Automated storage cabinet for trolleys, and aircraft incorporating such a cabinet
    61.
    发明授权
    Automated storage cabinet for trolleys, and aircraft incorporating such a cabinet 有权
    手推车自动存储柜,以及装有这样柜子的飞机

    公开(公告)号:US09463926B2

    公开(公告)日:2016-10-11

    申请号:US13772726

    申请日:2013-02-21

    Inventor: Bernard Guering

    CPC classification number: B65G1/06 B64D9/00 B64D11/0007 B64D11/04

    Abstract: The present invention relates to an automated storage cabinet for trolleys. It includes a device for automatically handling a single trolley with a handling basket including a vertical plate perpendicular to the waiting area, vertically movable between the floor of the waiting area and any one of the levels of the trolley storage cabinet, and two side flanks, connected to the vertical plate and provided with structure for supporting, on either side, two opposite sides of a trolley in the waiting area and for transferring the supported trolley through an opening of the predetermined compartment. The handling device can include structure for inserting the trolley into or extracting the trolley from the predetermined compartment.

    Abstract translation: 本发明涉及一种用于手推车的自动化存储柜。 它包括用于自动处理单个手推车的装置,其具有处理筐,该操纵筐包括垂直于等待区域的垂直板,可垂直地在等待区域的地板和台车存储柜的任一层之间移动,以及两个侧翼, 连接到垂直板并且设置有用于在任一侧上在等待区域中的台车的两个相对侧支撑并且用于将支撑的小车通过预定隔间的开口传送的结构。 处理装置可以包括用于将小车插入或从预定隔间提取手推车的结构。

    Device positioning two aircraft pieces relative to one another, such as a crossbeam and a fuselage frame
    62.
    发明申请
    Device positioning two aircraft pieces relative to one another, such as a crossbeam and a fuselage frame 审中-公开
    设备将两架飞机相对于彼此定位,例如横梁和机身框架

    公开(公告)号:US20150251775A1

    公开(公告)日:2015-09-10

    申请号:US14637770

    申请日:2015-03-04

    CPC classification number: B64F5/10 B64C1/061 B64C1/18 Y10T29/49622

    Abstract: A device for positioning a first piece relative to a second piece. The first piece comprises a free end with a first bore and the second piece comprises an engagement part with a second bore intended to come into correspondence with the first bore. The first and second bore are drilled to the definitive diameter thereof prior to the relative positioning thereof. The device comprises one or more positioning elements, which are able to position the first bore relative to the second bore along at least one of three geometric axes.

    Abstract translation: 一种用于相对于第二件定位第一件的装置。 第一件包括具有第一孔的自由端,并且第二件包括具有与第一孔相对应的第二孔的接合部。 在其相对定位之前,将第一和第二孔钻入其确定的直径。 该装置包括一个或多个定位元件,其能够沿三个几何轴线中的至少一个相对于第二孔定位第一孔。

    AIRCRAFT NOSE WITH COCKPIT AND AVIONICS BAY MODULES INTEGRATED THEREIN
    63.
    发明申请
    AIRCRAFT NOSE WITH COCKPIT AND AVIONICS BAY MODULES INTEGRATED THEREIN 有权
    飞机与航空航天飞机组合的航空器

    公开(公告)号:US20140175224A1

    公开(公告)日:2014-06-26

    申请号:US14138551

    申请日:2013-12-23

    Abstract: An aircraft nose comprising a primary fuselage structure, and housed inside said structure, a cockpit, and an avionics bay containing a plurality of avionics racks designed to receive electrical and/or electronic equipment. The cockpit and the avionics bay are each made in the form of a distinct module that is suitable for being installed in a single operation inside the primary fuselage structure. The use of modules for integrating in the aircraft nose makes it possible to reduce considerably the time required for fitting out the nose on the final assembly line of the aircraft.

    Abstract translation: 包括主机架结构并且容纳在所述结构内的飞行器鼻架,驾驶舱和航空电子设备舱,其包含设计成接收电和/或电子设备的多个航空电子设备架。 驾驶舱和航空电子设备舱均采用独特模块的形式,适合安装在主机身结构内的单一操作中。 使用用于集成在飞机鼻部中的模块可以大大减少在飞机的最终装配线上安装鼻子所需的时间。

    AIRCRAFT COCKPIT WITH EMERGENCY EXIT VIA A CENTRAL PANE
    64.
    发明申请
    AIRCRAFT COCKPIT WITH EMERGENCY EXIT VIA A CENTRAL PANE 有权
    飞机与紧急出口紧密联系

    公开(公告)号:US20140175220A1

    公开(公告)日:2014-06-26

    申请号:US14106113

    申请日:2013-12-13

    CPC classification number: B64D43/00 B64C1/1476 B64C1/32

    Abstract: The present invention relates to an aircraft cockpit with a double flight deck in which a central pane of a windscreen can be removed in order to at least partially clear an opening in order to constitute an emergency exit and ensure natural ventilation of the cockpit. Moreover, a central portion of a glare shield and of a flight station instrument panel are optionally moveable in order to facilitate access to the opening in the event of the need for emergency evacuation.

    Abstract translation: 本发明涉及具有双飞行甲板的飞行器驾驶舱,其中可以移除挡风玻璃的中央窗格以便至少部分地清除开口以构成紧急出口并确保驾驶舱的自然通风。 此外,眩光屏蔽和飞行台仪表板的中心部分可选地可移动,以便在需要紧急撤离的情况下方便进入开口。

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