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    PREMIXED PARTIAL OXIDATION SYNGAS GENERATOR
    1.
    发明申请
    PREMIXED PARTIAL OXIDATION SYNGAS GENERATOR 审中-公开
    预先部分氧化症候群发生器

    公开(公告)号：US20070249738A1

    公开(公告)日：2007-10-25

    申请号：US11380059

    申请日：2006-04-25

    申请人： Joel Haynes ,  John Herbon ,  Anthony Dean ,  Mohamed Ali

    发明人： Joel Haynes ,  John Herbon ,  Anthony Dean ,  Mohamed Ali

    IPC分类号： C07C27/06 ,  B01J19/00 ,  B01J3/00

    CPC分类号： C10G2/32

    摘要： A premixed partial oxidation (POx) syngas generator is provided. The syngas generator includes a premixing device configured to mix a fuel stream and oxygen in a premixing region to form a gaseous pre-mix. The premixing device includes a fuel inlet configured to introduce the fuel stream within the premixing device and a flow conditioning device configured to pre-condition the fuel stream. The premixing device also includes an oxygen inlet configured to introduce oxygen into the fuel stream to facilitate premixing of the fuel stream and oxygen in the premixing region located downstream of the flow conditioning device. The syngas generator also includes a combustion chamber configured to combust the gaseous pre-mix from the premixing device to produce a synthesis gas enriched with carbon monoxide and hydrogen gas.

    摘要翻译： 提供了一种预混合的部分氧化（PO x SO 2）合成气发生器。 合成气发生器包括预混合装置，其被配置为在预混合区域中混合燃料流和氧气以形成气态预混合物。 预混合装置包括配置成将燃料流引入预混合装置内的燃料入口和被配置为预处理燃料流的流量调节装置。 预混合装置还包括构造成将氧气引入燃料流中的氧气入口，以便于位于流动调节装置下游的预混合区域中的燃料流和氧气的预混合。 合成气发生器还包括燃烧室，该燃烧室被配置为从预混合装置燃烧气态预混物，以产生富含一氧化碳和氢气的合成气体。

    Trapped vortex combustor cavity manifold for gas turbine engine
    4.
    发明申请
    Trapped vortex combustor cavity manifold for gas turbine engine 审中-公开
    用于燃气涡轮发动机的捕获涡流燃烧器腔歧管

    公开(公告)号：US20060107667A1

    公开(公告)日：2006-05-25

    申请号：US10994833

    申请日：2004-11-22

    申请人： Joel Haynes ,  Benjamin Hojnacki

    发明人： Joel Haynes ,  Benjamin Hojnacki

    IPC分类号： F23R3/30

    CPC分类号： F23R3/346 ,  F23R3/286

    摘要： In accordance with one embodiment, the present technique provides a combustor assembly for use in a gas-turbine device. The combustor assembly includes a first combustion zone and a second combustion zone. The combustor assembly further includes a first premix chamber configured to receive a fuel and air to facilitate a first fuel-air mixture having a first fuel-to-air ratio, wherein the first premix chamber is fluidiclly coupled to the combustion chamber at the first combustion zone. The combustor assembly also includes a second premix chamber configured to receive a fuel and air to facilitate a second fuel-air mixture having a second fuel-to-air ratio, wherein the second premix chamber is fluidiclly coupled to the combustion chamber at the second combustion zone, wherein the second combustion zone is radially outboard of the first combustion zone.

    摘要翻译： 根据一个实施例，本技术提供了一种用于燃气涡轮机装置中的燃烧器组件。 燃烧器组件包括第一燃烧区和第二燃烧区。 燃烧器组件还包括第一预混合室，其构造成容纳燃料和空气，以便于具有第一燃料与空气的第一燃料 - 空气混合物，其中第一预混合室在第一燃烧时流体地联接到燃烧室 区。 燃烧器组件还包括第二预混合室，其构造成接收燃料和空气以便于具有第二燃料 - 空气比的第二燃料 - 空气混合物，其中第二预混合室在第二燃烧时流体地联接到燃烧室 区，其中所述第二燃烧区在所述第一燃烧区的径向外侧。

    Non-infectious, non-replicating, immunogenic human immunodeficiency virus-like particles
    5.
    发明授权
    Non-infectious, non-replicating, immunogenic human immunodeficiency virus-like particles 失效
    非感染性，非复制型，免疫原性人类免疫缺陷病毒样颗粒

