstract: A passenger seating arrangement for an aircraft cabin that includes first and. second adjacent columns of at least two seats that define a first longitudinally extending center axis that extends approximately parallel to a longitudinal axis of the aircraft cabin. The seats in the first column face away from and form an angle with the first axis of between about 1 ° and about 44°, and the seats in the second column face away from and form an angle with the first axis of between about 1 ° and about 44°. Each seat in the first column is staggered fore of a seat in the second column.

Abstract translation: 飞机机舱的乘客座椅安排，包括第一和 至少两个座的第二相邻列限定了大致平行于飞机机舱的纵向轴线延伸的第一纵向延伸的中心轴线。 第一列中的座位远离第一轴线并且与第一轴线形成约1°至约44°的角度，并且第二列中的座椅面向远离第一轴线并且与第一轴线形成约1°的角度 约44°。 第一列中的每个座位在第二列的座位前面交错。

公开(公告)号：WO2010117920A1

公开(公告)日：2010-10-14

申请号：PCT/US2010/029893

申请日：2010-04-05

Applicant: C&D ZODIAC, INC. ,  LE, Gary, Tien ,  KRIKORIAN, Aram, Aris

Inventor： LE, Gary, Tien ,  KRIKORIAN, Aram, Aris

IPC: B64D11/06 ,  B60N2/68 ,  B21C37/16

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

Abstract: Tubular bodies (106, 108) for use in frames for seats of vehicles such as aircraft are described. A tube (302) 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.

Abstract translation: 描述了用于诸如飞行器的车辆座椅的框架中的管状体（106,108）。 管（302）可以包括沿着管的长度具有可变厚度的侧壁。 侧壁的可变厚度可导致管沿着管的长度具有可变的内径。 管也可以包括可变外径。

公开(公告)号：WO2007120460A3

公开(公告)日：2007-10-25

申请号：PCT/US2007/008081

申请日：2007-04-02

Applicant: C & D ZODIAC, INC. ,  GHASSEMLOU, Paul ,  EISA, Victor ,  SIDHU, Amrik, S.

Inventor： GHASSEMLOU, Paul ,  EISA, Victor ,  SIDHU, Amrik, S.

IPC: A47J31/00 ,  A47J31/34 ,  A47J31/44

Abstract: The present invention provides a beverage maker having an in-line heating assembly (12) for heating water to make hot beverages such as coffee and tea. The heating assembly defines a flow path (14) that runs past a plurality of heaters (16) for heating water to a desired temperature. In this manner, the beverage maker heats water as it travels, alleviating the need for a water tank or vessel, resulting in increased savings in weight and size, as well as reducing brew time. Additionally, an optical sensor assembly (80) is provided to detect when a serving container of the beverage maker has a prescribed capacity of liquid within it. The sensor assembly includes at least one light source (82) aligned to shine into the container and at least one detector (86) aligned to detect light reflected off the liquid surface within the container. A drainage assembly (70) is also provided that can drain liquid through either a connector port into an airplane's wastewater system or through a drainage port into a drainage sump.

公开(公告)号：WO2018136955A1

公开(公告)日：2018-07-26

申请号：PCT/US2018/014895

申请日：2018-01-23

Applicant: C&D ZODIAC, INC.

Inventor： WILLIAMS, Corey ,  HEIMBACH, Eric

IPC: B64D11/00 ,  A47B46/00 ,  B60R5/00

Abstract: A method of pivoting an aircraft storage bin that includes a bucket that pivots with respect to an upper housing. The method includes pivoting the bucket from a closed position to an intermediate position and placing weight that exceeds a predetermined weight threshold in the bucket, thereby causing the bucket to move to an open position. Movement of the bucket to the open position causes a lift assist unit to activate. A first end of the lift assist unit is connected to the bucket and a second end of the lift assist unit is connected to the upper housing. The method also includes pivoting the bucket from the open position to the closed position. The lift assist unit provides assistance as the bucket is pivoting from the open position to the closed position.

