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公开(公告)号：US20150307192A1
公开(公告)日：2015-10-29
申请号：US14796829
申请日：2015-07-10
Applicant: C&D Zodiac, Inc.
Inventor： Scott Savian
IPC: B64D11/00
CPC classification number: B64D11/003 , B60Q3/43 , B64D11/0015 , B64D2011/0038 , B64D2011/0046 , B64D2011/0053 , 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。
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公开(公告)号：US09079668B2
公开(公告)日：2015-07-14
申请号：US13765396
申请日：2013-02-12
Applicant: C&D ZODIAC, INC.
Inventor： Kyle Gee , Marisa Ouchi , Nicholas Lee , Scott Savian
Abstract: A monument assembly configured to be positioned interior of an aircraft that includes a galley module, a first lavatory module and a second lavatory module. The module is positioned between the first and second lavatory modules, and the first lavatory module and the galley module share a first inboard dividing wall that includes at least a first non-vertical wall section.
Abstract translation: 配置为位于飞行器内部的纪念碑组件，其包括厨房模块，第一卫生间模块和第二卫生间模块。 模块位于第一和第二洗手间模块之间，并且第一洗手间模块和厨房模块共享包括至少第一非垂直壁部分的第一内侧分隔壁。
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公开(公告)号：US20150174881A1
公开(公告)日：2015-06-25
申请号：US14577398
申请日：2014-12-19
Applicant: C&D ZODIAC, INC.
Inventor： Michael O. Stoll , Thomas J. Grobelny , Matthew S. Taylor
CPC classification number: B32B3/12 , B29C53/285 , B29C65/3612 , B29C65/4815 , B29C65/4855 , B29C66/1312 , B29C66/438 , B29C66/73118 , B29C66/73921 , B29D99/0089 , B29L2031/608 , B31D3/0223 , B31D3/0292 , B32B3/28 , B32B5/24 , B32B7/12 , B32B9/005 , B32B27/08 , B32B2262/101 , B32B2605/18 , Y10T156/1025 , Y10T428/24149
Abstract: A method of bonding a first corrugated sheet and a second corrugated sheet to provide a honeycomb core assembly. The first corrugated sheet includes a plurality of lower node regions and the second corrugated sheet includes a plurality of upper node regions. The method includes applying a radio frequency activatable adhesive to one or both of a first lower node region of the first corrugated sheet and a first upper node region of the second corrugated sheet, positioning the first corrugated sheet adjacent to or in contact with the second corrugated sheet at the first upper node region and the first lower node region, and exposing the radio frequency activatable adhesives to a radio frequency to activate the radio frequency activatable adhesive, such that the first corrugated sheet is bonded to the second corrugated sheet.
Abstract translation: 一种接合第一波纹片和第二波纹片以提供蜂窝芯组件的方法。 第一波纹片包括多个下部节点区域，第二波纹片材包括多个上部节点区域。 该方法包括将无线电频率可激活的粘合剂施加到第一波纹片的第一下部节点区域和第二波纹片材的第一上部节点区域中的一个或两个上，将第一波纹片材与第二波纹片材相邻或接触地定位 在第一上部节点区域和第一下部节点区域处的片材，并且将射频激活的粘合剂暴露于射频以激活射频激活的粘合剂，使得第一波纹片材结合到第二波纹片材。
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公开(公告)号：US08899390B2
公开(公告)日：2014-12-02
申请号：US13765358
申请日：2013-02-12
Applicant: C&D Zodiac, Inc.
Inventor： Stephen Kearsey , Richard McClure
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，以及与所述车轴一起操作地配置并设置在所述壳体内的变速器组件。 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。
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公开(公告)号：US20140196206A1
公开(公告)日：2014-07-17
申请号：US14184653
申请日：2014-02-19
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。
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Patent Agency Ranking
公开(公告)号：US20130292989A1
公开(公告)日：2013-11-07
申请号：US13939247
申请日：2013-07-11
Applicant: C&D ZODIAC, INC.
Inventor： Gary Tien Le , Aram Aris Kirkorian
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.
Abstract translation: 描述了用于诸如飞机的车辆座椅的框架中的管状体。 管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。
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公开(公告)号：US20130106156A1
公开(公告)日：2013-05-02
申请号：US13662225
申请日：2012-10-26
Applicant: C&D Zodiac, Inc.
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.
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公开(公告)号：US20130105627A1
公开(公告)日：2013-05-02
申请号：US13665476
申请日：2012-10-31
Applicant: C&D ZODIAC, INC.
Inventor： Ben Orson , Elijah Dobrusin
IPC: B64D11/00
CPC classification number: B64D11/00 , B64D11/0601
Abstract: An aircraft that includes a cabin that has a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough, a first door positioned fore of the first class section, an economy class section positioned in the interior and aft of the first class section, and a longitudinally extending second aisle that extends parallel to the first aisle and that does not extend through the first class section. An economy class passenger that enters through the first door travels down the second aisle to enter the economy class section and never enters the first class section.
Abstract translation: 一种飞机，其包括具有地板，侧壁，天花板和内部的舱室，位于内部的第一类部分，其包括延伸穿过其中的纵向延伸的第一通道，位于第一类部分前方的第一门， 经济舱部分位于第一类部分的内部和后部，以及纵向延伸的第二通道，其平行于第一通道延伸并且不延伸穿过第一类部分。 通过第一个门进入的经济舱乘客从第二个通道行进，进入经济舱，不得进入第一类。
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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.
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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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