SYSTEM AND METHOD FOR CLASSIFYING PIXELS
    1.
    发明申请
    SYSTEM AND METHOD FOR CLASSIFYING PIXELS 有权
    用于分类像素的系统和方法

    公开(公告)号:US20150379376A1

    公开(公告)日:2015-12-31

    申请号:US14318135

    申请日:2014-06-27

    IPC分类号: G06K9/62

    摘要: Embodiments are disclosed that relate to processing image pixels. For example, one disclosed embodiment provides a system for classifying pixels comprising retrieval logic; a pixel storage allocation including a plurality of pixel slots, each pixel slot being associated individually with a pixel, where the retrieval logic is configured to cause the pixels to be allocated into the pixel slots in an input sequence; pipelined processing logic configured to output, for each of the pixels, classification information associated with the pixel; and scheduling logic configured to control dispatches from the pixel slots to the pipelined processing logic, where the scheduling logic and pipelined processing logic are configured to act in concert to generate the classification information for the pixels in an output sequence that differs from and is independent of the input sequence.

    摘要翻译: 公开了涉及处理图像像素的实施例。 例如,一个公开的实施例提供了一种用于对包括检索逻辑的像素进行分类的系统; 包括多个像素时隙的像素存储分配,每个像素时隙与像素相关联,其中所述检索逻辑被配置为使所述像素被分配到输入序列中的所述像素时隙中; 流水线处理逻辑被配置为针对每个像素输出与像素相关联的分类信息; 以及调度逻辑,被配置为控制从像素时隙到流水线处理逻辑的调度,其中调度逻辑和流水线处理逻辑被配置为一致地起作用以产生与输出序列不同且独立于的输出序列中的像素的分类信息 输入序列。

    Crashworthy external auxiliary fuel tank for aircraft
    2.
    发明授权
    Crashworthy external auxiliary fuel tank for aircraft 有权
    用于飞机的Crashworthy外部辅助燃料箱

    公开(公告)号:US06491255B1

    公开(公告)日:2002-12-10

    申请号:US09738125

    申请日:2000-12-15

    IPC分类号: B64D3704

    CPC分类号: B64D37/04 B64D37/32

    摘要: An external auxiliary fuel tank for aircraft including a crashworthy bladder carried within an elongated shell. A center structure is carried by the shell intermediate opposing ends thereof, through which the bladder passes. A mounting assembly is carried by the center structure for attaching the fuel tank to an aircraft.

    摘要翻译: 用于飞行器的外部辅助燃料箱,其包括承载在细长壳体内的耐碰撞气囊。 中心结构由壳体的中间相对端承载,膀胱通过该结构。 安装组件由用于将燃料箱附接到飞行器的中心结构承载。