公开(公告)号：WO2018035154A1

公开(公告)日：2018-02-22

申请号：PCT/US2017/047005

申请日：2017-08-15

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott

IPC: B64D11/00 ,  F16B5/00 ,  F16B12/12

Abstract: An aircraft storage bin that includes an upper housing and a bucket that cooperate to define a bin interior. The bucket is movable with respect to the upper housing between open and closed positions and includes a bottom and right and left side panels. The bottom includes lower and upper surfaces and right and left outer edges. The right and left side panels each include a first section having a first transverse width, a second section having a second transverse width, and a transition section that is located between the first and second sections. The second transverse width is less than the first transverse width. At least a portion of the second section of each of the side panels is received in a slot defined in the upper surface of the bottom of the bucket, such that the right and left side panels extend upwardly from the bottom.

Abstract translation: 飞机储藏箱，其包括协作以限定箱内部的上部壳体和桶。 铲斗相对于上部壳体在打开和关闭位置之间可移动，并且包括底部和左右侧面板。 底部包括下表面和上表面以及右侧和左侧的外边缘。 右侧和左侧板各自包括具有第一横向宽度的第一部分，具有第二横向宽度的第二部分以及位于第一和第二部分之间的过渡部分。 第二横向宽度小于第一横向宽度。 每个侧板的第二部分的至少一部分容纳在限定在桶底部的上表面中的槽中，使得右侧板和左侧板从底部向上延伸。

公开(公告)号：WO2016049064A1

公开(公告)日：2016-03-31

申请号：PCT/US2015/051520

申请日：2015-09-22

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott ,  JIN, Zhao

IPC: B64D11/02

CPC classification number: B64D11/02 ,  B64D11/04

Abstract: A monument configured to be positioned in the interior of an aircraft that includes first, second, third and fourth sides and first and second lavatories spaced apart from one another by at least a portion of a galley storage section that is open to the first side. The first and second sides are opposite to one another and the third and fourth sides are opposite to one another. The first lavatory defines a first lavatory interior and includes a first toilet therein and the second lavatory defines a second lavatory interior and includes a second toilet therein.

Abstract translation: 纪念碑，其被配置为位于飞行器的内部，其包括第一，第二，第三和第四侧以及第一和第二盥洗室，所述第一和第二盥洗室由朝向第一侧敞开的厨房存储部分的至少一部分彼此间隔开。 第一和第二面彼此相对，第三和第四面彼此相对。 第一洗手间限定第一洗手间内部并且在其中包括第一厕所，第二洗手间限定第二卫生间内部并且在其中包括第二厕所。

公开(公告)号：WO2016007915A1

公开(公告)日：2016-01-14

申请号：PCT/US2015/040038

申请日：2015-07-10

Applicant: C&D ZODIAC, INC.

Inventor： SAVIAN, Scott

IPC: B64D11/00

CPC classification number: B64D11/003 ,  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 and first and second opposing side walls extending upwardly from the bottom and pivots about a pivot axis with respect to the upper housing between an open position and a closed position. When the storage bin is installed in an aircraft, a first horizontal distance is defined between a first vertical line that extends through the pivot axis and the front edge of the bucket when the bucket is in the closed position, and a second horizontal distance is defined between the first vertical line and the front edge of the bucket when the bucket is in the open position. The first horizontal distance is greater than the second horizontal distance.

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，前边缘以及从底部向上延伸的第一和第二相对侧壁，并且在打开位置和关闭位置之间相对于上壳体枢转枢转。 当存储箱安装在飞行器中时，当铲斗处于关闭位置时，在通过枢转轴线延伸的第一垂直线和铲斗的前边缘之间限定第一水平距离，并且定义第二水平距离 当铲斗处于打开位置时，在第一垂直线和铲斗的前边缘之间。 第一个水平距离大于第二个水平距离。