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    • 33. 发明申请
    • System For Contactless Power Transfer
    • 非接触式电力传输系统
    • US20130167817A1
    • 2013-07-04
    • US13778805
    • 2013-02-27
    • AIRBUS OPERATIONS GMBH
    • Hans-Achim BauerAndre Zybala
    • F02P19/02
    • F02P19/02B64D11/0624H02J5/005H02J50/10H02J50/80
    • A system for inductive contactless power transfer between a first vehicle part and at least one collector that can be variably positioned relative to the first vehicle part in a passenger cabin of a vehicle includes primary windings (P1-PN) that with secondary windings (S1, S2) on collectors or second vehicle parts can form a transducer. Depending on operating-mode switching of the vehicle, the operation of collectors is prevented, which collectors for the purpose of providing electrical power for operating external cleaning or maintenance devices are brought into the vehicle. Because of the expansion of the function of an existing contactless power and data transfer system, the system is particularly cost-effective and flexible, and in addition is of a very lightweight design.
    • 一种用于在第一车辆部分和至少一个收集器之间的感应式非接触式动力传递系统,其能够相对于车辆的客舱中的第一车辆部件可变地定位,包括:初级绕组(P1-PN),其具有次级绕组(S1, S2)在收集器或第二车辆部件上可以形成换能器。 根据车辆的操作模式切换,防止收集器的操作,为了提供用于操作外部清洁或维护装置的电力的收集器被带入车辆。 由于现有的非接触式电力和数据传输系统功能的扩大,该系统特别具有成本效益和灵活性,而且还具有非常轻便的设计。
    • 38. 发明申请
    • CONVERTIBLE PASSENGER SEAT ASSEMBLY
    • 可换乘客座椅组件
    • US20100327634A1
    • 2010-12-30
    • US12844473
    • 2010-07-27
    • Glenn A. Johnson
    • Glenn A. Johnson
    • B60N2/32B60N2/44
    • B64D11/0638B60N3/004B60N2205/30B64D11/0624B64D11/0693
    • A passenger seat assembly and method for converting the seat assembly between a three-seat configuration and a two-seat configuration includes a seat assembly base and first, second, and third seats mounted on the seat assembly base. The first and third seats define outboard seats and the second seat defines an inboard seat disposed between the outboard seats. The seat back of the inboard seat includes an upper portion movably mounted to the lower portion. The seat bottom is removable and repositionable between the three-seat configuration and the two-seat configuration to form a convenience area between the outboard seats. A power console movably mounted on the seat assembly base supports the seat bottom of the inboard seat and provides at least one power outlet for supplying electrical power. In particular, the inboard seat is convertible between a seating configuration and a non-seating configuration.
    • 一种用于将座椅组件转换成三座椅构型和双座椅配置的乘客座椅组件和方法包括座椅组件基座和安装在座椅组件基座上的第一,第二和第三座椅。 第一和第三座椅限定外侧座椅,第二座椅限定设置在外侧座椅之间的内侧座椅。 内侧座椅的座椅靠背包括可移动地安装到下部的上部。 座椅底座是可拆卸的,可在三座椅配置和双座椅配置之间重新定位,以在外侧座椅之间形成方便区域。 可移动地安装在座椅组件基座上的动力控制台支撑内侧座椅的座椅底部并且提供至少一个用于提供电力的电源插座。 特别地,内侧座椅可在座椅配置和非座椅配置之间转换。
    • 39. 发明申请
    • DEVICE FOR HOLDING LINES IN AN AIRCRAFT
    • 用于在航空器内保持线路的装置
    • US20100314505A1
    • 2010-12-16
    • US12745945
    • 2008-12-17
    • Sandra DeimerJan HarderThomas KriebischAxel KönigJean-Marie Le CorreThomas MariakArne WilhelmMarkus Fritz
    • Sandra DeimerJan HarderThomas KriebischAxel KönigJean-Marie Le CorreThomas MariakArne WilhelmMarkus Fritz
    • F16L3/08
    • H02G11/003B64D11/0624
    • The invention relates to a device for holding lines in an aircraft that comprising at least one line inlet, at least one line outlet and at least one holding space for holding at least part of a line section extending between the line inlet and the line outlet, wherein the line section has a length that is equal to or greater than the clear distance between the relevant line inlet and line outlet, and wherein the holding space comprising means for separably holding, as well as for shortening or lengthening in a reversibly guided fashion, a line end that protrudes from the line inlet and/or line outlet. Due to the devices according to the invention, lines that are individually cut to length are no longer required for connecting reconfigurable rows of passenger seats because the device according to the invention releases or takes up excess line lengths depending on the position of the rows of passenger seats.
    • 本发明涉及一种用于在航空器中保持线路的装置,其包括至少一个线路入口,至少一个线路出口和至少一个保持空间,用于保持在线路入口和线路出口之间延伸的线路段的至少一部分, 其中所述线路段具有等于或大于所述相关线路入口和线路出口之间的清除距离的长度,并且其中所述保持空间包括用于以可逆地引导的方式可分离地保持以及缩短或延长的装置, 从线入口和/或线路出口突出的线端。 由于根据本发明的装置,由于根据本发明的装置根据乘客排的位置释放或占用多余的线路长度,所以不再需要单独切割成长度的线路用于连接可重新排列的乘客座椅 座位
    • 40. 发明授权
    • Heater system for an aircraft seat
    • 飞机座椅加热系统
    • US07823967B2
    • 2010-11-02
    • US12054071
    • 2008-03-24
    • William R. ParnisCorey S. CassavantThomas A. Stuef
    • William R. ParnisCorey S. CassavantThomas A. Stuef
    • A47C7/74
    • B64D11/0626B60N2/5685B64D11/0624B64D11/0647
    • A heater system for an aircraft seat includes a first heater pad secured to the bottom seat cushion and a second heater pad secured to the back seat cushion, with both pads being under an upholstery cover. The first and second heater pads each has a body of an open cell foam material that is self flame extinguishing, and an electric resistance wire embedded in a winding pattern within the body. A control module applies a variable electric current to the electric resistance wire in each of the first and second heater pads. Preferably only the second heater pad for the back seat cushion can be activated or both the first and second heater pads can be activated. A pushbutton switch module allows the seat occupant step the control module through a sequence of different heating levels.
    • 用于飞机座椅的加热器系统包括固定到底部座垫的第一加热垫和固定到后座垫上的第二加热垫,两个垫位于装饰盖下。 第一和第二加热器垫各自具有自熄灭的开孔泡沫材料的主体,以及嵌入在主体内的卷绕图案中的电阻丝。 控制模块对第一和第二加热器垫中的每一个中的电阻线施加可变电流。 优选地,只有用于后座垫的第二加热垫可被启动,或者可以启动第一和第二加热垫。 按钮开关模块允许座椅乘员通过一系列不同的加热水平步进控制模块。