SYSTEM AND METHOD FOR CRYOGENIC COOLING
    91.
    发明申请
    SYSTEM AND METHOD FOR CRYOGENIC COOLING 审中-公开
    冷冻冷却系统及方法

    公开(公告)号:US20120038120A1

    公开(公告)日:2012-02-16

    申请号:US13106180

    申请日:2011-05-12

    摘要: In accordance with an embodiment of the invention, there is provided a system for cooling a load. The system comprises a closed loop primary refrigeration system comprising: a primary compressor taking in a primary refrigerant at a low pressure and discharging the primary refrigerant at a high pressure; an insulated enclosure comprising an inlet receiving the primary refrigerant at the high pressure from the primary compressor and an outlet returning the primary refrigerant at the low pressure to the primary compressor; at least one heat exchanger within the insulated enclosure receiving the primary refrigerant at the high pressure and cooling the primary refrigerant using a secondary refrigerant from a secondary refrigeration system, the secondary refrigerant being in heat exchange relationship with the primary refrigerant in the at least one heat exchanger; an expansion unit within the insulated enclosure receiving the primary refrigerant at the high pressure from the at least one heat exchanger and discharging the primary refrigerant at the low pressure; and a supply line delivering the primary refrigerant at the low pressure to the load and a return line returning the primary refrigerant from the load to the primary refrigeration system. The system further comprises the secondary refrigeration system, wherein the secondary refrigeration system comprises at least one secondary cryogenic refrigerator. A system control unit controls operation of at least one of the primary refrigeration system and the secondary refrigeration system to provide a variable refrigeration capacity to the load based on at least one of: a pressure of the primary refrigerant delivered to the load, and at least one temperature of the load.

    摘要翻译: 根据本发明的实施例,提供了一种用于冷却负载的系统。 该系统包括闭环主要制冷系统,其包括:初级压缩机,其在低压下接收初级制冷剂并在高压下排出初级制冷剂; 绝缘外壳,其包括接收来自主压缩机的高压下的初级制冷剂的入口和将低压下的初级制冷剂返回到主压缩机的出口; 所述绝热壳体内的至少一个热交换器接收高压下的初级制冷剂并且使用来自二次制冷系统的二次制冷剂冷却所述初级制冷剂,所述二次制冷剂在所述至少一个热量中与所述初级制冷剂处于热交换关系 交换器 所述绝缘壳体内的膨胀单元接收来自所述至少一个热交换器的高压下的所述初级制冷剂,并且在所述低压下排出所述初级制冷剂; 以及将低压下的一次制冷剂输送到负载的供给管线和将一次制冷剂从负载返回到主制冷系统的返回管路。 该系统还包括二次制冷系统,其中次级制冷系统包括至少一个二次低温冰箱。 系统控制单元控制主要制冷系统和次级制冷系统中的至少一个的操作,以向负载提供可变制冷能力,其基于以下至少一个:输送到负载的一次制冷剂的压力,并且至少 一个温度的负载。

    Method of determining and controlling the inertial attitude of a spinning, artificial satellite and systems therefor
    92.
    发明申请
    Method of determining and controlling the inertial attitude of a spinning, artificial satellite and systems therefor 失效
    确定和控制旋转,人造卫星及其系统的惯性姿态的方法

    公开(公告)号:US20080087769A1

    公开(公告)日:2008-04-17

    申请号:US11818723

    申请日:2007-06-15

    申请人: William Johnson

    发明人: William Johnson

    IPC分类号: B64G1/36 B64G1/32

    摘要: A method of and apparatus for determining and controlling the inertial attitude of a spinning artificial satellite without using a suite of inertial gyroscopes. The method and apparatus operate by tracking three astronomical objects near the Earth's ecliptic pole and the satellite's and/or star tracker's spin axis and processing the track information. The method and apparatus include steps and means for selecting preferably three astronomical objects using a histogram method and determining a square of a first radius (R12) of a track of a first astronomical object; determining a square of a second radius (R22) of a track of a second astronomical object; determining a square of a third radius (R32) of a track of a third astronomical object; determining the inertial attitude of the spin axis using the squares of the first, second, and third radii (R12, R22, and R32) to calculate pitch, yaw, and roll rate; determining a change in the pitch and yaw of the artificial satellite; and controlling on-board generated current flow to various orthogonally-disposed current-carrying loops to act against the Earth's magnetic field and to apply gyroscopic precession to the spinning satellite to correct and maintain its optimum inertial attitude.

