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    Method and apparatus to produce synthetic gas
    5.
    发明授权
    Method and apparatus to produce synthetic gas 有权
    生产合成气的方法和装置

    公开(公告)号：US08685120B2

    公开(公告)日：2014-04-01

    申请号：US12538949

    申请日：2009-08-11

    申请人： Kenneth M. Sprouse ,  Shahram Farhangi ,  Robert M. Saxelby

    发明人： Kenneth M. Sprouse ,  Shahram Farhangi ,  Robert M. Saxelby

    IPC分类号： F16K49/00 ,  B01J7/00

    CPC分类号： C10J3/506 ,  C10J2200/152 ,  C10J2300/093 ,  C10J2300/0959 ,  C10J2300/0973 ,  F23D1/005 ,  Y02E20/16 ,  Y02E20/18 ,  Y10T137/6416

    摘要： A method of producing a synthetic gas (syngas) includes injecting a plurality of reactant streams into a gasification reactor via at least one injection device having a plurality of injection annuli, an inner portion that extends annularly about a centerline extending through the at least one injection device, and an outer portion extending substantially annularly about the inner portion. At least a portion of the outer portion is oriented obliquely with respect to the at least one injection device centerline. The method also includes mixing at least a portion of each of the streams together such that a plurality of recirculation zones is defined by the streams. The method further includes producing a syngas within the recirculation zones via mixing at least a portion of each of the streams. The injection device includes an inner portion that extends annularly about a centerline extending through the injection device. The device also includes an outer portion extending substantially annularly about the inner portion that includes at least one of at least one carbonaceous reactant injection port oriented obliquely with respect to the injection device centerline and at least one outer face oriented obliquely with respect to the injection device centerline.

    摘要翻译： 一种生产合成气体（合成气）的方法包括通过至少一个具有多个注射环的注射装置将多个反应物流注入气化反应器，内部部分围绕延伸穿过至少一个注射器的中心线环形延伸 装置，以及围绕内部大致环形延伸的外部部分。 外部部分的至少一部分相对于至少一个注射装置中心线倾斜定向。 该方法还包括将每个流的至少一部分混合在一起，使得由流限定多个再循环区。 该方法还包括通过混合每个流的至少一部分在再循环区内产生合成气。 注射装置包括围绕延伸穿过注射装置的中心线环形延伸的内部部分。 该装置还包括围绕内部基本上环形地延伸的外部部分，该外部部分包括相对于注射装置中心线倾斜定向的至少一个碳质反应物注入口中的至少一个和相对于注射装置倾斜定向的至少一个外表面 中心线。

    METHOD AND APPARATUS TO PRODUCE SYNTHETIC GAS
    6.
    发明申请
    METHOD AND APPARATUS TO PRODUCE SYNTHETIC GAS 有权
    生产合成气体的方法和装置

    公开(公告)号：US20110036011A1

    公开(公告)日：2011-02-17

    申请号：US12538949

    申请日：2009-08-11

    申请人： Kenneth M. Sprouse ,  Shahram Farhangi ,  Robert M. Saxelby

    发明人： Kenneth M. Sprouse ,  Shahram Farhangi ,  Robert M. Saxelby

    IPC分类号： C10J3/68 ,  C10J3/00 ,  F16K49/00

    CPC分类号： C10J3/506 ,  C10J2200/152 ,  C10J2300/093 ,  C10J2300/0959 ,  C10J2300/0973 ,  F23D1/005 ,  Y02E20/16 ,  Y02E20/18 ,  Y10T137/6416

    摘要： A method of producing a synthetic gas (syngas) includes injecting a plurality of reactant streams into a gasification reactor via at least one injection device having a plurality of injection annuli, an inner portion that extends annularly about a centerline extending through the at least one injection device, and an outer portion extending substantially annularly about the inner portion. At least a portion of the outer portion is oriented obliquely with respect to the at least one injection device centerline. The method also includes mixing at least a portion of each of the streams together such that a plurality of recirculation zones is defined by the streams. The method further includes producing a syngas within the recirculation zones via mixing at least a portion of each of the streams. The injection device includes an inner portion that extends annularly about a centerline extending through the injection device. The device also includes an outer portion extending substantially annularly about the inner portion that includes at least one of at least one carbonaceous reactant injection port oriented obliquely with respect to the injection device centerline and at least one outer face oriented obliquely with respect to the injection device centerline.

