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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
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。
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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
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。
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公开(公告)号：US20140192544A1
公开(公告)日：2014-07-10
申请号：US14150603
申请日：2014-01-08
Applicant: C&D Zodiac, Inc.
Inventor： Ben Orson , Zhao Jin , Christian Mecke
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。
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公开(公告)号：US20140160775A1
公开(公告)日：2014-06-12
申请号：US14102486
申请日：2013-12-10
Applicant: C&D Zodiac, Inc.
Inventor： William Wai-Loong Young , Glen A. Noda , Ian Geoffrey Scoley , Nicholas Lee
CPC classification number: F21V21/00 , B64D45/00 , B64D2045/007 , F21S45/00
Abstract: A graphics display module that includes a frame with a front portion and a rear portion that cooperate to secure a hated panel having a front surface and a rear surface therebetween. The front portion defines a central opening through which the front surface of the lighted panel can be viewed, The front portion and rear portion cooperate to define a channel that includes lighting disposed therein that is configured to back light the lighted panel.
Abstract translation: 图形显示模块，其包括具有前部和后部的框架，所述框架协作以固定具有前表面和后表面的讨厌面板。 前部分限定中心开口，照明面板的前表面可通过该中心开口被观看。前部分和后部协作以形成包括设置在其中的照明通道的通道，该通道被配置为背光点亮点亮的面板。
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公开(公告)号：US20140158826A1
公开(公告)日：2014-06-12
申请号：US14102473
申请日：2013-12-10
Applicant: C&D Zodiac, Inc.
Inventor： William Wai-Loong Young , Glen A. Noda , Ian Geoffrey Scoley , Nicholas Lee
IPC: B64D11/00
CPC classification number: B64D11/0023 , B64D11/02 , B64D11/04
Abstract: A partition configured to be positioned within an aircraft. The partition includes a first divider assembly that includes a first wall portion having a first jamb member secured to an inboard surface thereof and a first door hingedly connected to the first jamb member. The first jamb member includes first lighting that illuminates the first door, and the first door is movable between a stowed position and a deployed position. The partition also includes a second divider assembly that includes a second wall portion having a second jamb member secured to an inboard surface thereof and a second door hingedly connected to the second jamb member. The second jamb member includes second lighting that illuminates the second door, and the second door is movable between a stowed position and a deployed position. The second door is spaced apart from the first door.
Abstract translation: 配置成定位在飞行器内的分隔件。 隔板包括第一分隔件组件，该第一分隔组件包括第一壁部分，第一壁部分具有固定到其内侧表面的第一侧柱部件和铰接地连接到第一侧柱部件的第一门。 第一侧柱构件包括照亮第一门的第一照明，并且第一门可在收起位置和展开位置之间移动。 分隔件还包括第二分隔件组件，其包括具有固定到其内侧表面的第二侧柱构件的第二壁部分和铰接地连接到第二侧柱构件的第二门。 第二侧柱构件包括照亮第二门的第二照明，并且第二门可在收起位置和展开位置之间移动。 第二扇门与第一扇门隔开。
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Patent Agency Ranking
公开(公告)号：US20130208490A1
公开(公告)日：2013-08-15
申请号：US13765646
申请日：2013-02-12
Applicant: C&D ZODIAC, INC.
Inventor： Scott Savian
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。
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公开(公告)号：US07615939B2
公开(公告)日：2009-11-10
申请号：US10802277
申请日：2004-03-17
Applicant: Michael A. Halter
Inventor： Michael A. Halter
IPC: G05F1/00
CPC classification number: H05B33/0818 , H01L25/0753 , H01L2924/0002 , H01L2924/3011 , H05B33/086 , H05B33/0866 , H01L2924/00
Abstract: An LED lighting system is disclosed. The lighting system includes means to calibrate the light temperature and intensity between multiple modules in one system, or to calibrate the light temperature and intensity against a known reference standard. The lighting system may be used in many illumination applications, including the cabin sections of aircraft and watercraft.
Abstract translation: 公开了一种LED照明系统。 照明系统包括用于校准一个系统中的多个模块之间的光温度和强度的装置，或者针对已知的参考标准来校准光的温度和强度。 照明系统可用于许多照明应用，包括飞机和船只的舱室部分。
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公开(公告)号：US20070272085A1
公开(公告)日：2007-11-29
申请号：US11695538
申请日：2007-04-02
Applicant: Paul Ghassemlou , Victor Eisa , Amrik Sidhu
Inventor： Paul Ghassemlou , Victor Eisa , Amrik Sidhu
IPC: A47J31/057
CPC classification number: A47J31/005 , A47J31/4457 , A47J31/46 , A47J31/545 , A47J2203/00
Abstract: The present invention provides a beverage maker having an in-line heating assembly for heating water to make hot beverages such as coffee and tea. The heating assembly defines a flow path that runs past a plurality of heaters 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 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 aligned to shine into the container and at least one detector aligned to detect light reflected off the liquid surface within the container. A drainage assembly 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.
Abstract translation: 本发明提供一种具有用于加热水以形成诸如咖啡和茶的热饮料的在线加热组件的饮料制造机。 加热组件限定了流过多个加热器以将水加热到所需温度的流动路径。 以这种方式，饮料制造商在运行时加热水，减轻对水箱或容器的需要，从而增加了重量和尺寸的节省以及减少酿造时间。 此外，提供光学传感器组件以检测何时饮料制造商的服务容器在其内具有规定的液体容量。 传感器组件包括至少一个光源，其被对准以照射到容器中，并且至少一个检测器被对准以检测从容器内的液体表面反射的光。 还提供一种排水组件，其可将液体通过连接器端口排入飞机的废水系统或通过排水口排入排水池。
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公开(公告)号：US10781607B2
公开(公告)日：2020-09-22
申请号：US16203390
申请日：2018-11-28
Applicant: C&D ZODIAC, INC.
Inventor： Raul Rogel , Joel Anthony Vizarra , Ajay Hari , Francisco Palafox
Abstract: A handle attachment assembly that includes first and second insert members, and a handle assembly that includes a cover and a main body portion. The main body portion includes a handle portion and first and second attachment portions extending from the handle portion. The cover is removably connected to the main body portion and the main body portion and the cover cooperate to define a handle interior. The first and second attachment portions include first and second attachment members, respectively. The first attachment portion and the first insert member are secured together by a first fastener, and the second attachment portion and the second insert member are secured together by a second fastener.
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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.
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