Aircraft cabin dividing device
    1.
    发明授权
    Aircraft cabin dividing device 失效
    飞机舱分隔装置

    公开(公告)号:US5393013A

    公开(公告)日:1995-02-28

    申请号:US982860

    申请日:1992-11-30

    IPC分类号: B64D11/00 E04B2/74

    CPC分类号: B64D11/0023

    摘要: An aircraft cabin divider is so constructed that its installation can easily be handled by one person taking advantage of the force of gravity. For this purpose the divider has a frame with a first plug-in section that cooperates with a second socket section in the cabin structure, for example, the cabin floor or the cabin seating structure. The plug-in and socket sections cooperate so that an automatic lock-in is accomplished or so that a slight turn will provide the required interlocking. At least two couplings each including a plug-in section and a socket section are provided.

    摘要翻译: 飞机舱分隔件的构造使得其安装可以容易地由一个人利用重力的力量来处理。 为此,分隔器具有框架,其具有第一插入部分,其与机舱结构中的第二插座部分(例如,机舱地板或客舱座椅结构)协作。 插件和插座部分协作,以便实现自动锁定,或者轻微的转动将提供所需的互锁。 提供至少两个联接器,每个联接器包括插入部分和插座部分。

    Floor system for a fuselage airframe of an aircraft
    2.
    发明授权
    Floor system for a fuselage airframe of an aircraft 有权
    飞机机身机身的地板系统

    公开(公告)号:US08074928B2

    公开(公告)日:2011-12-13

    申请号:US12842769

    申请日:2010-07-23

    IPC分类号: B64C1/18

    摘要: A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as primary structure. Consequent to the free or self-supporting design of the floor system in the fuselage cell, the layout of the floor system along an aircraft axis can be matched to customer specifications in a simple manner without reference to structural boundary conditions of the fuselage structure. A floor surface for the floor system is formed from a number of floor elements which can be fitted with functional elements, wherein filling of empty spaces or cavities can be achieved with a number of floor equalization elements. As the floor elements have a relatively large support or fixing surface the loads induced by the functional elements are introduced into the floor system distributed over a large area such that the structural components thereof can be of a structurally lighter and thus weight-saving size.

    摘要翻译: 提供飞机机身部分的地面系统。 地板系统具有基本上自支撑的设计,并且基本上机械地与作为主结构的机身部分分离。 由于机身单元中的地板系统的自由或自支撑设计,沿着飞行器轴线的地板系统的布局可以以简单的方式与客户规格相匹配,而不参考机身结构的结构边界条件。 用于地板系统的地板表面由许多可装配有功能元件的地板元件形成,其中可以利用多个地板均衡元件来实现空的空间或空腔的填充。 由于地板元件具有相对较大的支撑或固定表面,所以由功能元件引起的载荷被引入到分布在大面积上的地板系统中,使得其结构部件可以具有结构上较轻且因此减轻重量的尺寸。

    FUEL TANK FOR A MOTOR VEHICLE
    4.
    发明申请
    FUEL TANK FOR A MOTOR VEHICLE 审中-公开
    燃油车用于汽车

    公开(公告)号:US20070204920A1

    公开(公告)日:2007-09-06

    申请号:US11669562

    申请日:2007-01-31

    IPC分类号: B60K15/035

    摘要: The invention concerns a fuel tank (1) for a motor vehicle comprising a filler connection (2) enclosing a tank refueling passage (11) and operational and tank refueling venting conduits (3, 4) which are connected to a filler head (6) of the filler connection (2), wherein the filler head (6) has at least one change-over switching valve (9) which in a first switching position (tank refueling position) opens a flow path from the tank refueling venting conduit (3) to a fuel vapor filter and closes a connection of the operational venting conduit (4) to the tank refueling passage (11), and which in a second switching position (operational position) opens the connection of the operational venting conduit (4) to the tank refueling passage (11) and closes the flow path from the tank refueling venting conduit (3) to the fuel vapor filter. The fuel tank according to the invention is distinguished in that the operational venting means is connected to the fuel vapor filter primarily by way of the change-over switching valve (9), wherein the change-over switching valve opens the flow path from the operational venting conduit (4) to the fuel vapor filter in the second switching position and closes same in the first switching position (FIG. 1).

    摘要翻译: 本发明涉及一种用于机动车辆的燃料箱(1),其包括封闭加油通道(11)的填充连接(2)和连接到填料头(6)的操作和罐加油排放管道(3,4) ,其中所述加注头(6)具有至少一个切换切换阀(9),所述切换切换阀(9)在第一切换位置(油箱加油位置)打开来自所述加油通道导管(3)的流动路径 )连接到燃料蒸气过滤器并且关闭操作通风管道(4)到加油槽(11)的连接,并且在第二切换位置(操作位置)中,将操作排气管道(4)连接到 该罐加油通道(11)并且关闭从加油通气导管(3)到燃料蒸汽过滤器的流动路径。 根据本发明的燃料箱的特征在于,主要通过转换切换阀(9)将操作排气装置连接到燃料蒸汽过滤器,其中转换切换阀从操作开启流动路径 在第二切换位置将燃气蒸气过滤器排气到第一切换位置(图1)。

