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    • 7. 发明申请
    • DATA PROVISIONING REGISTRY
    • 数据提供注册
    • US20100145999A1
    • 2010-06-10
    • US12413125
    • 2009-03-27
    • Richard M. WilsonEric B. StanleyCharles B. Lomax, JR.Benjamin Alexander LeesonMary Carla DeAngelis
    • Richard M. WilsonEric B. StanleyCharles B. Lomax, JR.Benjamin Alexander LeesonMary Carla DeAngelis
    • G06F17/30
    • G06Q10/00G06F17/30286
    • A registry for designating authoritative sourcing of data from a data environment in a computer readable storage medium. Selected data content resides into a first data subject area in the form of a common business language, and metadata including characteristics of data stores in the data environment resides into a second data subject area, which is a metadata repository. Data linking a term in the first data subject area with an authoritative location of data associated with the term, as identified in the second data subject area, resides into a third subject area, which is the registry. A basis of authority of the data location and operating scope of the data may be designated in the third data store. Operating scopes may be functional, geographic, temporal, organizational, or a combination thereof. A computer program product and computer readable memory system for designating authoritative sourcing in a data environment are provided.
    • 用于从计算机可读存储介质中的数据环境指定数据的权威采集的注册表。 所选择的数据内容以普通业务语言的形式驻留在第一数据主题区域中,并且包括数据环境中的数据存储的特​​征的元数据驻留在作为元数据存储库的第二数据主题区域中。 将第一数据主题区域中的术语与第二数据主题区域中标识的与该术语相关联的数据的权威位置链接的数据驻留在作为注册表的第三主题区域中。 可以在第三数据存储器中指定数据位置的权限和数据的操作范围。 操作范围可以是功能,地理,时间,组织或其组合。 提供了一种用于在数据环境中指定权威采购的计算机程序产品和计算机可读存储器系统。
    • 8. 发明授权
    • Spa cover support assembly
    • 水疗护罩支撑组件
    • US5644803A
    • 1997-07-08
    • US605490
    • 1996-02-26
    • Richard M. Wilson
    • Richard M. Wilson
    • E04H4/08E04H4/06
    • E04H4/088
    • A spa cover support assembly is provided with a plurality of support arms having upper and lower ends with the lower ends pivotally attached to an external surface of the spa side wall for pivotal rotation of the upper ends of the support arms through an arc from a point above and adjacent to the side wall to a point away from the side wall at a point where the upper ends of the support arms are within the generally horizontal plane defined by the top surfaces of the side walls and at a distance away from the side wall wherein the center of gravity of the spa cover supported between the side wall and the upper ends of the support arms will fall between the side wall and the upper ends of the support arm assembly. A generally horizontal support bar is provided attached to the upper ends of the support arms for supporting the spa cover.
    • 温泉护罩支撑组件设置有多个支撑臂,所述多个支撑臂具有上端和下端,下端可枢转地附接到温泉侧壁的外表面,用于支撑臂的上端通过弧从一点 在支撑臂的上端位于由侧壁的顶表面限定的大致水平的平面内并且远离侧壁的距离处,在侧壁上方并且靠近侧壁到远离侧壁的点 其中支撑在所述侧壁和所述支撑臂的上端之间的所述温泉护罩的重心将落在所述支撑臂组件的侧壁和所述上端之间。 提供附接到支撑臂的上端的大致水平的支撑杆,用于支撑温泉护罩。
    • 9. 发明授权
    • Method and apparatus for using hot fuels to de-ice aircraft
    • 使用热燃料去除飞机的方法和装置
    • US5558303A
    • 1996-09-24
    • US364301
    • 1994-12-27
    • Terence L. KoetheRichard M. WilsonGary L. Reid
    • Terence L. KoetheRichard M. WilsonGary L. Reid
    • B64F5/00B64D15/02
    • B64F5/0072Y10T137/6552
    • A method and apparatus are provided for de-icing an aircraft of the type having wings and fuel storage in the wings. Hot fuel is provided for fueling the aircraft. The hot fuel is at elevated temperatures which are sufficiently high enough to transfer heat from the fuel, through a fuel tank extending within the wings, and to the exterior of the wings to de-ice the aircraft. A storage tank stores the fuel, and a heater heats the fuel to elevated temperatures. An intermediate thermal transfer system having a secondary thermal fluid transfers heat from a primary power source to the fuel. Further, a substantial volume of the secondary thermal fuel may be maintained at elevated temperatures to provide a sufficient thermal reserve capacity for heating the fuel upon demand.
    • 提供一种方法和装置,用于使具有机翼和燃料储存在翼中的类型的飞机除冰。 提供热燃料来加油飞机。 热燃料处于升高的温度,这些高温足够高以从燃料传递热量,通过在翼内延伸的燃料箱以及机翼的外部来使飞机脱冰。 储罐储存燃料,加热器将燃料加热到升高的温度。 具有次级热流体的中间热传递系统将热量从主电源传递到燃料。 此外,大量的二次热燃料可以保持在升高的温度下,以提供足够的热储备容量以根据需要加热燃料。