Reformer system and method reforming
    1.
    发明申请
    Reformer system and method reforming 审中-公开
    改革者制度和方法改革

    公开(公告)号:US20070086934A1

    公开(公告)日:2007-04-19

    申请号:US11248162

    申请日:2005-10-13

    IPC分类号: B01J19/00 C01B3/26 H01M8/06

    摘要: A reformer system has a reformer for converting a hydrocarbon-containing fuel to a hydrogen-gas-rich reformate gas, and an HC adsorber, which is connected to an output side of the reformer and adsorbs, as a function of temperature, hydrocarbons contained in the reformate gas, or for desorbing previously adsorbed hydrocarbons to the reformate gas. The reformer system transmits the reformate gas after passing through the HC adsorber to a consuming device. The chronological progression of the adsorption/desorption behavior of the HC adsorber during an operating phase of the reformer as a function of the reformate gas temperature occurring in the operating phase and/or a temperature gradient of the reformate gas occurring in the operating phase is coordinated with the chronological progression of the operating behavior of the consuming device such that a significant desorption of hydrocarbons from the HC adsorber takes place only when the consuming device is in an operating condition in which the desorbed hydrocarbons are processed by the consuming device such that the hydrocarbon fraction of the gases expelled from the consuming device and/or the function of the consuming device is/are not significantly influenced by the desorbed hydrocarbons.

    摘要翻译: 重整器系统具有用于将含烃燃料转化为富氢重整气体的重整器,和连接到重整器的输出侧并吸附作为温度的函数的HC吸附器,其包含在 重整气体,或将先前吸附的烃解吸到重整气体中。 重整器系统通过HC吸附器将重整气体传送到消耗装置。 在重整器的操作阶段期间,HC吸附剂在操作阶段发生的重整产物气体温度和/或在操作阶段发生的重整气体的温度梯度的函数的HC吸附剂的吸附/解吸行为的时间顺序进行协调 随着消耗装置的操作行为的时间顺序进行,使得仅当消耗装置处于其中解吸的烃被消耗装置处理的操作状态时才从HC吸附器显着解吸烃,使得烃 从消耗装置排出的气体的分数和/或消耗装置的功能不受解吸烃的显着影响。

    Operating method for a system composed of a reformer and a catalytic exhaust gas aftertreatment device
    3.
    发明授权
    Operating method for a system composed of a reformer and a catalytic exhaust gas aftertreatment device 失效
    由重整器和催化废气后处理装置组成的系统的操作方法

    公开(公告)号:US08015803B2

    公开(公告)日:2011-09-13

    申请号:US12273166

    申请日:2008-11-18

    IPC分类号: F01N3/00

    摘要: An operating method for a system including a reformer which in reformate mode can convert hydrocarbon-containing fuel to a hydrogen-rich reformate gas, and a catalytic exhaust gas aftertreatment device which is acted upon by reformer gas to reach the catalytic converter light-off temperature more rapidly. During cold starts, the reformer, after its own starting phase, is initially operated in a so-called lean-burn mode, and the reformer is switched from lean-burn mode to reformate mode as soon as combustible constituents in the catalytic aftertreatment device can be independently oxidized. During the reformer lean-burn mode, the combustible constituents of the engine's exhaust gas react with the hot reformer gas, such that the cumulative exhaust gas flow has the composition of exhaust gas generated by stoichiometric combustion.

    摘要翻译: 一种用于包括重整器模式的重整器的系统的操作方法,其可以将含烃燃料转化为富氢重整气体,并且通过重整器气体作用于催化转化器的关闭温度的催化废气后处理装置 更快 在冷启动期间,改造者在其起始阶段之后最初以所谓的稀燃方式运行,一旦催化后处理装置中的可燃成分就可以从重燃模式切换到重燃模式 被独立氧化。 在重整器稀燃模式中,发动机废气的可燃成分与热重整器气体反应,使得累积废气流具有由化学计量燃烧产生的废气的组成。

    Operating Method for a System Composed of a Reformer and a Catalytic Exhaust Gas Aftertreatment Device
    4.
    发明申请
    Operating Method for a System Composed of a Reformer and a Catalytic Exhaust Gas Aftertreatment Device 失效
    由改造器和催化废气后处理装置组成的系统的操作方法

