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    Distributed combustion process and burner
    3.
    发明授权
    Distributed combustion process and burner 有权
    分布式燃烧过程和燃烧器

    公开(公告)号：US08827691B2

    公开(公告)日：2014-09-09

    申请号：US12848132

    申请日：2010-07-31

    申请人： Rajeev S. Prabhakar ,  Remi Pierre Tsiava ,  Magnus Mortberg ,  Benoit Grand ,  Bertrand Leroux ,  Vivek Gautam

    发明人： Rajeev S. Prabhakar ,  Remi Pierre Tsiava ,  Magnus Mortberg ,  Benoit Grand ,  Bertrand Leroux ,  Vivek Gautam

    IPC分类号： F23C5/00 ,  F23D14/32 ,  F23D14/22

    CPC分类号： F23D14/32 ,  F23C2900/07022 ,  F23C2900/99001 ,  F23D14/22 ,  Y02E20/342 ,  Y02E20/344

    摘要： During a heating phase, injection of a jet of fuel and oxidant (fuel annularly enshrouding oxidant or oxidant annularly enshrouding fuel) from a fuel-oxidant nozzle is combusted in a combustion space. During a transition from the heating phase to a distributed combustion phase, an amount of a secondary portion of either the fuel or oxidant is injected as a jet into the combustion space while the primary portion of that same reactant from the fuel-oxidant nozzle is decreased. At some point during the transition phase, a jet of actuating fluid is injected at an angle towards the jet of reactants from the fuel-oxidant nozzle and/or towards the jet of the secondary portion of reactant. The jet of primary portions of reactants and/or secondary portion of reactant is caused to be bent/deviated towards the other of the two jets. The staging of the secondary portion of reactant is increased until a desired degrees of staging and commencement of a distributed combustion phase are achieved.

    摘要翻译： 在加热阶段期间，从燃料 - 氧化剂喷嘴喷射燃料和氧化剂（燃料环形地包围氧化剂或氧化剂，环形地封闭的燃料）在燃烧空间中燃烧。 在从加热阶段到分散燃烧阶段的过渡期间，燃料或氧化剂的二次部分的量作为射流注入燃烧空间，同时来自燃料 - 氧化剂喷嘴的相同反应物的主要部分减少 。 在过渡阶段的某个时刻，致动流体的射流以一定角度注入来自燃料 - 氧化剂喷嘴和/或反应物次级部分的射流的反应物射流。 引起反应物的主要部分和/或反应物的次要部分的射流朝向两个射流中的另一个弯曲/偏离。 反应物的次级部分的分级增加，直到实现分散燃烧阶段的期望程度的分段和开始。

    DISTRIBUTED COMBUSTION PROCESS AND BURNER
    4.
    发明申请
    DISTRIBUTED COMBUSTION PROCESS AND BURNER 审中-公开
    分布式燃烧过程和燃烧器

    公开(公告)号：US20120009531A1

    公开(公告)日：2012-01-12

    申请号：US12848131

    申请日：2010-07-31

    申请人： Rajeev S. Prabhakar ,  Remi Pierre TSIAVA ,  Magnus MORTBERG ,  Vivek GAUTAM ,  Benoit GRAND ,  Bertrand LEROUX

    发明人： Rajeev S. Prabhakar ,  Remi Pierre TSIAVA ,  Magnus MORTBERG ,  Vivek GAUTAM ,  Benoit GRAND ,  Bertrand LEROUX

    IPC分类号： F23C5/08 ,  F23K5/06 ,  F23D14/22 ,  F23L7/00

    CPC分类号： F23D14/32 ,  F23C2900/07022 ,  F23C2900/99001 ,  F23D14/22 ,  Y02E20/342 ,  Y02E20/344

    摘要： During a heating phase, injection of a jet of fuel and oxidant (fuel annularly enshrouding oxidant or oxidant annularly enshrouding fuel) from a fuel-oxidant nozzle is combusted in a combustion space. During a transition from the heating phase to a distributed combustion phase, an amount of a secondary portion of either the fuel or oxidant is injected as a jet into the combustion space while the primary portion of that same reactant from the fuel-oxidant nozzle is decreased. At some point during the transition phase, a jet of actuating fluid is injected at an angle towards the jet of reactants from the fuel-oxidant nozzle and/or towards the jet of the secondary portion of reactant. The jet of primary portions of reactants and/or secondary portion of reactant is caused to be bent/deviated towards the other of the two jets. The staging of the secondary portion of reactant is increased until a desired degrees of staging and commencement of a distributed combustion phase are achieved.

    摘要翻译： 在加热阶段期间，从燃料 - 氧化剂喷嘴喷射燃料和氧化剂（燃料环形地包围氧化剂或氧化剂，环形地封闭的燃料）在燃烧空间中燃烧。 在从加热阶段到分散燃烧阶段的过渡期间，燃料或氧化剂的二次部分的量作为射流注入燃烧空间，同时来自燃料 - 氧化剂喷嘴的相同反应物的主要部分减少 。 在过渡阶段的某个时刻，致动流体的射流以一定角度注入来自燃料 - 氧化剂喷嘴和/或反应物次级部分的射流的反应物射流。 引起反应物的主要部分和/或反应物的次要部分的射流朝向两个射流中的另一个弯曲/偏离。 反应物的次级部分的分级增加，直到实现分散燃烧阶段的期望程度的分段和开始。