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    Integral abradable seals
    1.
    发明申请
    Integral abradable seals 有权
    整体耐磨密封件

    公开(公告)号：US20100151183A1

    公开(公告)日：2010-06-17

    申请号：US12316991

    申请日：2008-12-17

    申请人： Janet Davis ,  David Marshall ,  Olivier Sudre

    发明人： Janet Davis ,  David Marshall ,  Olivier Sudre

    IPC分类号： D03D27/00 ,  B32B7/02

    CPC分类号： D03D25/005 ,  B32B3/30 ,  B32B5/024 ,  B32B5/26 ,  B32B9/005 ,  B32B2262/105 ,  B32B2262/106 ,  B32B2307/554 ,  B32B2581/00 ,  B32B2605/18 ,  Y10T428/23914 ,  Y10T428/23957 ,  Y10T428/23979 ,  Y10T428/23986 ,  Y10T428/24992 ,  Y10T428/24996 ,  Y10T428/249967

    摘要： Devices, systems and methods for fabricating improved ceramic composite turbine shrouds with abradable seals are disclosed. A high temperature seal with an abradable coating is provided. The seal comprises a three-dimensional, high-density woven composite base structure recessed below the abradable coating, with loops incorporated in and protruding from the base structure. The abradable coating is integrally attached to the base structure via the loops. Additionally, a graded density seal is provided with a three-dimensional, low-density woven composite structure. The low-density structure is abradable. A three-dimensional, high-density woven composite base structure is recessed below the low-density structure, with the low-density structure integrally attached to the base structure via weaving.

    摘要翻译： 公开了用于制造具有可磨损密封件的改进的陶瓷复合涡轮机护罩的装置，系统和方法。 提供了具有耐磨涂层的高温密封。 密封件包括在可磨损涂层下面凹陷的三维，高密度织造复合基底结构，其中结合到基部结构中并从基部结构突出。 可磨损涂层通过环一体地附接到基底结构。 此外，分级密度密封件设置有三维低密度编织复合结构。 低密度结构是可磨损的。 三维，高密度织造复合基底结构凹陷在低密度结构下方，低密度结构通过编织整体连接到基座结构。

    Integral abradable seals
    2.
    发明授权
    Integral abradable seals 有权
    整体耐磨密封件

    公开(公告)号：US08309197B2

    公开(公告)日：2012-11-13

    申请号：US12316991

    申请日：2008-12-17

    申请人： Janet Davis ,  David Marshall ,  Olivier Sudre

    发明人： Janet Davis ,  David Marshall ,  Olivier Sudre

    IPC分类号： B32B7/02 ,  F01D11/08

    CPC分类号： D03D25/005 ,  B32B3/30 ,  B32B5/024 ,  B32B5/26 ,  B32B9/005 ,  B32B2262/105 ,  B32B2262/106 ,  B32B2307/554 ,  B32B2581/00 ,  B32B2605/18 ,  Y10T428/23914 ,  Y10T428/23957 ,  Y10T428/23979 ,  Y10T428/23986 ,  Y10T428/24992 ,  Y10T428/24996 ,  Y10T428/249967

    摘要： Devices, systems and methods for fabricating improved ceramic composite turbine shrouds with abradable seals are disclosed. A high temperature seal with an abradable coating is provided. The seal comprises a three-dimensional, high-density woven composite base structure recessed below the abradable coating, with loops incorporated in and protruding from the base structure. The abradable coating is integrally attached to the base structure via the loops. Additionally, a graded density seal is provided with a three-dimensional, low-density woven composite structure. The low-density structure is abradable. A three-dimensional, high-density woven composite base structure is recessed below the low-density structure, with the low-density structure integrally attached to the base structure via weaving.

