Mapping engine for a storage device
    5.
    发明授权
    Mapping engine for a storage device 有权
    存储设备的映射引擎

    公开(公告)号:US08402198B1

    公开(公告)日:2013-03-19

    申请号:US12790255

    申请日:2010-05-28

    IPC分类号: G06F12/00

    CPC分类号: G06F12/0866

    摘要: A hardware search structure quickly determines the status of cache lines associated with a large disk array and at the same time reduces the amount of memory space needed for tracking the status. The search structure is configurable in hardware to different cache line sizes and different primary and secondary index sizes. A maintenance feature invalidates state record entries based both on their time stamps and on associated usage statistics.

    摘要翻译: 硬件搜索结构可以快速确定与大型磁盘阵列相关联的高速缓存行的状态,同时减少跟踪状态所需的内存空间。 搜索结构可以在硬件中配置为不同的高速缓存行大小和不同的主索引和辅助索引大小。 维护功能使状态记录条目基于其时间戳和关联的使用统计信息无效。

    Current-aligned auto-generated non-equiaxial hole shape for wiring
    6.
    发明授权
    Current-aligned auto-generated non-equiaxial hole shape for wiring 有权
    电流对齐自动生成的非等轴孔形状用于接线

    公开(公告)号:US08299775B2

    公开(公告)日:2012-10-30

    申请号:US11160428

    申请日:2005-06-23

    IPC分类号: G01R19/00

    摘要: A method, system and program product for replacing isotropic hole shapes in a wiring layout with non-equiaxial hole shapes that are arranged in a direction of current flow, which increases current flow along the wire's longitudinal axis while decreasing current flow along the wire's transverse axis. One aspect of the invention includes a method including determining a direction of electrical current flow in a portion of a wiring layout; and placing at least one non-equiaxial hole shape within the portion of the wiring layout, wherein the non-equiaxial hole shape is arranged in the direction of electrical current flow. The invention accommodates the limitations of copper CMP within an automated tool without sacrificing the efficiency of a hand-tuned layout. The invention also includes a semiconductor device including at least one non-equiaxial hole shape.

    摘要翻译: 一种方法,系统和程序产品,用于在沿着电流流动方向布置的非等轴孔形状的布线布局中替换各向同性孔形状,其沿着线的纵向轴线增加电流,同时沿着线的横轴减小电流 。 本发明的一个方面包括一种方法,其包括确定布线布局的一部分中的电流流动的方向; 并且在所述布线布置部分内布置至少一个非等轴孔形状,其中所述非等轴孔形状沿电流流动方向布置。 本发明在自动化工具中适应铜CMP的限制,而不牺牲手动布局的效率。 本发明还包括包括至少一个非等轴孔形状的半导体器件。

    HIGH PRESSURE PASTEURIZING OF FROZEN GROUND MEATS
    7.
    发明申请
    HIGH PRESSURE PASTEURIZING OF FROZEN GROUND MEATS 审中-公开
    冷冻地面肉的高压消毒

    公开(公告)号:US20120269953A1

    公开(公告)日:2012-10-25

    申请号:US13497876

    申请日:2010-09-24

    IPC分类号: A23B4/06 A23L1/317 A23L1/314

    摘要: A process for preserving frozen ground meat comprises the steps of a) packaging frozen ground meat in a sealed package; b) placing the packaged frozen ground meat in a pressurization vessel and closing the vessel; c) pressurizing the pressurization vessel containing the packaged frozen ground meat to an elevated pressure of at least about 50,000 psi pressure so the packaged frozen ground meat is placed under the elevated pressure; d) maintaining the elevated pressure on the packaged frozen ground meat for a time of from about 1 to about 300 seconds and at a temperature of from about −50° to about 45° F.; e) then reducing the pressure on the packaged frozen ground meat to ambient pressure; and f) removing the packaged frozen ground meat from the pressurization vessel. Pathogens are effectively killed using this process, providing manufacturing efficiencies and longer product shelf life as compared to other ground meat handling procedures.