    摘要翻译: 用于在不使用一套惯性陀螺仪的情况下确定和控制旋转人造卫星的惯性姿态的方法和装置。 该方法和装置通过跟踪地球黄道附近的三个天文物体和卫星和/或星形跟踪器的自旋轴进行操作并处理轨道信息。 所述方法和装置包括用于使用直方图方法优选地选择三个天文物体并且确定一个轨道的第一半径的平方的步骤和装置(R 1> 1 < 第一个天文物体; 确定第二天文物体的轨道的第二半径(R 2 2&lt; 2&gt; 2&gt;)的平方; 确定第三天文物体的轨道的第三半径(R 3 3 2)的平方; 使用第一,第二和第三半径的平方(R 1,L 2,R 2,...,SUP)来确定自旋轴的惯性姿态 > 2&lt; 3&gt;和R 3&lt; 2&gt; 2)以计算俯仰,偏航和滚动速率; 确定人造卫星的俯仰和偏航的变化; 并且控制板上产生的电流流向各种正交布置的载流回路,以对地球的磁场起作用,并对旋转卫星施加陀螺进动,以校正和保持其最佳惯性姿态。

    Amorphous metal foam as a property-matched bone scaffold substitute
    93.
    发明申请
    Amorphous metal foam as a property-matched bone scaffold substitute 有权
    无定形金属泡沫作为属性匹配的骨架替代品

    公开(公告)号:US20080060725A1

    公开(公告)日:2008-03-13

    申请号:US11891992

    申请日:2007-08-13

    IPC分类号: C22C45/00 C21D1/00

    摘要: Amorphous metal foams and methods of making the same are provided. The amorphous metal foams have properties matching those of natural bone, enabling their use as bone replacement scaffolds. In one embodiment, for example, an amorphous metal foam has a density-dependent stiffness (or Young's modulus, denoted E) ranging from about 640ρ3.75 τo αβoντ 2900ρ0.78, and a density dependent strength (σy) greater than about 8.1ρ2.57, wherein ρ (the density) is less than about 1.7 g/cc.

    摘要翻译: 提供无定形金属泡沫及其制备方法。 非晶金属泡沫具有与天然骨相匹配的特性,使其能够用作骨替代支架。 在一个实施方案中,例如,非晶态金属泡沫体具有范围从约640立方米3.75英寸2900微米至0.78克的密度依赖刚度(或杨氏模量,表示为E),以及 大于约8.1微米×2.57的密度依赖强度(σσy),其中rho(密度)小于约1.7g / cc。

    Towable backhoe
    94.
    发明申请
    Towable backhoe 审中-公开
    拖曳反铲

    公开(公告)号:US20080000652A1

    公开(公告)日:2008-01-03

    申请号:US11804206

    申请日:2007-05-17

    申请人: William Johnson

    发明人: William Johnson

    IPC分类号: A01B35/32

    CPC分类号: E02F9/003 E02F9/024

    摘要: A towable backhoe having a frame with a pair of hydraulically indirectly operated front wheels and a pair of rear wheels. The front wheels include lock out hubs. The rear wheels can be configured between a lowered work configuration and a raised towing configuration. The backhoe includes a rear hitch for connecting to a towing vehicle in the towing configuration.

    摘要翻译: 一种带有一对液压间接操作的前轮和一对后轮的框架的可拖曳的反铲车。 前轮包括锁定中心。 后轮可以在下降的工作配置和升高的牵引配置之间配置。 该反铲装置包括用于在拖曳配置中连接到牵引车辆的后连接件。

    Method of maintaining a data log related to a programmable logic controller (PLC)
    95.
    发明申请
    Method of maintaining a data log related to a programmable logic controller (PLC) 有权
    维护与可编程逻辑控制器(PLC)相关的数据记录的方法

    公开(公告)号:US20070300021A1

    公开(公告)日:2007-12-27

    申请号:US11899115

    申请日:2007-09-04

    IPC分类号: G06F12/00

    摘要: Certain exemplary embodiments can provide a method for utilizing a memory cartridge connected to a Programmable Logic Controller (PLC). The memory cartridge can comprise a plurality of memory segments. The method can comprise a plurality of activities comprising: providing a default identifying stamp for records in a data log file, a structure for the data log file stored separately from the data log file in the memory cartridge, and obtaining a request to provide the data log file.