    公开(公告)号:US20090071420A1

    公开(公告)日:2009-03-19

    申请号:US12273166

    申请日:2008-11-18

    IPC分类号: F02B43/00 F01N3/00 F01N3/20

    摘要: An operating method for a system including a reformer which in reformate mode can convert hydrocarbon-containing fuel to a hydrogen-rich reformate gas, and a catalytic exhaust gas aftertreatment device which is acted upon by reformer gas to reach the catalytic converter light-off temperature more rapidly. During cold starts, the reformer, after its own starting phase, is initially operated in a so-called lean-burn mode, and the reformer is switched from lean-burn mode to reformate mode as soon as combustible constituents in the catalytic aftertreatment device can be independently oxidized. During the reformer lean-burn mode, the combustible constituents of the engine's exhaust gas react with the hot reformer gas, such that the cumulative exhaust gas flow has the composition of exhaust gas generated by stoichiometric combustion.

    摘要翻译: 一种用于包括重整器模式的重整器的系统的操作方法,其可以将含烃燃料转化为富氢重整气体,并且通过重整器气体作用于催化转化器的关闭温度的催化废气后处理装置 更快 在冷启动期间,改造者在其起始阶段之后最初以所谓的稀燃方式运行,一旦催化后处理装置中的可燃成分就可以从重燃模式切换到重燃模式 被独立氧化。 在重整器稀燃模式中,发动机废气的可燃成分与热重整器气体反应,使得累积废气流具有由化学计量燃烧产生的废气的组成。

    Compressor of a gas turbine
    5.
    发明授权
    Compressor of a gas turbine 有权
    燃气轮机的压缩机

    公开(公告)号:US08333553B2

    公开(公告)日:2012-12-18

    申请号:US12528436

    申请日:2008-02-14

    IPC分类号: F04D29/54 F04D29/64

    摘要: The invention relates to a compressor, particularly a high pressure compressor, of a gas turbine, particularly of a gas turbine aircraft engine, having at least one rotating blade ring on the rotor side, and having at least one guide blade ring on the stator side, wherein the, or each, guide blade ring is formed of a plurality of guide blade segments, and wherein each guide blade segment is formed of a plurality of individual blades. According to the invention, adjacent individual blades (11, 12; 12, 13; 13, 14) are permanently connected to each other within each guide blade segment (10) of at least one guide blade ring on opposing surfaces positioned radially outward, whereas the same are not connected to each other on opposing surfaces positioned radially inward.

    摘要翻译: 本发明涉及一种特别是燃气轮机飞机发动机的燃气轮机的压缩机,特别是高压压缩机,其具有在转子侧上的至少一个旋转叶片环,并且在定子侧具有至少一个导向叶片环 其中所述导向叶片环或每个引导叶片环由多个引导叶片段形成,并且其中每个引导叶片段由多个单独叶片形成。 根据本发明,相邻的单个叶片(11,12; 12,13; 13,14)在位于径向向外定位的相对表面上的至少一个引导叶片环的每个引导叶片段(10)内彼此永久连接,而 它们在径向向内定位的相对表面上彼此不相连。

    COMPRESSOR OF A GAS TURBINE
    6.
    发明申请
    COMPRESSOR OF A GAS TURBINE 有权
    气体涡轮压缩机

    公开(公告)号:US20100322758A1

    公开(公告)日:2010-12-23

    申请号:US12528436

    申请日:2008-02-14

    IPC分类号: F01D11/00

    摘要: The invention relates to a compressor, particularly a high pressure compressor, of a gas turbine, particularly of a gas turbine aircraft engine, having at least one rotating blade ring on the rotor side, and having at least one guide blade ring on the stator side, wherein the, or each, guide blade ring is formed of a plurality of guide blade segments, and wherein each guide blade segment is formed of a plurality of individual blades. According to the invention, adjacent individual blades (11, 12; 12, 13; 13, 14) are permanently connected to each other within each guide blade segment (10) of at least one guide blade ring on opposing surfaces positioned radially outward, whereas the same are not connected to each other on opposing surfaces positioned radially inward.

    摘要翻译: 本发明涉及一种特别是燃气轮机飞机发动机的燃气轮机的压缩机,特别是高压压缩机,其具有在转子侧上的至少一个旋转叶片环,并且在定子侧具有至少一个导向叶片环 其中所述导向叶片环或每个引导叶片环由多个引导叶片段形成,并且其中每个引导叶片段由多个单独叶片形成。 根据本发明,相邻的单个叶片(11,12; 12,13; 13,14)在位于径向向外定位的相对表面上的至少一个引导叶片环的每个引导叶片段(10)内彼此永久连接,而 它们在径向向内定位的相对表面上彼此不相连。