Compact mixer for the mixing of gaseous hydrocarbon and gaseous oxidants
    5.
    发明申请
    Compact mixer for the mixing of gaseous hydrocarbon and gaseous oxidants 有权
    用于混合气态烃和气态氧化剂的紧凑型混合器

    公开(公告)号:US20060201065A1

    公开(公告)日:2006-09-14

    申请号:US11076286

    申请日:2005-03-09

    IPC分类号: C01B3/24 B01J8/04 B01J10/00

    摘要: Embodiments include methods and apparatus for mixing feedgases and producing synthesis gas. The apparatus includes a vessel containing a mixing system comprising one or more channels and a reaction zone downstream of the mixing system. A first feedgas and a second feedgas are separately injected into different injection portions of each channel, such that the second feedgas is injected in an acute direction into the first feedgas flowstream. The injected feedgases thereafter mix in a mixing portion of the channel. The mixing portion of each channel may have a reduced cross-sectional area so as to increase the total velocity of the feedgases while they mix. A feedgas mixture exits each channel of the mixing system to feed the reaction zone where it gets converted. Preferred embodiments include mixing O2 with a hydrocarbon gas and converting the mixture in a catalytic reaction zone to produce synthesis gas.

    摘要翻译: 实施例包括用于混合进料气并生产合成气的方法和装置。 该装置包括容纳包含一个或多个通道的混合系统和混合系统下游的反应区的容器。 第一进料气和第二进料气分别注入每个通道的不同喷射部分,使得第二进料气体沿急性方向注入第一进料气流。 然后,注入的进料气体在通道的混合部分中混合。 每个通道的混合部分可以具有减小的横截面积,以便在它们混合时增加进料气体的总速度。 进料气混合物离开混合系统的每个通道,以将反应区送入其中进行转化。 优选的实施方案包括将O 2 O 2与烃气混合并在催化反应区中转化混合物以产生合成气。

    HYDROGEN SEPARATION PROCESS
    6.
    发明申请
    HYDROGEN SEPARATION PROCESS 有权
    氢分离方法

    公开(公告)号:US20080000350A1

    公开(公告)日:2008-01-03

    申请号:US11671344

    申请日:2007-02-05

    IPC分类号: B01D53/22 B29C47/76 B32B15/00

    摘要: A method for separating a hydrogen-rich product stream from a feed stream comprising hydrogen and at least one carbon-containing gas, comprising feeding the feed stream, at an inlet pressure greater than atmospheric pressure and a temperature greater than 200° C., to a hydrogen separation membrane system comprising a membrane that is selectively permeable to hydrogen, and producing a hydrogen-rich permeate product stream on the permeate side of the membrane and a carbon dioxide-rich product raffinate stream on the raffinate side of the membrane. A method for separating a hydrogen-rich product stream from a feed stream comprising hydrogen and at least one carbon-containing gas, comprising feeding the feed stream, at an inlet pressure greater than atmospheric pressure and a temperature greater than 200° C., to an integrated water gas shift/hydrogen separation membrane system wherein the hydrogen separation membrane system comprises a membrane that is selectively permeable to hydrogen, and producing a hydrogen-rich permeate product stream on the permeate side of the membrane and a carbon dioxide-rich product raffinate stream on the raffinate side of the membrane. A method for pretreating a membrane, comprising: heating the membrane to a desired operating temperature and desired feed pressure in a flow of inert gas for a sufficient time to cause the membrane to mechanically deform; decreasing the feed pressure to approximately ambient pressure; and optionally, flowing an oxidizing agent across the membrane before, during, or after deformation of the membrane. A method of supporting a hydrogen separation membrane system comprising selecting a hydrogen separation membrane system comprising one or more catalyst outer layers deposited on a hydrogen transport membrane layer and sealing the hydrogen separation membrane system to a porous support.

    摘要翻译: 一种从含有氢气和至少一种含碳气体的进料流中分离富氢产物流的方法,包括在大于大气压和大于200℃的入口压力下将进料流进料至大于200℃的温度, 氢分离膜系统,其包括选择性地可渗透氢的膜,并且在膜的渗透侧产生富氢渗透物产物流和在膜的萃余液侧上的富含二氧化碳的产物萃余液流。 一种从含有氢气和至少一种含碳气体的进料流中分离富氢产物流的方法,包括在大于大气压和大于200℃的入口压力下将进料流进料至大于200℃的温度, 一种集成的水煤气变换/氢分离膜系统,其中氢分离膜系统包括选择性渗透氢的膜,并且在膜的渗透侧产生富氢渗透物产物流和富含二氧化碳的产物残液 在膜的萃余液侧流。 一种用于预处理膜的方法,包括:将所述膜在惰性气体流中加热到所需的操作温度和所需的进料压力足够的时间以使膜机械地变形; 将进料压力降至约环境压力; 并且任选地,在膜的变形之前,期间或之后使氧化剂流过膜。 一种支撑氢分离膜系统的方法,包括选择氢分离膜系统,其包含沉积在氢输送膜层上的一个或多个催化剂外层,并将氢分离膜系统密封到多孔载体上。

    On-line device for predicting at least one fluid flow parameter in a process
    9.
    发明授权
    On-line device for predicting at least one fluid flow parameter in a process 有权
    用于在过程中预测至少一个流体流参数的在线设备

    公开(公告)号:US06564157B2

    公开(公告)日:2003-05-13

    申请号:US09729921

    申请日:2000-12-06

    IPC分类号: G01F100

    摘要: An on-line device for predicting at least one fluid flow parameter in a process includes structure and/or function whereby a flow domain has disposed therein a pre-determined portion in which a fluid flows. Preferably, the device includes a computer having: (i) a memory for receiving a database, the database including relative information in respect of a plurality of nodes or a plurality of particle pathways in the pre-determined portion; (ii) structure to receive input data from the process, and (iii) structure to calculate the at least one fluid flow parameter from the database and the input data. The device is particularly advantageously employed as a UV dosimeter.

    摘要翻译: 用于在过程中预测至少一个流体流动参数的在线装置包括结构和/或功能,其中流动域在其中设置流体流动的预定部分。 优选地,该设备包括具有以下功能的计算机:(i)用于接收数据库的存储器,所述数据库包括关于预定部分中的多个节点或多个粒子路径的相关信息; (ii)从过程接收输入数据的结构,以及(iii)从数据库和输入数据计算至少一个流体流量参数的结构。 该装置特别有利地用作UV剂量计。

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    10.
    发明公开

    公开(公告)号:US20240317410A1

    公开(公告)日:2024-09-26

    申请号:US18653441

    申请日:2024-05-02

    申请人: Harold Wright

    发明人: Harold Wright

    IPC分类号: B64D25/12 B64C1/14 B64D17/80

    摘要: A “G” load suppressing aircraft incorporating a fuselage having a nose end; a cavity, extending downwardly into the fuselage, the cavity opening upwardly at the fuselage's nose end; a cockpit capsule fitted for receipt within the cavity; explosive bolts for releasably attaching the cockpit capsule to the fuselage, the explosive bolts holding the cockpit capsule within the cavity; a liquid supply line for filling the cockpit capsule with a transparent liquid, the liquid supply line being connected operatively to the cockpit capsule; and rocket engines for ejecting the cockpit capsule from the cavity, the rocket engines being connected operatively to the cockpit.