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    • 4. 发明申请
    • REFORMED MULTI-FUEL PREMIXED LOW EMISSION COMBUSTOR AND RELATED METHOD
    • 改进的多燃料低排放COMBUSTOR及相关方法
    • US20120186266A1
    • 2012-07-26
    • US13010828
    • 2011-01-21
    • Abdul Rafey KhanHasan KarimJonathan Dwight Berry
    • Abdul Rafey KhanHasan KarimJonathan Dwight Berry
    • F02C6/18F02G3/00
    • F02C3/20F02C7/22F23C2900/03002F23R3/28Y02T50/678
    • A reformer for use in a gas turbine engine specially configured to treat a supplemental fuel feed to the combustor that includes a reformer core containing a catalyst composition and an inlet flow channel for transporting the reformer fuel mixture, air and steam (either saturated or superheated) into a reformer core. An outlet flow channel transports the resulting reformate stream containing reformed and thermally cracked hydrocarbons and substantial amounts of hydrogen out of the reformer core for later combination with the main combustor feed. Because the catalytic partial oxidation reaction in the reformer is highly exothermic, the additional heat is transferred (and thermally integrated) using one or more heat exchange units for a first and/or second auxiliary gas turbine fuel stream that undergo thermal cracking and vaporization before combining with the reformate. The combined, hydrogen-enriched feed significantly improves combustor performance.
    • 一种用于燃气涡轮发动机的改质器,其特别构造为处理燃烧器的补充燃料,其包括含有催化剂组合物的重整器芯和用于输送重整器燃料混合物的入口流动通道,空气和蒸汽(饱和或过热) 进入重组核心。 出口流动通道将得到的重整产物流输送到重整器芯中,以便与主燃烧器进料混合。 因为重整器中的催化部分氧化反应是高度放热的,所以使用一个或多个用于在组合之前经受热裂解和蒸发的第一和/或第二辅助燃气轮机燃料流的热交换单元转移(并热集成)附加的热量 与重组。 组合的富氢进料显着提高了燃烧室性能。
    • 5. 发明授权
    • Reformed multi-fuel premixed low emission combustor and related method
    • 改进型多燃料预混低排放燃烧器及相关方法
    • US08931283B2
    • 2015-01-13
    • US13010828
    • 2011-01-21
    • Abdul Rafey KhanHasan KarimJonathan Dwight Berry
    • Abdul Rafey KhanHasan KarimJonathan Dwight Berry
    • F02C6/18F02C1/00F02C7/22F02C3/20F23R3/28F02C9/00F02C7/00F02C3/30
    • F02C3/20F02C7/22F23C2900/03002F23R3/28Y02T50/678
    • A reformer for use in a gas turbine engine specially configured to treat a supplemental fuel feed to the combustor that includes a reformer core containing a catalyst composition and an inlet flow channel for transporting the reformer fuel mixture, air and steam (either saturated or superheated) into a reformer core. An outlet flow channel transports the resulting reformate stream containing reformed and thermally cracked hydrocarbons and substantial amounts of hydrogen out of the reformer core for later combination with the main combustor feed. Because the catalytic partial oxidation reaction in the reformer is highly exothermic, the additional heat is transferred (and thermally integrated) using one or more heat exchange units for a first and/or second auxiliary gas turbine fuel stream that undergo thermal cracking and vaporization before combining with the reformate. The combined, hydrogen-enriched feed significantly improves combustor performance.
    • 一种用于燃气涡轮发动机的改质器,其特别构造为处理燃烧器的补充燃料进料,其包括含有催化剂组合物的重整器芯和用于输送重整器燃料混合物的入口流动通道,空气和蒸汽(饱和或过热) 进入重组核心。 出口流动通道将得到的重整产物流输送到重整器芯中,以便与主燃烧器进料混合。 因为重整器中的催化部分氧化反应是高度放热的,所以使用一个或多个用于在组合之前经受热裂解和蒸发的第一和/或第二辅助燃气轮机燃料流的热交换单元转移(并热集成)附加的热量 与重组。 组合的富氢进料显着提高了燃烧室性能。
    • 10. 发明授权
    • Impingement cooled transition piece aft frame
    • 冲击冷却过渡件后框架
    • US08707705B2
    • 2014-04-29
    • US12553153
    • 2009-09-03
    • Jonathan Dwight BerryKevin Weston McMahan
    • Jonathan Dwight BerryKevin Weston McMahan
    • F02C7/12
    • F23R3/002F01D9/023F23R2900/03043F23R2900/03044
    • An aft frame of a turbine engine transition piece body is provided and includes an annular body disposed within a first annular space defined between an impingement sleeve and a compressor discharge casing and aft of a second annular space defined between the transition piece body and the impingement sleeve and including a main portion with a first surface facing the first annular space and a second surface facing the forward annular space. The main portion has an impingement hole extending therethrough from an inlet at the first surface of the annular body to an outlet at the second surface of the annular body to define a fluid path along which the first and second annular spaces communicate with one another.
    • 提供了一种涡轮发动机过渡件本体的后框架,并且包括设置在限定在冲击套筒和压缩机排出壳体之间的第一环形空间内的环形体,以及限定在过渡件主体和冲击套筒之间的第二环形空间的后部 并且包括具有面向第一环形空间的第一表面的主要部分和面向前部环形空间的第二表面。 主要部分具有从环形体的第一表面处的入口延伸到环形体的第二表面处的出口的冲击孔,以限定第一和第二环形空间彼此连通的流体路径。