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    • 1. 发明授权
    • Method and apparatus for a catalytic firebox reactor
    • 用于催化火炉反应器的方法和装置
    • US06174159B1
    • 2001-01-16
    • US09272395
    • 1999-03-18
    • Lance L. SmithShahrokh EtemadHasan UlkarimMarco J. CastaldiWilliam C. Pfefferle
    • Lance L. SmithShahrokh EtemadHasan UlkarimMarco J. CastaldiWilliam C. Pfefferle
    • F23D1418
    • F23C13/00
    • A catalytic firebox reactor employing an exothermic catalytic reaction channel and multiple cooling conduits for creating a partially reacted fuel/oxidant mixture. An oxidation catalyst is deposited on the walls forming the boundary between the multiple cooling conduits and the exothermic catalytic reaction channel, on the side of the walls facing the exothermic catalytic reaction channel. This configuration allows the oxidation catalyst to be backside cooled by any fluid passing through the cooling conduits. The heat of reaction is added to both the fluid in the exothermic catalytic reaction channel and the fluid passing through the cooling conduits. After discharge of the fluids from the exothermic catalytic reaction channel, the fluids mix to create a single combined flow. A further innovation in the reactor incorporates geometric changes in the exothermic catalytic reaction channel to provide streamwise variation of the velocity of the fluids in the reactor.
    • 使用放热催化反应通道的催化火炉反应器和用于产生部分反应的燃料/氧化剂混合物的多个冷却管道。 氧化催化剂沉积在形成多个冷却导管和放热催化反应通道之间边界壁的壁上,面对放热催化反应通道。 这种构造允许氧化催化剂由通过冷却导管的任何流体背面冷却。 反应热量加入放热催化反应通道中的流体和通过冷却管道的流体。 在从放热催化反应通道排出流体之后,流体混合以产生单一的组合流。 反应器中的进一步创新包括放热催化反应通道中的几何变化,以提供反应器中流体速度的流动变化。
    • 5. 发明申请
    • Compact aircraft combustor
    • 紧凑型飞机燃烧器
    • US20110079016A1
    • 2011-04-07
    • US12924671
    • 2010-09-30
    • Shahrokh EtemadBenjamin D. BairdSubir RoychoudhuryWilliam C. Pfefferle
    • Shahrokh EtemadBenjamin D. BairdSubir RoychoudhuryWilliam C. Pfefferle
    • F02C6/18F23R3/04F02C6/04F02C7/264
    • F23R3/40F23C6/045F23C13/06F23C2900/03002F23C2900/9901F23R3/286F23R3/32Y02T50/678
    • The present invention provides a combustor for an aerospace gas turbine engine comprising two stages wherein each stage defines an inlet and an exit. The second stage inlet is in fluid communication with the first stage exit such that a first flowpath is defined and it passes substantially through the second stage. A plurality of flow channel tubes is positioned within the second stage and each flow channel tube passes sealingly through a header plate positioned upstream of the second stage inlet thereby defining a second flowpath that also passes substantially through the second stage. The first flowpath exit and the second flowpath exit are positioned adjacent and proximate to one another to provide for the generation of microflames or microflame jets exiting the second stage from between and around the flow channel tube exits. The first stage of the combustor provides a gasifier and a reformer. The present invention also may comprise an igniter for further combustion of the reacted products or an external heat source for start-up. The second stage also may comprise a microflame combustor.
    • 本发明提供一种用于航空航天燃气涡轮发动机的燃烧器,其包括两个阶段,其中每个阶段限定入口和出口。 第二级入口与第一级出口流体连通,使得限定第一流动路径,并且其基本上通过第二级。 多个流动通道管定位在第二阶段内,并且每个流动通道管密封地穿过位于第二阶段入口上游的集管板,从而限定也基本上通过第二阶段的第二流动路径。 第一流路出口和第二流路出口相邻并且靠近彼此定位,以提供从流动通道管出口之间和周围离开第二阶段的微火焰或微火焰射流的产生。 燃烧器的第一阶段提供气化器和重整器。 本发明还可以包括用于进一步燃烧反应产物的点火器或用于启动的外部热源。 第二阶段还可以包括微火焰燃烧器。
    • 7. 发明授权
    • Catalytic reactor for low-Btu fuels
    • 用于低Btu燃料的催化反应器
    • US07521028B2
    • 2009-04-21
    • US11261190
    • 2005-10-27
    • Lance SmithShahrokh EtemadHasan KarimWilliam C. Pfefferle
    • Lance SmithShahrokh EtemadHasan KarimWilliam C. Pfefferle
    • B01J8/04F23D21/00
    • B01J8/067B01J8/062B01J8/065B01J12/007B01J2208/00132B01J2219/00081F28D7/0041
    • An improved catalytic reactor includes a housing having a plate positioned therein defining a first zone and a second zone, and a plurality of conduits fabricated from a heat conducting material and adapted for conducting a fluid therethrough. The conduits are positioned within the housing such that the conduit exterior surfaces and the housing interior surface within the second zone define a first flow path while the conduit interior surfaces define a second flow path through the second zone and not in fluid communication with the first flow path. The conduit exits define a second flow path exit, the conduit exits and the first flow path exit being proximately located and interspersed. The conduits define at least one expanded section that contacts adjacent conduits thereby spacing the conduits within the second zone and forming first flow path exit flow orifices having an aggregate exit area greater than a defined percent of the housing exit plane area. Lastly, at least a portion of the first flow path defines a catalytically active surface.
    • 改进的催化反应器包括壳体,其具有定位在其中的板,其中限定第一区域和第二区域,以及由导热材料制成并适于传导流体通过其中的多个管道。 导管定位在壳体内,使得导管外表面和第二区域内的壳体内表面限定第一流动路径,同时导管内表面限定穿过第二区域的第二流动路径并且不与第一流体流体连通 路径。 导管出口限定第二流动路径出口,导管离开并且第一流动路径出口被近似定位并散布。 导管限定了至少一个膨胀部分,其接触相邻的管道,从而将第二区域内的管道隔开并形成第一流路出口流动孔口,其具有大于壳体出口平面面积的限定百分比的总出口面积。 最后,第一流路的至少一部分限定催化活性表面。