    摘要翻译: 某些示例性实施例可以提供一种利用连接到可编程逻辑控制器(PLC)的存储器盒的方法。 存储器盒可以包括多个存储器段。 该方法可以包括多个活动,包括:为数据日志文件中的记录提供默认标识标记,与存储盒中的数据日志文件分开存储的数据日志文件的结构,以及获得提供数据的请求 日志文件。

    Method of reducing gaseous inclusions in a glass making process
    97.
    发明申请
    Method of reducing gaseous inclusions in a glass making process 有权
    在玻璃制造过程中还原气态夹杂物的方法

    公开(公告)号:US20070175241A1

    公开(公告)日:2007-08-02

    申请号:US11732463

    申请日:2007-04-03

    IPC分类号: C03B5/16

    CPC分类号: C03B5/193 C03B5/225

    摘要: Feed materials are melted in a first vessel to form a glass melt at a first temperature T1, the glass melt containing at least one fining agent. The molten glass is next cooled to a second temperature T2 less than T1 in a second vessel wherein an oxygen-comprising gas is not actively added (e.g. bubbled) into the melt during the duration of the time the melt is at T2. The molten glass is thereafter heated to a third temperature T3 greater than T1 and subsequently formed into a glass article.

    摘要翻译: 进料在第一容器中熔化以在第一温度T 1下形成玻璃熔体,玻璃熔体含有至少一种澄清剂。 在第二容器中将熔融玻璃冷却至小于T 1 N 2的第二温度T 2以下,其中不将含氧气体(例如鼓泡)加入 在熔体处于T 2时间的持续时间内熔化。 然后将熔融玻璃加热到大于T 1的第三温度T 3 3℃,随后形成玻璃制品。

    Fe-base in-situ compisite alloys comprising amorphous phase
    98.
    发明申请
    Fe-base in-situ compisite alloys comprising amorphous phase 有权
    包含非晶相的Fe基原位合金合金

    公开(公告)号:US20070079907A1

    公开(公告)日:2007-04-12

    申请号:US10573148

    申请日:2004-10-01

    IPC分类号: C22C45/02

    CPC分类号: C22C45/02 C22C38/00

    摘要: An Fe-base in-situ composite alloy, castable into 3-dimensional bulk objects, where the alloy includes a matrix having one or both of a nano-crystalline phase and an amorphous phase, and a face-centered cubic crystalline phase. The alloy has an Fe content more than 60 atomic percent.

    摘要翻译: 一种Fe基原位复合合金,可浇铸成3维体积物质,其中合金包括具有纳米晶相和非晶相中的一个或两个的基体和面心立方晶体相。 该合金的Fe含量大于60原子%。

    Method of producing composite members having increased strength
    99.
    发明申请
    Method of producing composite members having increased strength 审中-公开
    具有增加强度的复合构件的制造方法

    公开(公告)号:US20070045886A1

    公开(公告)日:2007-03-01

    申请号:US11507358

    申请日:2006-08-21

    申请人: William Johnson

    发明人: William Johnson

    摘要: This invention relates to extruded composite materials specifically focusing on the increasing load bearing capacity and the overall strength of composites. Injectable conformable structural core materials are used to replace foam cells inside extruded composite materials thereby increasing the overall load bearing stability and strength. The core materials are tailored to have a desired CTE with respect to the structural materials. The core materials may also incorporate fibers and solid structural fillers for increasing the strength of the composite member. The objective is to enable composite materials to have the highest structural load bearing capability possible so that these technologies can be used as the replacement of wood, in aerospace applications and for other purposes.

    摘要翻译: 本发明涉及挤出复合材料,其特别涉及增加的承载能力和复合材料的总体强度。 可注射的适形结构芯材料用于替代挤压复合材料内的泡沫细胞,从而提高整体承载稳定性和强度。 核心材料被定制成相对于结构材料具有期望的CTE。 芯材料还可以加入纤维和固体结构填料以增加复合构件的强度。 目的是使复合材料具有最高的结构承载能力,使得这些技术可以用作木材的替代品,在航空航天应用中和用于其它目的。