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    • 1. 发明申请
    • User managed method for capturing and pricing data items to develop a salable digital persona
    • 用户管理的方法,用于捕获和定价数据项以开发可销售的数字人物角色
    • US20150310457A1
    • 2015-10-29
    • US14265311
    • 2014-04-29
    • Stanley Smith
    • Stanley Smith
    • G06Q30/02
    • G06Q30/0201
    • A method for a user to capture, configure, store, link, exchange, and set trading parameters (prices and other exchange values) for data drawn from the user's personal data file combined with other user generated data; including data resulting from the user's interactions with file creation software, data items generated from user interactions with electronic devices and components, and data automatically generated by electronic components and devices owned by a user. In combination, these combined data sources coupled with a personal data file form a digital persona or a “digital doppelganger” that may be traded or sold or retained as private in a data marketplace.
    • 一种用于捕获,配置,存储,链接,交换和设置用户个人数据文件与其他用户生成的数据相结合的数据的交易参数(价格和其他交换值)的方法; 包括用户与文件创建软件交互的数据,从用户与电子设备和组件的交互产生的数据项,以及由用户拥有的电子组件和设备自动生成的数据。 与个人数据文件相结合的这些组合数据源组合在一起,形成数字角色或可在数据市场中作为私人交易或出售或保留的“数字多媒体”。
    • 2. 发明授权
    • Oil system for aircraft gas turbine engine
    • 飞机燃气轮机发动机油系
    • US4531358A
    • 1985-07-30
    • US305706
    • 1981-09-25
    • Stanley Smith
    • Stanley Smith
    • F02C7/06B64D33/00F01D25/20F16N29/02
    • F01D25/20F16N29/02Y02T50/671
    • A fully aerobatic oil system for an aircraft gas turbine engine includes two re-circulatory oil systems the pumps for which have inlets 19 and 31a disposed at locations in the engine such that when one inlet is starved of oil, due to the aircraft attitude changing, oil will be supplied to the other one. In a specific embodiment, the breather of the oil system 30 (FIG. 2) is positioned in the engine gearbox and provides the lowest pressure point in the system. The breather is of the type described in UK Pat. No. 1,508,212 which includes a rotating compartment filled with RETIMET (Regd. Trade Mark). The bearing chambers are pressurised with air from the engine and the air/oil mixture in each chamber is vented via a first series of vents 24 to the breather where the air and oil are separated. The breather is used as a pump to pump the separated oil back to the oil tank via a scavenge line 35 which includes a relief valve 38. A bleed line 36 takes some of the oil from line 35 to the main oil supply gallery 23 via a non-return check valve 37. In normal flight pump 20 supplies the gallery 23 from the tank 18 via pump inlet 19, the relief valve 38 being set to a pressure lower than that of relief valve 40 which controls the pump pressure. The check valve 37 thus remains shut. When the inlet 19 is starved of oil because the flight attitude of the aircraft changes, the pressure in gallery 23 drops to the extent that check valve 37 opens and the breather/pump takes over circulating oil from the gearbox and bearings around the second system.
    • 用于飞机燃气涡轮发动机的完全特技制油系统包括两个再循环油系统,其泵具有设置在发动机中的位置处的入口19和31a,使得当一个入口缺油时,由于飞行器姿态改变, 油将供应给另一个。 在具体实施例中,油系统30(图2)的通气器定位在发动机齿轮箱中并且在系统中提供最低压力点。 呼吸器是英国Pat。 包括装有RETIMET(Regd。商标)的旋转隔间的1,508,212号。 轴承室由来自发动机的空气加压,并且每个室中的空气/油混合物经由第一系列通风口24排放到空气和油分离的通气孔。 呼吸器用作泵,通过包括释放阀38的清扫管线35将分离的油泵送回油箱。排放管线36将一些油从管线35经由主油供应廊23经由 止回止回阀37.在正常的飞行泵20中,通过泵入口19从储罐18供给储存器23,溢流阀38被设定为低于控制泵压力的溢流阀40的压力。 止回阀37因此保持关闭。 当入口19由于飞行器的飞行姿态而变空时,喷射器19的压力变小,喷射器23中的压力下降到止回阀37打开的程度,并且呼吸器/泵接收来自齿轮箱的循环油和围绕第二系统的轴承。
    • 3. 发明申请
    • Novel CMP endpoint detection process
    • 新型CMP端点检测过程
    • US20060211157A1
    • 2006-09-21
    • US11082406
    • 2005-03-17
    • Stanley SmithChristopher Borst
    • Stanley SmithChristopher Borst
    • H01L21/4763
    • H01L21/7684H01L21/3212H01L22/26
    • The present invention provides a method for polishing a layer of material, a method for manufacturing a damascene interconnect structure, and a method for manufacturing an integrated circuit. The method for polishing a layer of material, among other steps, includes obtaining a substrate (310) having a layer of material (330) located thereover, and polishing the layer of material (330) using a polishing surface (410). The step of polishing the layer of material may include subjecting the layer of material (330) to a first polishing process using a first endpoint detection method, the first polishing process removing a portion of the layer of material, and subjecting remaining portions (420) of the layer of material (330) to a second polishing process using a second different optical endpoint detection method.