    摘要翻译： 公开了用于制造具有可磨损密封件的改进的陶瓷复合涡轮机护罩的装置，系统和方法。 提供了具有耐磨涂层的高温密封。 密封件包括在可磨损涂层下面凹陷的三维，高密度织造复合基底结构，其中结合到基部结构中并从基部结构突出。 可磨损涂层通过环一体地附接到基底结构。 此外，分级密度密封件设置有三维低密度编织复合结构。 低密度结构是可磨损的。 三维，高密度编织复合基底结构在低密度结构下面凹陷，低密度结构通过编织整体连接到基座结构。

    Morphable ceramic composite skins and structures for hypersonic flight
    3.
    发明申请
    Morphable ceramic composite skins and structures for hypersonic flight 有权
    变形陶瓷复合材料和超音速飞行结构

    公开(公告)号：US20070262201A1

    公开(公告)日：2007-11-15

    申请号：US11432865

    申请日：2006-05-11

    申请人： Brian Cox ,  Janet Davis ,  Sergio Lucato ,  David Marshall ,  Brock McCabe ,  Olivier Sudre

    发明人： Brian Cox ,  Janet Davis ,  Sergio Lucato ,  David Marshall ,  Brock McCabe ,  Olivier Sudre

    IPC分类号： B64B1/14

    CPC分类号： B64C30/00 ,  B64D33/02 ,  B64D2033/026 ,  F02C7/042 ,  F05D2220/80 ,  F05D2300/2112 ,  F05D2300/224 ,  F05D2300/226 ,  F05D2300/2261 ,  F05D2300/228 ,  F05D2300/614 ,  Y02T50/672 ,  Y10T428/249928

    摘要： An exemplary morphable ceramic composite structure includes a flexible ceramic composite skin and a truss structure attached to the skin. The truss structure can morph shape of the skin from a first shape to a second shape that is different than the first shape. The flexible ceramic composite skin may include a single-layer of three-dimensional woven fabric fibers and a ceramic matrix composite. The truss structure may include at least one actuatable element or an actuator may move a portion of the truss structure from a first position to a second position. A cooling component may be disposed in thermal communication with the skin. The cooling component may include thermal insulation or a cooling system that circulates cooling fluid in thermal communication with the skin. The morphable ceramic composite structure may be incorporated into any of an air inlet, combustor, exhaust nozzle, or control surfaces of a hypersonic aircraft.

    摘要翻译： 示例性的变形陶瓷复合结构包括柔性陶瓷复合材料表皮和附着于皮肤的桁架结构。 桁架结构可以将皮肤的形状从第一形状变形为与第一形状不同的第二形状。 柔性陶瓷复合表皮可以包括单层三维织物纤维和陶瓷基复合材料。 桁架结构可以包括至少一个可启动元件，或者致动器可将桁架结构的一部分从第一位置移动到第二位置。 冷却部件可以设置成与皮肤热连通。 冷却部件可以包括热绝缘或冷却系统，其使冷却流体与皮肤热连通。 变形陶瓷复合结构可以结合到超音速飞机的空气入口，燃烧器，排气喷嘴或控制表面中的任何一个中。

    MATERIALS FOR SELF-TRANSPIRING HOT SKINS FOR HYPERSONIC VEHICLES OR REUSABLE SPACE VEHICLES
    4.
    发明申请
    MATERIALS FOR SELF-TRANSPIRING HOT SKINS FOR HYPERSONIC VEHICLES OR REUSABLE SPACE VEHICLES 有权
    用于超自行车或可重复使用的空间车辆的自发性皮肤的材料

    公开(公告)号：US20070252045A1

    公开(公告)日：2007-11-01

    申请号：US11380450

    申请日：2006-04-27

    申请人： Brian Cox ,  Janet Davis ,  Julia Mack ,  David Marshall ,  Peter Morgan ,  Olivier Sudre

    发明人： Brian Cox ,  Janet Davis ,  Julia Mack ,  David Marshall ,  Peter Morgan ,  Olivier Sudre

    IPC分类号： B64G1/52

    CPC分类号： B64G1/58 ,  B64G1/14

    摘要： A self-transpiring hot skin for a hypersonic or reusable space vehicle that can provide protection to the vehicle during short periods of abnormally high heat flux (either planned in the flight profile or an off-nominal event). The hot skin includes a ceramic composite structure having an internal cavity that is coupled either to the insulating layer or directly to the support structure of the hypersonic vehicle. The internal cavity includes a material system that vaporizes, sublimes or decomposes into a gas when the temperature exceeds the upper temperature capability of the composite material. The gas transpires through the outer layer of the composite material to provide cooling to the outer layer below the upper temperature capability. Cooling may occur both by conduction of heat from the composite material to the transpiring gas and by the interaction of the transpiring gas with the boundary layer of hypersonic flow over the outer surface, leading to a reduction of the heat flux entering the surface.