    摘要翻译： 一种生产合成气体（合成气）的方法包括通过至少一个具有多个注射环的注射装置将多个反应物流注入气化反应器，内部部分围绕延伸穿过至少一个注射器的中心线环形延伸 装置，以及围绕内部大致环形延伸的外部部分。 外部部分的至少一部分相对于至少一个注射装置中心线倾斜定向。 该方法还包括将每个流的至少一部分混合在一起，使得由流限定多个再循环区。 该方法还包括通过混合每个流的至少一部分在再循环区内产生合成气。 注射装置包括围绕延伸穿过注射装置的中心线环形延伸的内部部分。 该装置还包括围绕内部基本上环形地延伸的外部部分，该外部部分包括相对于注射装置中心线倾斜定向的至少一个碳质反应物注入口中的至少一个和相对于注射装置倾斜定向的至少一个外表面 中心线。

    Method of fabricating a rocket engine combustion chamber
    7.
    发明授权
    Method of fabricating a rocket engine combustion chamber 失效
    制造火箭发动机燃烧室的方法

    公开(公告)号：US5249357A

    公开(公告)日：1993-10-05

    申请号：US9908

    申请日：1993-01-27

    申请人： Richard R. Holmes ,  Timothy N. McKechnie ,  Christopher A. Power ,  Ronald L. Daniel, Jr. ,  Robert M. Saxelby

    发明人： Richard R. Holmes ,  Timothy N. McKechnie ,  Christopher A. Power ,  Ronald L. Daniel, Jr. ,  Robert M. Saxelby

    IPC分类号： B23P15/00 ,  C23C4/12 ,  F02K9/64

    CPC分类号： B23P15/008 ,  C23C4/134 ,  F02K9/64 ,  Y10T29/49346

    摘要： A process for making a combustion chamber for a rocket engine wherein a copper alloy in particle form is injected into a stream of heated carrier gas in plasma form which is then projected onto the inner surface of a hollow metal jacket having the configuration of a rocket engine combustion chamber. The particles are in the plasma stream for a sufficient length of time to heat the particles to a temperature such that the particles will flatten and adhere to previously deposited particles but will not spatter or vaporize. After a layer is formed, cooling channels are cut in the layer, than the channels are filled with a temporary filler and another layer of particles is deposited.

    摘要翻译： 一种用于制造用于火箭发动机的燃烧室的方法，其中将颗粒形式的铜合金注入到等离子体形式的加热载气流中，然后将其投影到具有火箭发动机构型的中空金属护套的内表面上 燃烧室。 颗粒在等离子体流中足够长的时间以将颗粒加热到使得颗粒变平并粘附到先前沉积的颗粒但不会飞溅或蒸发的温度。 在形成层之后，在层中切割冷却通道，而不是用临时填料填充通道，并沉积另一层颗粒。

    Injector assembly for a fluid fueled engine
    8.
    发明授权
    Injector assembly for a fluid fueled engine 失效
    用于流体燃料发动机的喷射器组件

    公开(公告)号：US4801092A

    公开(公告)日：1989-01-31

    申请号：US93068

    申请日：1987-08-31

    申请人： William T. Webber ,  Robert M. Saxelby

    发明人： William T. Webber ,  Robert M. Saxelby

    IPC分类号： B05B7/08 ,  F02K9/52 ,  F23D11/38 ,  B05B7/06

    CPC分类号： F23D11/38 ,  B05B7/0807 ,  B05B7/0892 ,  F02K9/52

    摘要： An injector assembly 10 for injecting propellants into a fluid fueled rocket engine. Injection assembly 10 comprises a plate member 12 with an opening 16 therethrough. Injector element 14 is sealed within opening 16. Oxidizer flows through central bore 18 and through orifices 26 into combustion chamber 27. Fuel flows from passageway 34 into an annular manifold 38 formed at an interface between flanged portion 32 and plate member 12. Fuel is then injected through orifices 42 into combustion chamber 27 where it impinges with the oxidizer at predetermined points in the combustion chamber 27.

    摘要翻译： 用于将推进剂喷射到流体燃料火箭发动机中的喷射器组件10。 注射组件10包括具有穿过其中的开口16的板构件12。 注射器元件14密封在开口16内。氧化剂流过中心孔18并通过孔口26进入燃烧室27.燃料从通道34流入形成在凸缘部分32和板构件12之间的界面处的环形歧管38中。然后燃料 通过孔42注入到燃烧室27中，在燃烧室27中与燃烧室27中的预定点与氧化剂碰撞。