SYSTEM AND METHOD FOR VERIFYING COMPATIBILITY OF COMPUTER EQUIPMENT WITH A SOFTWARE PRODUCT
    81.
    发明申请
    SYSTEM AND METHOD FOR VERIFYING COMPATIBILITY OF COMPUTER EQUIPMENT WITH A SOFTWARE PRODUCT 有权
    用于验证计算机设备与软件产品兼容性的系统和方法

    公开(公告)号:US20100100772A1

    公开(公告)日:2010-04-22

    申请号:US12629421

    申请日:2009-12-02

    CPC classification number: G06F11/2289 G06F11/3688

    Abstract: System and method for verifying compatibility of computer equipment with a software product. A system and method are provided to verify compatibility of computer equipment with software. This verification can include gathering information about configurations of the computer equipment, and creating at least one file based on the information. The file or files coordinate testing of the computer equipment. The testing produces results that can be stored and analyzed or evaluated. The results can be contained in a file or a plurality of files. The results provide a description of the configurations in addition to an indication of whether the testing has produced any failures. The configuration descriptions or parts thereof can be stored in a configuration database that can be used to apply credit against future testing of computer equipment so that future testing needs can be reduced.

    Abstract translation: 用于验证计算机设备与软件产品的兼容性的系统和方法。 提供了一种系统和方法来验证计算机设备与软件的兼容性。 该验证可以包括收集关于计算机设备的配置的信息,以及基于该信息创建至少一个文件。 文件或文件对计算机设备进行坐标测试。 测试产生可以存储和分析或评估的结果。 结果可以包含在文件或多个文件中。 除了指示测试是否产生任何故障之外,结果还提供了配置的描述。 配置描述或其部分可以存储在配置数据库中,可以用于对未来的计算机设备测试应用信用,从而可以减少未来的测试需求。

    LIGHTWEIGHT GRIP AND METHOD OF MAKING SAME
    82.
    发明申请
    LIGHTWEIGHT GRIP AND METHOD OF MAKING SAME 有权
    轻量级GRIP及其制作方法

    公开(公告)号:US20100077568A1

    公开(公告)日:2010-04-01

    申请号:US12240315

    申请日:2008-09-29

    Inventor: David Keith Gill

    Abstract: A light flexible hand grip and method of making with an inner tubular core of flexible rubber with apertures formed therein and an outer tubular cover disposed over the core with a lighter weight annular flexible foam spacer between the core and outer cover. The spacer may be formed by injecting curable material through the apertures. The apertures may be formed by inserting a mandrel in the core, punching the holes and removing the mandrel.

    Abstract translation: 柔性手柄和方法,其制成具有形成在其中的孔的柔性橡胶的内部管状芯和设置在芯上的外部管状盖,在芯和外盖之间具有较轻重量的环形柔性泡沫隔离物。 间隔物可以通过将可固化材料注入孔中而形成。 孔可以通过将心轴插入芯中,冲孔和移除心轴来形成。

    Carbon Dioxide Capture
    83.
    发明申请
    Carbon Dioxide Capture 有权
    二氧化碳捕获

    公开(公告)号:US20100034724A1

    公开(公告)日:2010-02-11

    申请号:US12488230

    申请日:2009-06-19

    Abstract: A method of carbon dioxide capture is disclosed. In a step (a) anhydrous sodium carbonate is separated from a first aqueous solution formed by reacting carbon dioxide and an aqueous solution of sodium hydroxide. In step (b) the anhydrous sodium carbonate is treated by causticization to generate carbon dioxide and sodium hydroxide. The first aqueous solution of step (a) is formed by scrubbing a gas containing carbon dioxide with an aqueous solution of sodium hydroxide.

    Abstract translation: 公开了一种捕获二氧化碳的方法。 在步骤(a)中,将无水碳酸钠与通过二氧化碳和氢氧化钠水溶液反应形成的第一水溶液分离。 在步骤(b)中,通过苛化处理无水碳酸钠以产生二氧化碳和氢氧化钠。 通过用氢氧化钠水溶液洗涤含二氧化碳的气体来形成步骤(a)的第一水溶液。

    Counter tip baffle airfoil
    84.
    发明授权
    Counter tip baffle airfoil 有权
    台顶挡板翼型

    公开(公告)号:US07607893B2

    公开(公告)日:2009-10-27

    申请号:US11507132

    申请日:2006-08-21

    CPC classification number: F01D5/20 F01D5/145 F05D2250/70 Y02T50/671 Y02T50/673

    Abstract: A turbine blade includes an airfoil having first and second tip ribs extending along the opposite pressure and suction sides thereof. The tip ribs are spaced apart between the leading and trailing edges of the airfoil to include a tip baffle. The baffle extends chordally in counter profile with the first rib to define a first pocket, and in counter profile with the second rib to define a second pocket.

    Abstract translation: 涡轮叶片包括具有沿其相对的压力和吸力侧延伸的第一和第二末端肋的翼型件。 末端肋在翼型件的前缘和后缘之间间隔开,以包括顶端挡板。 所述挡板以第一肋条与第一肋条相反地延伸,以相反轮廓延伸,以限定第一凹槽,并且与第二肋条对置形成第二凹槽。

    Rotor blade profile optimization
    90.
    发明授权
    Rotor blade profile optimization 有权
    转子叶片轮廓优化

    公开(公告)号:US07497663B2

    公开(公告)日:2009-03-03

    申请号:US11586952

    申请日:2006-10-26

    CPC classification number: F01D5/141 F05D2250/74 Y10S416/02

    Abstract: An airfoil for a rotor blade including an uncoated profile substantially in accordance with Cartesian coordinate values of X, Y and Z to facilitate balancing performance and durability of the rotor blade and to facilitate improving an operating efficiency of a high-pressure turbine is provided. The profile is carried only to four decimal places, wherein Y represents a distance from a platform on which the airfoil is mounted, and X and Z are coordinates defining the profile at each distance Y from the platform.

    Abstract translation: 提供了一种用于转子叶片的翼型件,其包括基本上根据X,Y和Z的笛卡尔坐标值的未涂覆轮廓,以便于平衡转子叶片的性能和耐久性,并且有助于提高高压涡轮机的操作效率。 配置文件仅承载四位小数,其中Y表示与安装有翼型件的平台的距离,X和Z是从平台每个距离Y定义轮廓的坐标。

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