    摘要翻译: 一种保存冷冻碎肉的方法包括以下步骤:a)将冷冻的碎肉包装在密封包装中; b)将包装的冷冻肉放在加压容器中并关闭容器; c)将含有包装的冷冻碎肉的加压容器加压至至少约50,000psi压力的升高的压力,使包装的冷冻碎肉置于升高的压力下; d)将包装的冷冻碎肉上的升高的压力保持在约1至约300秒的时间和约-50°至约45°F的温度; e)然后将包装的冷冻肉肉的压力降低至环境压力; 以及f)从所述加压容器中取出包装的冷冻碎肉。 与其他肉类处理程序相比,使用该过程有效杀死病原体,提供制造效率和更长的产品保质期。

    Cooled gas turbine vane assembly
    8.
    发明授权
    Cooled gas turbine vane assembly 有权
    冷却燃气轮机组件

    公开(公告)号:US08142137B2

    公开(公告)日:2012-03-27

    申请号:US12323736

    申请日:2008-11-26

    IPC分类号: F03B11/00 F01D5/14

    摘要: A gas turbine vane to improve vane performance by addressing known failure mechanisms. A cooling circuit to the trailing edge of a vane airfoil is fed from the outer diameter platform, which prevents failure due to an oxidized and eroded airfoil trailing edge. The gas turbine includes an outer diameter platform, a hollow airfoil and an inner diameter platform with a plurality of cooling tubes extending radially through the airfoil. The cooling tubes are open at the outer diameter end and closed with covers at the inner diameter end. The inner diameter platform is also cooled and includes a meterplate for a portion of the cooling passageway and includes an undercut to improve thermal deflections of the inner diameter platform.

    摘要翻译: 一种燃气轮机叶片,通过解决已知的故障机制来改善叶片性能。 从外径平台供给到叶片翼型的后缘的冷却回路,这防止由于氧化和侵蚀的翼型后缘造成的故障。 燃气轮机包括外径平台,中空翼型件和具有径向延伸穿过翼型件的多个冷却管的内径平台。 冷却管在外径端开口,在内径端用盖封闭。 内径平台也被冷却,并且包括用于冷却通道的一部分的仪表板,并且包括底切以改善内径平台的热偏转。

    COOLED GAS TURBINE VANE ASSEMBLY
    9.
    发明申请
    COOLED GAS TURBINE VANE ASSEMBLY 有权
    冷却气体涡轮风扇组件

    公开(公告)号:US20100129196A1

    公开(公告)日:2010-05-27

    申请号:US12323736

    申请日:2008-11-26

    IPC分类号: F02C7/12

    摘要: A gas turbine vane to improve vane performance by addressing known failure mechanisms. A cooling circuit to the trailing edge of a vane airfoil is fed from the outer diameter platform, which prevents failure due to an oxidized and eroded airfoil trailing edge. The gas turbine includes an outer diameter platform, a hollow airfoil and an inner diameter platform with a plurality of cooling tubes extending radially through the airfoil. The cooling tubes are open at the outer diameter end and closed with covers at the inner diameter end. The inner diameter platform is also cooled and includes a meterplate for a portion of the cooling passageway and includes an undercut to improve thermal deflections of the inner diameter platform.

    摘要翻译: 一种燃气轮机叶片,通过解决已知的故障机制来改善叶片性能。 从外径平台供给到叶片翼型的后缘的冷却回路,这防止由于氧化和侵蚀的翼型后缘造成的故障。 燃气轮机包括外径平台,中空翼型件和具有径向延伸穿过翼型件的多个冷却管的内径平台。 冷却管在外径端开口,在内径端用盖封闭。 内径平台也被冷却,并且包括用于冷却通道的一部分的仪表板,并且包括底切以改善内径平台的热偏转。

    COMPRESSOR AIRFOIL
    10.
    发明申请
    COMPRESSOR AIRFOIL 有权
    压缩机AIRFOIL

    公开(公告)号:US20090290987A1

    公开(公告)日:2009-11-26

    申请号:US12175822

    申请日:2008-07-18

    IPC分类号: F01D5/14

    CPC分类号: F01D5/141 F05D2220/3216

    摘要: A compressor component having an airfoil with a profile in accordance with Table 1 is disclosed. The compressor component, such as a compressor blade, has an increased thickness over a portion of the airfoil span in order to increase stiffness. Furthermore, the airfoil has been restacked so as to induce a compressive stress in the blade root/attachment area. The increased stiffness and restacked airfoil combine to improve high-cycle fatigue capability of the compressor component.

    摘要翻译: 公开了具有根据表1的轮廓的翼型的压缩机部件。 压缩机部件,例如压缩机叶片,在翼型跨度的一部分上具有增加的厚度,以增加刚度。 此外,已经重新安装翼型件以在叶片根部/附接区域中引起压缩应力。 增加的刚度和复位翼型结合起来以改善压缩机部件的高循环疲劳能力。