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    • 2. 发明授权
    • Method of monitoring aircraft cabin systems
    • 监控飞机机舱系统的方法
    • US07506272B2
    • 2009-03-17
    • US10713224
    • 2003-11-17
    • Kirsten KopitzkeMartin FreyJoerg HolstChristian Riedel
    • Kirsten KopitzkeMartin FreyJoerg HolstChristian Riedel
    • G06F3/048G06F3/00
    • B64D11/00Y02T50/46Y10S715/97
    • A method of monitoring and controlling aircraft cabin systems using a user interface having a touch sensitive display and a plurality of input keys corresponding to the systems. One of the input keys corresponding to a first aircraft cabin system is activated to display a first system graphical menu having status information and operating functions of the first system, and a touch sensitive input area of the first system graphical menu is touched to perform selection or control of the first system. Another one of the input keys corresponding to a second aircraft cabin system can be activated to display a second system graphical menu having status information and operating functions of the second system, and a touch sensitive input area of the second system graphical menu can be touched to perform selection and control of the second system.
    • 一种使用具有触敏显示器的用户界面和对应于该系统的多个输入键来监视和控制飞机机舱系统的方法。 对应于第一飞行器舱系统的输入键之一被激活以显示具有第一系统的状态信息和操作功能的第一系统图形菜单,并且触摸第一系统图形菜单的触敏输入区以执行选择或 控制第一个系统。 可以激活对应于第二飞行器舱系统的另一个输入键,以显示具有第二系统的状态信息和操作功能的第二系统图形菜单,并且可以将第二系统图形菜单的触敏输入区域触及 执行第二系统的选择和控制。
    • 9. 发明授权
    • Device for the electrical and mechanical connection of two printed circuit boards
    • 用于两个印刷电路板的电气和机械连接的装置
    • US06435881B1
    • 2002-08-20
    • US09868675
    • 2001-12-06
    • Walter ZeinRalf SchmidMartin Frey
    • Walter ZeinRalf SchmidMartin Frey
    • H01R1200
    • H01R12/772H01R4/4809H01R12/721H01R12/79H05K3/326
    • A device for the electrical and mechanical connection of a first, preferably elastically flexible printed circuit board to a second printed circuit board wherein an electrically conductive contact pin, protruding from the second printed circuit board and projecting through an opening in the first printed circuit board, is electrically conductively connected to a conductor track of the first printed circuit board. The device further includes an electrically conductive clamping part with elastically flexible protrusions embodied on it that embrace the contact pin by nonpositive engagement, and a bearing region of the clamping part that is electrically connected to the protrusions is pressed in prestressed fashion against a conductor track disposed on the first printed circuit board.
    • 一种用于将第一优选弹性柔性印刷电路板电连接到第二印刷电路板的装置,其中从第二印刷电路板突出并突出穿过第一印刷电路板中的开口的导电接触销, 导电连接到第一印刷电路板的导体轨道。 该装置还包括导电夹持部分,其具有弹性柔性突起,其上嵌有柔性突起,其通过非正向接合包围接触销,并且电连接到突起的夹持部分的支承区域以预定方式被压靠在布置的导体轨道上 在第一个印刷电路板上。
    • 10. 发明授权
    • Passenger service unit and an aircraft cabin systems control with such service units
    • 乘客服务单位和飞机舱系统控制与这些服务单位
    • US06393343B1
    • 2002-05-21
    • US09651711
    • 2000-08-31
    • Martin FreyDirk Andersen
    • Martin FreyDirk Andersen
    • G06F1900
    • B64D11/00Y02T50/46
    • Passenger service units in an aircraft are equipped with a passenger interface and supply adapter (10). Each adapter includes an individual processor (14) which is programmable independently of the aircraft central control through a programming input. The programmable interface (10) permits controlling passenger service components in the passenger cabin such as lamps in a cabin lighting system, a public address system, and so forth, directly by the interface (10) independently of the aircraft central control. The interface (10) with its own individual processor (14) and memory (15) is connected through a databus (11) to the aircraft central control (12), for example, for remote programming of the interface and for reporting the module's activities to the aircraft central control. The interface (10) reduces the memory capacity requirements for the aircraft central control and permits the individual programming of each passenger service unit also independently of any other passenger service unit thereby avoiding retesting of the entire cabin system when for example only one passenger service unit is reprogrammed.
    • 飞机上的乘客服务单位配有乘客接口和供电适配器(10)。 每个适配器包括单独的处理器(14),其通过编程输入独立于飞机中央控制器来编程。 可编程接口(10)允许通过接口(10)独立于飞机中央控制器直接控制客舱中的乘客服务部件,例如客舱照明系统中的灯,公共广播系统等。 具有其自己的单独处理器(14)和存储器(15)的接口(10)通过数据总线(11)连接到飞行器中央控制器(12),例如用于远程编程接口并用于报告模块的活动 到飞机中央控制。 接口(10)减少了飞机中央控制器的存储器容量要求,并且允许每个乘客服务单元的单独编程也独立于任何其他乘客服务单元,从而避免了当例如仅一个乘客服务单元 重新编程。