    摘要翻译： 用于超音速或可重复使用的空中交通工具的自发热皮肤，可在短时间内异常高的热通量（在飞行情况下计划或非标称事件）中为车辆提供保护。 热皮肤包括具有内腔的陶瓷复合结构，其内部耦合到绝缘层或直接连接到超音速车辆的支撑结构。 内部空腔包括当温度超过复合材料的较高温度能力时气化，升华或分解成气体的材料体系。 气体通过复合材料的外层渗透，以便在较高温度能力以下向外层提供冷却。 冷却可以通过从复合材料传导到蒸发气体以及蒸发气体与外表面上的超音速流动边界层的相互作用而发生，导致进入表面的热通量减少。

    Method and system for administering the hedging of an employee deferred compensation plan using swaps
    7.
    发明申请
    Method and system for administering the hedging of an employee deferred compensation plan using swaps 有权
    使用互换方式管理员工递延薪酬计划的对冲方法和制度

    公开(公告)号：US20050131798A1

    公开(公告)日：2005-06-16

    申请号：US10752213

    申请日：2004-01-06

    申请人： Clifford Eisler ,  David Marshall

    发明人： Clifford Eisler ,  David Marshall

    IPC分类号： G06F17/60

    CPC分类号： G06Q40/06 ,  G06Q40/02 ,  G06Q40/04 ,  G06Q40/10

    摘要： A method and system for administering the hedging of an employee deferred compensation plan, e.g., which employs hedging of NQDC plan liabilities using total return swaps and/or put and call options and/or forwards, for tax purposes. A plan coordinator coordinates a transfer of information between an employer/plan sponsor, a plan administrator that communicates with the employees/plan participants, and a balance sheet provider. The plan coordinator receives and reconciles data and then calculates and modifies relevant information for tax purposes and use in reports that are provided to the plan sponsor and balance sheet provider. Calculations and modifications for tax purposes allow the plan sponsor to reap tax benefits from the NQDC plan swap hedge. The reports include an upcoming transactions report, which indicates new compensation deferrals, reallocations of previously deferred compensation among specified indices, and withdrawals. A NQDC plan swap hedge re-weighting request report is prepared to notify the balance sheet provider of necessary changes to the NQDC plan swap hedge. Deferred compensation plan details and summary reports are also provided to show the plan information in both individual form and aggregated plan form. Moreover, swap details/summary reports, a put and call option details report, and a forward details report may be provided which indicates future payments that the balance sheet provider must pay the plan sponsor under the swap and/or option and/or forward hedge, as well as hedge instrument information in both in disaggregated individual form and aggregated form. A deferred compensation exposure/swap position summary report is based on differences between deferred compensation liabilities and NQDC plan swap hedges, which represent the plan sponsor's net risk or exposure.

    摘要翻译： 用于管理员工递延薪酬计划对冲的方法和系统，例如，为了税收目的，使用总回报掉期和/或置换和看涨期权和/或转账来对冲NQDC计划负债。 计划协调员协调雇主/计划发起人，与员工/计划参与者沟通的计划管理员和资产负债表提供者之间的信息转移。 计划协调员接收和核对数据，然后计算和修改税务相关信息，并在提供给计划发起人和资产负债表提供者的报告中使用。 计算和修改税务目的允许计划发起人从NQDC计划互换对冲中获得税收优惠。 这些报告包括即将到来的交易报告，其中指出新的赔偿延期，特定指数之间的以前延期赔偿的重新分配和撤回。 NQDC计划互换对冲重新加权请求报告准备向资产负债表提供者通报NQDC计划互换对冲的必要变更。 还提供递延薪酬计划细节和总结报告，以个人形式和汇总计划表格显示计划信息。 此外，可能会提供掉期细节/汇总报告，期权详情报告和期货详情报告，这些报表指示资产负债表提供者在交换和/或期权和/或远期套期保值下支付计划发起人的未来付款 ，以及分类个人形式和汇总形式的对冲工具信息。 递延薪酬敞口/掉期头寸摘要报告是根据递延薪酬负债与NQDC计划互换对冲之间的差异，代表计划发起人的净风险或风险敞口。

