PIVOT BIN ASSEMBLY
    111.
    发明公开
    PIVOT BIN ASSEMBLY 审中-公开

    公开(公告)号:EP3166847A1

    公开(公告)日:2017-05-17

    申请号:EP15818886.2

    申请日:2015-07-10

    Inventor: SAVIAN, Scott

    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: 一种飞机储物箱,其包括上部壳体和枢转地连接到上部壳体的铲斗,该上部壳体与上部壳体协作以限定箱内部。 该桶包括底部,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围绕枢转轴线相对于上部壳体枢转。 当储存箱安装在飞机中时,第一水平距离限定在当铲斗处于关闭位置时延伸穿过枢转轴线的第一竖直线与铲斗的前边缘之间,并且限定第二水平距离 当铲斗处于打开位置时,在第一竖直线与铲斗的前边缘之间。 第一水平距离大于第二水平距离。

    AIRCRAFT PANEL ASSEMBLY WITH REINFORCEMENT LAYERS
    112.
    发明公开
    AIRCRAFT PANEL ASSEMBLY WITH REINFORCEMENT LAYERS 审中-公开
    带有加固层的飞机面板组件

    公开(公告)号:EP3159149A1

    公开(公告)日:2017-04-26

    申请号:EP16193483.1

    申请日:2016-10-12

    Inventor: Del Pinto, James

    Abstract: A panel assembly (10) that includes at least a first upper base layer (16) made of a thermoplastic material that includes fibers therein, at least a first lower base layer (18) made of a thermoplastic material that includes fibers therein, and at least a first reinforcement layer (12) sandwiched or positioned between the first upper base layer and first lower base layer. The upper and lower surfaces of the first reinforcement layer have a smaller surface area than the upper and lower surfaces of the first upper and first lower base layers. The lower surface of the first upper base layer is welded to the upper surface of the first reinforcement layer, and the lower surface of the first reinforcement layer is welded to the upper surface of the first lower base layer.

    Abstract translation: 一种面板组件(10),其包括至少第一上基层(16)和第二上基层(16),所述第一上基层由热塑性材料制成,所述热塑性材料在其中包括纤维,至少第一下基层(18)由其中包含纤维的热塑性材料制成, 至少第一加强层(12),夹在或位于第一上基层和第一下基层之间。 第一增强层的上表面和下表面具有比第一上基层和第一下基层的上表面和下表面小的表面积。 第一上基层的下表面焊接到第一加强层的上表面,并且第一加强层的下表面焊接到第一下基层的上表面。

    SEAT SHELL AND INTEGRATED OVERHEAD STORAGE BIN
    116.
    发明公开
    SEAT SHELL AND INTEGRATED OVERHEAD STORAGE BIN 有权
    座椅和集成存储TANK的头

    公开(公告)号:EP2694371A4

    公开(公告)日:2014-12-03

    申请号:EP12767726

    申请日:2012-04-04

    Inventor: SAVIAN SCOTT

    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.

    AIRCRAFT SEATING CONFIGURATION
    117.
    发明公开
    AIRCRAFT SEATING CONFIGURATION 有权
    飞机座位配置

    公开(公告)号:EP2686242A1

    公开(公告)日:2014-01-22

    申请号:EP12843565.8

    申请日:2012-10-29

    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.

    BEVERAGE MAKER
    118.
    发明授权
    BEVERAGE MAKER 有权
    饮料泡制

    公开(公告)号:EP2001344B1

    公开(公告)日:2011-03-16

    申请号:EP07754583.8

    申请日:2007-04-02

    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.

    DUAL URINAL LAVATORY MONUMENT
    119.
    发明申请

    公开(公告)号:WO2019089217A1

    公开(公告)日:2019-05-09

    申请号:PCT/US2018/055934

    申请日:2018-10-15

    Abstract: A lavatory monument configured to be positioned in an aircraft interior that includes an enclosure that includes first, second, third and fourth walls, and defines a lavatory interior, a first lavatory compartment that includes a first urinal unit positioned therein, and a second lavatory compartment that includes a second urinal unit positioned therein. The first lavatory compartment includes a first door and the second lavatory compartment includes a second door. A divider wall separates at least a portion of the first lavatory compartment from at least a portion of the second lavatory compartment. The first door is positioned on one of the first or second walls and the second door is positioned on one of the first or third walls.

    AIRCRAFT STORAGE BIN ASSEMBLY WITH UPPER AND LOWER BINS

    公开(公告)号:WO2019070481A1

    公开(公告)日:2019-04-11

    申请号:PCT/US2018/052976

    申请日:2018-09-26

    Inventor: SAVIAN, Scott

    CPC classification number: B64D11/003

    Abstract: An aircraft overhead storage bin assembly that includes a housing, a door pivotably attached to the housing and a bucket pivotably connected to the housing that cooperates with the housing to define a bin interior. The housing includes a front, a back, and an upper storage section defined therein. The upper storage section includes an upper storage section opening that communicates the upper storage section with an exterior of the housing. The door pivotably attached to the housing and is movable between an open and a closed position. In the closed position the door closes the upper storage section opening. The bucket is positioned below the upper storage section and is pivotable with respect to the housing between an open position and a closed position.

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