    • 本发明提供了一种用于抛光材料层的方法,一种用于制造镶嵌互连结构的方法和一种用于制造集成电路的方法。 除了其他步骤之外,用于抛光材料层的方法包括获得具有位于其上的材料层(330)的衬底(310),并且使用抛光表面(410)抛光材料层(330)。 抛光材料层的步骤可以包括使用第一端点检测方法对材料层(330)进行第一抛光工艺,第一抛光工艺移除材料层的一部分,以及对剩余部分(420)进行处理, 使用第二种不同的光学终点检测方法将材料层(330)转移到第二抛光工艺。
    • 4. 发明授权
    • Spinner fishing lure
    • 旋转钓鱼诱饵
    • US5355612A
    • 1994-10-18
    • US971016
    • 1992-11-02
    • Stanley Smith
    • Stanley Smith
    • A01K85/00
    • A01K85/00
    • A spinner fishing lure having a frame including first and second diverging arms lying generally in the same plane. A hook is connected to the frame at the distal end of the first arm and lies generally in the plane of the first and second arms. The lure also includes at least two blades and connectors for connecting the blades to the frame generally at the distal end of the second arm. The blades are tethered to the connectors at spaced apart connection points such that the blades may swivel relative to the connectors generally sweeping out overlapping cones as the blades travel through the water so that the blades periodically strike one another to produce a noise attractive to fish. The connectors are configured so that the connection points of the blades and the blades are substantially vertically aligned as the lure is pulled through the water.
    • 旋转器钓鱼诱饵具有框架,该框架包括通常位于同一平面中的第一和第二分叉臂。 钩在第一臂的远端处连接到框架,大体上位于第一和第二臂的平面中。 诱饵还包括至少两个叶片和连接器,用于将叶片大致在第二臂的远端处连接到框架。 叶片在间隔开的连接点处连接到连接器,使得当叶片穿过水流时,叶片可相对于连接器旋转,通常扫过重叠的锥体,使得叶片周期性地相互撞击以产生对鱼有吸引力的噪声。 连接器构造成使得当诱饵被拉过水时,叶片和叶片的连接点基本垂直对准。
    • 5. 发明授权
    • Gas turbine engine oil systems
    • 燃气轮机发动机油系统
    • US4576001A
    • 1986-03-18
    • US573312
    • 1984-01-24
    • Stanley Smith
    • Stanley Smith
    • F02C7/06F01D25/18F16N7/40F16N13/20F16N39/06F02G3/00
    • F16N13/20F01D25/18F16N39/06F16N7/40
    • A gas turbine engine oil system is provided in which the centrifugal separator is arranged to act as a pump for supplying bearing chambers directly, and the scavenging of the bearing chambers is achieved primarily by the pressurization air which flows into the chambers to prevent oil leakage. To avoid the use of pressure regulating valves for controlling the oil flow an oil tank is pressurized and communicates with an auxiliary outlet from the separator, the pressure in which is governed by the quantity of oil flowing around the system. The tank and the bearing chambers are fluidly connected to the centrifugal separator in two separate fluid circuits with each circuit having the separator as an element thereof.
    • 提供了一种燃气涡轮发动机油系统,其中离心分离器布置成用作直接供应轴承室的泵,并且主要通过流入室中的加压空气来实现轴承室的清除,以防止漏油。 为了避免使用压力调节阀来控制油流量,油箱被加压并与来自分离器的辅助出口连通,其压力由系统周围的油量控制。 罐和轴承室在两个独立的流体回路中流体地连接到离心分离器,每个回路具有分离器作为其元件。