ELECTRONICS ENCLOSURES WITH HIGH THERMAL PERFORMANCE AND RELATED METHOD
    2.
    发明授权
    ELECTRONICS ENCLOSURES WITH HIGH THERMAL PERFORMANCE AND RELATED METHOD 有权
    具有高热性能的电子外壳及相关方法

    公开(公告)号:EP2848106B1

    公开(公告)日:2018-04-25

    申请号:EP13797147.9

    申请日:2013-03-11

    申请人: Raytheon Company

    摘要: Various apparatuses, methods, and systems are provided for cooling electronic components. For example, an apparatus includes an electronics enclosure having multiple ribs configured to separate electronic components. The apparatus also includes at least one fluid transport structure encased within the electronics enclosure. Each fluid transport structure includes multiple pipes and multiple flow channels. The flow channels are located within the ribs of the electronics enclosure, and the pipes are configured to transport cooling fluid to and from the flow channels. The fluid transport structure(s) and the electronics enclosure are formed from different materials. The at least one fluid transport structure can be resistant to corrosion caused by the cooling fluid, and the electronics enclosure can be susceptible to corrosion caused by the cooling fluid. As an example, the at least one fluid transport structure could consist essentially of nickel, and the electronics enclosure could consist essentially of aluminum.

    RF/MICROWAVE HIGH POWER SWITCHING COMBINER UNIT
    3.
    发明公开
    RF/MICROWAVE HIGH POWER SWITCHING COMBINER UNIT 审中-公开
    射频/微波高功率开关组合器单元

    公开(公告)号:EP3249813A1

    公开(公告)日:2017-11-29

    申请号:EP17001022.7

    申请日:2015-09-17

    IPC分类号: H03F1/52 H03F3/60 H01P1/10

    摘要: A switching combiner unit (SCU) that combines coherent RF or microwave outputs from multiple power amplifier units (PAUs), each of which can be switched between an on-line mode (on-line PAU), during which the PAU amplifies a coherent instance of the same RF or microwave input signal and delivers that amplified input signal to an output, and a standby or off-line mode (standby/off-line PAU), during which the PAU does not amplify an instance of the same RF or microwave input signal or deliver an amplified input signal to the output, comprising:
    an input port that connects to each of the PAU outputs;
    a control signal input that receives one or more control signals that indicate whether each PAU is in the on-line or standby/off-line mode;
    signal combining circuitry that coherently sums the outputs from all of the on-line PAUs, while simultaneously isolating the standby/off-line PAUs from the output of the SCU and the outputs of the on-line PAUs; and
    an SCU output port that delivers the coherently summed outputs from all of the on-line PAUs.

    摘要翻译: 开关组合器单元(SCU),结合来自多个功率放大器单元(PAU)的相干RF或微波输出,其中的每一个都可以在在线模式(在线PAU)之间切换,在此期间PAU放大相干实例 的相同的RF或微波输入信号并且将该放大的输入信号传送到输出以及备用或离线模式(备用/离线PAU),在此期间PAU不放大相同RF或微波的实例 输入信号或将放大的输入信号传送到输出端,包括:连接到每个PAU输出端的输入端口; 控制信号输入,其接收指示每个PAU是处于在线模式还是处于待机/离线模式的一个或多个控制信号; 信号组合电路,其对来自所有在线PAU的输出进行相干求和,同时将备用/离线PAU与SCU的输出和在线PAU的输出隔离; 和一个SCU输出端口,用于传输来自所有在线PAU的相干求和输出。

    FLUGZEUGSIGNALRECHNERSYSTEM MIT EINER MEHRZAHL VON MODULAREN SIGNALRECHNEREINHEITEN
    7.
    发明公开
    FLUGZEUGSIGNALRECHNERSYSTEM MIT EINER MEHRZAHL VON MODULAREN SIGNALRECHNEREINHEITEN 有权
    具有模块信号微机单位多架飞机信号微机系统

    公开(公告)号:EP2305016A1

    公开(公告)日:2011-04-06

    申请号:EP09777867.4

    申请日:2009-08-13

    IPC分类号: H05K7/20

    摘要: The invention relates to an aircraft signal computer system (10) comprising a plurality of modular signal computer units (12) and a liquid cooling device for cooling the modular signal computer units (12), wherein the liquid cooling device comprises a coolant line (16), which can be connected to a central liquid cooling system of an aircraft in order to feed a liquid coolant medium at a desired low temperature to the liquid cooling device, and wherein the coolant line (16) of the liquid cooling device is in thermal surface contact with the modular signal computer units (12) in order to dissipate heat from the modular signal computer units (12).

    Support de calculateur de turbomachine d'aviation
    9.
    发明公开
    Support de calculateur de turbomachine d'aviation 失效
    支持涡轮飞行机器的计算机。

    公开(公告)号:EP0213019A1

    公开(公告)日:1987-03-04

    申请号:EP86401656.3

    申请日:1986-07-24

    发明人: Rambach, Daniel

    IPC分类号: H05K7/14 H05K7/20

    摘要: L'invention concerne les supports de dispositifs électroniques.
    Le support selon l'invention est caractérisé en ce que des premiers moyens d'accrochage (19, 119, 219) portés par des faces du support coopèrent aves des secondes moyens (20, 120, 220) portés par les faces correspondantes du calculateur d'abord dans un premier mouvement d'introduction du calculateur de l'avant vers l'arrière jusqu'à la mise en contact du calculateur avec la face arrière refroidie (6) du support puis dans un second mouvement orthogonal au premier jusqu'à l'emboîtement de connecteurs appariés (resp. 18a, 18b, 118a, 118b, 218a, 218b) portés par le calculateur et une face latérale du support.
    Application aux régulations électroniques disposées sur la paroi d'un turboréacteur.