    Luggage Retention Device and Seat with Such a Luggage Retention Device
    5.
    发明申请
    Luggage Retention Device and Seat with Such a Luggage Retention Device 审中-公开
    具有行李保持装置的行李保持装置和座椅

    公开(公告)号:US20070152480A1

    公开(公告)日:2007-07-05

    申请号:US11618303

    申请日:2006-12-29

    IPC分类号: A47C7/62

    摘要: A luggage retention device may be affixed underneath a seat area of a passenger seat and includes an upper element and a lower element which may be made of flexible materials. The upper element in the region of a backrest of the passenger seat is spaced apart from the lower element to form a raised part, and in the region of a front edge of a seat area contacts the lower element to form a part of the luggage retention device, the part being arranged so as to be lying substantially flat.

    摘要翻译: 行李保持装置可以固定在乘客座椅的座位区域的下面,并且包括可由柔性材料制成的上部元件和下部元件。 乘客座椅的靠背区域中的上部元件与下部元件间隔开以形成凸起部分,并且在座位区域的前边缘的区域中接触下部元件以形成行李保持件的一部分 装置,该部分被布置成基本平坦。

    Passenger chair with a convenience device
    6.
    发明授权
    Passenger chair with a convenience device 有权
    乘客椅带便利设备

    公开(公告)号:US06601913B2

    公开(公告)日:2003-08-05

    申请号:US09804536

    申请日:2001-03-09

    IPC分类号: A47C762

    摘要: A passenger chair or a group of passenger chairs, particularly in an aircraft cabin, is equipped with a convenience device that includes an open storage bail which can hold only flat articles but not waste material, and a waste container for holding waste material but not flat articles. The storage bail and waste container form either a mounting unit or retrofit kit or are separate components. In both instances the mounting unit and the separate components are secured to a back facing area of a chair or group of chairs. The separate components are preferably so constructed that individual retrofit kits are provided.

    摘要翻译: 乘客椅或一组乘客椅,特别是在飞机机舱中,配备有便利装置,该便利装置包括可容纳平坦物品而不是废料的露天储藏箱,以及用于容纳废料而不是平的废物容器 文章。 储存保释和废物容器形成安装单元或改装套件,也可以是单独的部件。 在这两种情况下,安装单元和单独的部件固定到椅子或一组椅子的面向后的区域。 单独的部件优选地被构造成提供单独的改装套件。

    System and method for detecting data extrusion in software applications

    公开(公告)号:US10025688B2

    公开(公告)日:2018-07-17

    申请号:US13621379

    申请日:2012-09-17

    摘要: Comprehensive techniques identify data leaks in software applications using Asset Flow Analysis (AFA) to determine whether critical data leaves a system through an exit point such that the data is no longer protected by mechanisms of the system. A novel data extrusion mechanism makes use of a relevant subset of all the possible data paths detected by AFA using a knowledge base of critical business functions and critical database content. The system checks if any code performs read access to critical business data and subsequently transfers this data beyond the control limits of the target system. The knowledge base can be extended by configuring which database content is to be regarded as critical in any given organization. The approach is particularly valuable in protecting systems that manipulate, distribute, or store sensitive information associated with financial, business, or personal data, including SAP® ABAP™ software applications.

    Telescopic stowage bin
    9.
    发明授权
    Telescopic stowage bin 有权
    伸缩式装载箱

    公开(公告)号:US07922119B2

    公开(公告)日:2011-04-12

    申请号:US11618290

    申请日:2006-12-29

    IPC分类号: B64D11/00

    CPC分类号: B64D11/003 Y02T50/46

    摘要: A stowage bin arrangement for fastening a stowage bin for an aircraft, includes a stowage bin unit with a first direction of extension. The stowage bin unit may be fastened to an aircraft structure and be designed such that the stowage bin unit is capable of being telescopically extended along the first direction of extension.

    摘要翻译: 用于紧固用于飞行器的存放箱的存放箱装置包括具有第一延伸方向的装载箱单元。 装载箱单元可以被紧固到飞机结构,并且被设计成使得该装载箱单元能够沿着第一延伸方向伸缩地延伸。

    SEAT DEVICE FOR AN AIRCRAFT
    10.
    发明申请
    SEAT DEVICE FOR AN AIRCRAFT 有权
    用于飞机的座椅装置

    公开(公告)号:US20080099608A1

    公开(公告)日:2008-05-01

    申请号:US11873474

    申请日:2007-10-17

    IPC分类号: B64D11/06

    摘要: The present invention relates to a seat device for an aircraft. The seat device comprises a seat installation and a shell structure. In this arrangement the inside of the shell structure comprises an enclosed stowage space, wherein the shell structure is designed to attach the seat installation to a floor structure. In this arrangement the enclosed stowage space is designed to accommodate an item of baggage.

    摘要翻译: 本发明涉及一种用于飞行器的座椅装置。 座椅装置包括座椅安装件和壳体结构。 在这种布置中,壳体结构的内部包括封闭的堆放空间,其中壳体结构被设计成将座椅安装件附接到地板结构。 在这种安排中,封闭的装载空间被设计成容纳一件行李。