Communication system and method for synchronizing a plurality of network nodes after a network lock condition occurs
    1.
    发明授权
    Communication system and method for synchronizing a plurality of network nodes after a network lock condition occurs 有权
    在发生网络锁定状态之后使多个网络节点同步的通信系统和方法

    公开(公告)号:US08861664B2

    公开(公告)日:2014-10-14

    申请号:US13524323

    申请日:2012-06-15

    CPC classification number: H04J3/0638 H04J3/0647 H04J3/0673

    Abstract: A communication system and method is provided herein for synchronizing a plurality of network nodes after a network lock condition occurs within a network. According to one embodiment, the method may generate a local trigger signal simultaneously at each of the plurality of network nodes by compensating for unique phase delays attributed to each of the plurality of network nodes. As described herein, the local trigger signals may be used for synchronizing devices, such as multimedia devices, which may be coupled to the network nodes. More specifically, the local trigger signals may be used to synchronize events occurring within devices, which are coupled to different nodes of the network.

    Abstract translation: 本文提供了一种在网络中发生网络锁定状况之后同步多个网络节点的通信系统和方法。 根据一个实施例,该方法可以通过补偿属于多个网络节点中的每一个的唯一相位延迟来在多个网络节点中的每一个处同时产生本地触发信号。 如本文所述,本地触发信号可以用于同步诸如可以耦合到网络节点的多媒体设备的设备。 更具体地,本地触发信号可以用于同步在耦合到网络的不同节点的设备内发生的事件。

    Communication System and Method for Synchronizing a Plurality of Network Nodes After a Network Lock Condition Occurs
    2.
    发明申请
    Communication System and Method for Synchronizing a Plurality of Network Nodes After a Network Lock Condition Occurs 有权
    网络锁定状态发生后的多个网络节点同步的通信系统和方法

    公开(公告)号:US20130336435A1

    公开(公告)日:2013-12-19

    申请号:US13524323

    申请日:2012-06-15

    CPC classification number: H04J3/0638 H04J3/0647 H04J3/0673

    Abstract: A communication system and method is provided herein for synchronizing a plurality of network nodes after a network lock condition occurs within a network. According to one embodiment, the method may generate a local trigger signal simultaneously at each of the plurality of network nodes by compensating for unique phase delays attributed to each of the plurality of network nodes. As described herein, the local trigger signals may be used for synchronizing devices, such as multimedia devices, which may be coupled to the network nodes. More specifically, the local trigger signals may be used to synchronize events occurring within devices, which are coupled to different nodes of the network.

    Abstract translation: 本文提供了一种在网络中发生网络锁定状况之后同步多个网络节点的通信系统和方法。 根据一个实施例,该方法可以通过补偿属于多个网络节点中的每一个的唯一相位延迟来在多个网络节点中的每一个处同时产生本地触发信号。 如本文所述,本地触发信号可以用于同步诸如可以耦合到网络节点的多媒体设备的设备。 更具体地,本地触发信号可以用于同步在耦合到网络的不同节点的设备内发生的事件。

    Aircraft side fairing
    3.
    发明授权

    公开(公告)号:US08490365B2

    公开(公告)日:2013-07-23

    申请号:US12308926

    申请日:2007-06-22

    Abstract: The invention relates to an aircraft side fairing, with a component (9) in the form of individual hollow chambers (12, 13, 14) which are arranged essentially in a preferably curved plane and are arranged between two cover layers (1, 2), wherein a gastight film which completely encases the component (9) with the hollow chambers (12, 13, 14) is provided and, after application of a vacuum to evacuate the hollow chambers (12, 13, 14), surrounds the component (9) with the hollow chambers in a gastight manner.

    Aircraft side fairing
    10.
    发明申请
    Aircraft side fairing 有权
    飞机侧整流罩

    公开(公告)号:US20090304979A1

    公开(公告)日:2009-12-10

    申请号:US12308926

    申请日:2007-06-22

    Abstract: The invention relates to an aircraft side fairing, with a component (9) in the form of individual hollow chambers (12, 13, 14) which are arranged essentially in a preferably curved plane and are arranged between two cover layers (1, 2), wherein a gastight film which completely encases the component (9) with the hollow chambers (12, 13, 14) is provided and, after application of a vacuum to evacuate the hollow chambers (12, 13, 14), surrounds the component (9) with the hollow chambers in a gastight manner.

    Abstract translation: 本发明涉及一种飞机侧整流罩,其具有基本上位于优选弯曲平面中并且布置在两个覆盖层(1,2)之间的单个中空室(12,13,14)形式的部件(9) 其特征在于,提供将所述部件(9)完全包住所述中空室(12,13,14)的气密膜,并且在施加真空以抽空所述中空室(12,13,14)之后,围绕所述部件 9)以气密的方式与中空室。

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