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    • 3. 发明申请
    • AN AVIONIC CENTRAL CONTROL COMPUTER
    • 海洋中央控制计算机
    • WO2016140637A1
    • 2016-09-09
    • PCT/TR2016/050052
    • 2016-03-02
    • ASELSAN ELEKTRONIK SANAYI VE TICARET ANONIM SIRKETI
    • SERDAR, YukselCALISLAR, Huseyin DincerAKINCI, UmurDURMUS, Mehmet UnalAKYUREK, SefaDORTKARDESLER, SerkanADEMOGLU, Mahmut Celal
    • G06F1/18G08G5/00H05K7/14
    • G06F1/182G06F1/185G06F1/188H05K7/1412
    • The present invention relates to an avionic central control computer (1) enabling to control target detection and weapon, electronic warfare, navigation, tactical data transmission and communication systems integrated on an aircraft, to perform mission and flight management, to manage display presentation and to supervise all information exchange on the platform from a single center, and essentially comprising a chassis (2) which provides mounting interface for the electronic cards located therein, at least one avionic processor card (3) which is adapted to perform navigation, communication, surveillance, emergency management and task planning processes, an MIL-STD-1553 interface mezzanine board (4), an ARINC-429 interface mezzanine board (5), at least one graphic processing card (6) which is adapted to generate graphic to be displayed on the screens for user interface, at least one video processing card (7) which is adapted to perform the process of switching video signals and changing the video forms, and at least one discrete interface card (8) which provides discrete input and output interface for discrete markers.
    • 本发明涉及一种航空电子中央控制计算机(1),其能够控制目标检测和集成在飞行器上的武器,电子战,导航,战术数据传输和通信系统,以执行任务和飞行管理,以管理显示呈现和 从单个中心监控平台上的所有信息交换,并且基本上包括为位于其中的电子卡提供安装接口的底盘(2),至少一个适于执行导航,通信,监视的航空电子处理器卡 ,紧急管理和任务规划过程,MIL-STD-1553接口夹层板(4),ARINC-429接口夹层板(5),至少一个图形处理卡(6),适用于生成要显示的图形 在用户界面的屏幕上,至少一个视频处理卡(7),其适于执行切换视频信号和改变的过程 以及至少一个离散接口卡(8),其提供用于离散标记的离散输入和输出接口。
    • 9. 发明申请
    • POWER SUPPLY COOLING SYSTEM
    • 电源冷却系统
    • WO2007061713A2
    • 2007-05-31
    • PCT/US2006044319
    • 2006-11-14
    • RACKABLE SYSTEM INCSEIBOLD LAWRENCE B
    • SEIBOLD LAWRENCE B
    • G06F1/20
    • G06F1/20G06F1/188
    • A power supply for use in a negative pressure computer system is provided, including: an enclosure; an air exhaust port provided on a First side of the enclosure; an air intake port provided on a second side of the enclosure, said second side being adjacent to the first side having the exhaust port; and an air mover configured to draw cooling air into the intake port and exhaust cooling air out of the exhaust port. A computer system is provided, including: a chassis; a printed circuit board (PCB) mounted in the chassis; one or more computer components coupled to the printed circuit board; a power supply for supplying power to the one or more computer components. The power supply includes: a power supply enclosure; a power supply intake port for receiving cooling air into the power supply housing; a power supply exhaust port oriented to exhaust air from the power supply housing into an interior region of the chassis; and a power supply air mover configured to draw cooling air into the power supply intake port and exhaust cooling air out of the exhaust port and into the interior region of the chassis. The computer system further includes one or more chassis air movers to draw the cooling air emitted from the exhaust port of the power supply out of the interior region of the chassis.
    • 提供用于负压计算机系统的电源,包括:外壳; 设置在所述外壳的第一侧的排气口; 设置在所述外壳的第二侧的进气口,所述第二侧与具有所述排气口的所述第一侧相邻; 以及空气移动器,其构造成将冷却空气吸入进气口并将冷却空气排出排出口。 提供一种计算机系统,包括:底盘; 安装在底盘中的印刷电路板(PCB); 耦合到印刷电路板的一个或多个计算机组件; 用于向所述一个或多个计算机部件供电的电源。 电源包括:电源外壳; 电源吸入口,用于将冷却空气接收到电源壳体中; 电源排气口,其定向为将空气从所述电源壳体排出到所述底盘的内部区域; 以及电源送风机,被配置为将冷却空气吸入电源进气口并将冷却空气排出排出口并进入底盘的内部区域。 计算机系统还包括一个或多个底盘空气推动器,以将从电源的排气口排出的冷却空气从机箱的内部区域抽出。