    Method and apparatus for compressing digital image data
    8.
    发明授权
    Method and apparatus for compressing digital image data 失效
    用于压缩数字图像数据的方法和装置

    公开(公告)号：US06512853B2

    公开(公告)日：2003-01-28

    申请号：US09011714

    申请日：1998-05-18

    申请人： Jonathan Marshall Thomas Kennedy ,  Simon Frederick Kennedy ,  Nicholas Paul Kennedy ,  David Marshall

    发明人： Jonathan Marshall Thomas Kennedy ,  Simon Frederick Kennedy ,  Nicholas Paul Kennedy ,  David Marshall

    IPC分类号： G06K936

    CPC分类号： H04N19/593

    摘要： A method for compressing digital image data with greyscale values comprises making at least three predictions of the greyscale value of each pixel and comparing the predicted values with the actual value of the pixel. The difference values between the respective predicted values and the actual value of each pixel is computed, and the median difference value of the three difference values is selected for bit coding. Bit coding is carried out by using variable length bit codes, the shortest length bit code being assigned to the most frequently occurring median difference value. The coded values of the median differences are bit packed, and in the case of a pixel where the absolute median difference value exceeds a predetermined value, the actual pixel value is bit packed.

    摘要翻译： 用灰度值压缩数字图像数据的方法包括对每个像素的灰度值进行至少三次预测，并将预测值与像素的实际值进行比较。 计算各个预测值与各像素的实际值之间的差值，并选择三个差分值的中值差值进行位编码。 通过使用可变长度位码来执行位编码，最短长度位码被分配给最频繁出现的中值差值。 中值差的编码值是位打包的，并且在绝对中值差值超过预定值的像素的情况下，实际像素值是位打包的。

    Water absorbing polymers
    9.
    发明授权
    Water absorbing polymers 失效
    吸水聚合物

    公开(公告)号：US5384343A

    公开(公告)日：1995-01-24

    申请号：US915887

    申请日：1992-07-20

    申请人： David Farrar ,  Peter Flesher ,  Malcolm Skinner ,  John Clarke ,  David Marshall

    发明人： David Farrar ,  Peter Flesher ,  Malcolm Skinner ,  John Clarke ,  David Marshall

    IPC分类号： C10L9/10 ,  C22B1/244 ,  C08K11/00

    CPC分类号： C22B1/244 ,  C10L9/10

    摘要： A water absorbing particulate polymer material wherein the polymer material when in dry powder form has a particle size of about 50 .mu.m to about 500 .mu.m and wherein the particles consist of internally bonded finer particles which finer particles have a size below 50 .mu.m. The process of using the water absorbing polymer, material to convert a wet sticky mass of inorganic particulate such as coal fines into a crumbly or flowable solid. A process using a water absorbing particulate polymer material to convert a wet sticky mass of organic particulate material into a crumbly or flowable solid wherein the organic matter can be, for example, food waste or sewage.

    摘要翻译： 一种吸水性粒状聚合物材料，其中当干粉形式的聚合物材料具有约50μm至约500μm的粒度，并且其中所述颗粒由内部粘合的较细颗粒组成，其中较细颗粒的尺寸低于50μm。 使用吸水性聚合物的过程是将湿的粘性物质如煤粉转化为易碎或可流动的固体。 一种使用吸水性粒状聚合物材料将湿粘性有机颗粒材料转化成易碎或可流动的固体的方法，其中有机物可以是例如食物废物或污水。