    公开(公告)号：US07008784B1

    公开(公告)日：2006-03-07

    申请号：US09389364

    申请日：1999-09-03

    申请人： Joel Haynes ,  Michel Henri Klein ,  Benjamin Rovinski ,  Shi Xian Cao

    发明人： Joel Haynes ,  Michel Henri Klein ,  Benjamin Rovinski ,  Shi Xian Cao

    IPC分类号： C12N7/04

    CPC分类号： C07K14/005 ,  A61K39/00 ,  C12N2740/16023 ,  C12N2740/16122

    摘要： The present invention is directed toward methods for the production of non-infectious, replication-deficient, immunogenic human immunodeficiency virus (HIV)-like particles. These particles are prepared from a recombinant expression vector comprising a heterologous promoter operatively connected to a DNA molecule comprising a modified HIV genome devoid of the long terminal repeat (LTR) regulatory regions but containing at least the gag and pol genes in their natural genomic arrangement. This vector is introduced into mammalian cells to produce the particles of interest. These particles should prove useful in a number of diagnostic, virologic, and immunologic applications.

    摘要翻译： 本发明涉及生产非感染性，复制缺陷型，免疫原性人类免疫缺陷病毒（HIV）样颗粒的方法。 这些颗粒由包含异源启动子的重组表达载体制备，所述异源启动子可操作地连接到DNA分子，所述DNA分子包含缺乏长末端重复（LTR）调节区但在其天然基因组排列中至少含有gag和pol基因的修饰的HIV基因组。 将该载体导入哺乳动物细胞以产生感兴趣的颗粒。 这些颗粒应证明在许多诊断，病毒学和免疫学应用中是有用的。

    GAS TURBINE ENGINE COMBUSTOR CAN WITH TRAPPED VORTEX CAVITY
    9.
    发明申请
    GAS TURBINE ENGINE COMBUSTOR CAN WITH TRAPPED VORTEX CAVITY 有权
    燃气涡轮发动机可以搭配VORTEX CAVITY

    公开(公告)号：US20050034458A1

    公开(公告)日：2005-02-17

    申请号：US10762993

    申请日：2004-01-22

    申请人： David Burrus ,  Narendra Joshi ,  Joel Haynes ,  Alan Feitelberg

    发明人： David Burrus ,  Narendra Joshi ,  Joel Haynes ,  Alan Feitelberg

    IPC分类号： F23R3/18 ,  F02C7/18 ,  F23R3/06 ,  F23R3/28 ,  F23R3/32 ,  F23R3/34 ,  F23R3/58 ,  F23R3/42

    CPC分类号： F23R3/346 ,  F23C2900/07001 ,  F23D2900/14004 ,  F23R3/283 ,  F23R3/286 ,  F23R3/58 ,  F23R2900/00015

    摘要： A gas turbine engine combustor can downstream of a pre-mixer has a pre-mixer flowpath therein and circumferentially spaced apart swirling vanes disposed across the pre-mixer flowpath. A primary fuel injector is positioned for injecting fuel into the pre-mixer flowpath. A combustion chamber surrounded by an annular combustor liner disposed in supply flow communication with the pre-mixer. An annular trapped dual vortex cavity located at an upstream end of the combustor liner is defined between an annular aft wall, an annular forward wall, and a circular radially outer wall formed therebetween. A cavity opening at a radially inner end of the cavity is spaced apart from the radially outer wall. Air injection first holes are disposed through the forward wall and air injection second holes are disposed through the aft wall. Fuel injection holes are disposed through at least one of the forward and aft walls.

    摘要翻译： 在预混合器下游的燃气涡轮发动机燃烧器具有预混合器流动路径，并且横跨预混合器流动路径设置周向间隔开的涡流叶片。 主燃料喷射器定位成将燃料喷射到预混合器流路中。 由环形燃烧器衬套围绕的燃烧室，其设置成与预混合器供应流动连通。 位于燃烧器衬套的上游端的环形捕获双涡流腔限定在环形后壁，环形前壁和形成在其间的圆形径向外壁。 在空腔的径向内端处的空腔开口与径向外壁间隔开。 空气注入第一孔穿过前壁设置，空气注入第二孔穿过后壁。 燃料喷射孔通过前壁和后壁中的至少一个设置。