Catalyst combustion device
    11.
    发明授权
    Catalyst combustion device 失效
    催化剂燃烧装置

    公开(公告)号:US06394789B1

    公开(公告)日:2002-05-28

    申请号:US09622129

    申请日:2000-09-25

    IPC分类号: F23D340

    摘要: A catalytic combustion apparatus comprises a combustor 11, a fuel tank 12, a valve 13, and an ignition device 14. The combustor 11 further comprises a gas nozzle 16, an air intake/ejector 17, a mixing chamber 18, a firing chamber 19, an ignition plug 20, a combustion chamber 21, a catalyst for combustion 22 housed inside the combustion chamber 21, and an exhaust port 23. The mixing chamber 18 is made into a straight cylindrical passage, a cylindrical firing chamber 19 is provided in parallel to the mixing chamber 18 so that an opening 24 on the side of the firing chamber 19 communicates with the combustion chamber 21, a burner port 25 is disposed on the boundary between the mixing chamber 18 and the firing chamber 19, and the burner 25 is configured with a catalytic net 25a. With this configuration, a flame is formed on the upstream side of the catalyst for combustion 22, the catalyst for combustion 22 is heated by the heat of the flame to a catalytic combustion enabling temperature thus also effecting catalytic combustion on the catalytic net 25a. The flame spontaneously disappears, and the catalyst for combustion 22 commences catalytic combustion. As catalytic combustion can be effected without fail even when the combustion chamber 21 is configured into a low profile, the thickness of the catalytic body can be reduced without reducing the combustion characteristics, thereby enabling reduction in the height of the burner and providing a downsized and thin catalytic combustion apparatus.

    摘要翻译: 催化燃烧装置包括燃烧器11,燃料箱12,阀13和点火装置14.燃烧器11还包括气体喷嘴16,进气/喷射器17,混合室18,燃烧室19 ,火花塞20,燃烧室21,燃烧室21内的燃烧用催化剂22和排气口23.混合室18形成为直的圆筒状的通路,圆筒形的燃烧室19平行设置 到混合室18,使得在燃烧室19一侧的开口24与燃烧室21连通,在混合室18和燃烧室19之间的边界上设有燃烧口25,燃烧器25是 配置有催化网25a。 由此,在燃烧用催化剂22的上游侧形成有火焰,将燃烧用催化剂22通过火焰的热量加热至催化燃烧使能温度,从而也对催化剂网25a进行催化燃烧。 火焰自发消失,燃烧催化剂22开始催化燃烧。 即使当燃烧室21被构造成低轮廓时,即使催化燃烧也可以毫不费力地实现,可以在不降低燃烧特性的情况下降低催化剂体的厚度,从而能够降低燃烧器的高度并提供小型化和 薄催化燃烧装置。

    Catalytic combustion chamber and method for igniting and controlling the catalytic combustion chamber
    12.
    发明授权
    Catalytic combustion chamber and method for igniting and controlling the catalytic combustion chamber 失效
    催化燃烧室及催化燃烧室点火控制方法

    公开(公告)号:US06302683B1

    公开(公告)日:2001-10-16

    申请号:US09215971

    申请日:1998-12-18

    IPC分类号: F23D340

    摘要: Methods for operating catalytic combustion chambers including first and second catalytic reactors disposed in series with an intermediate chamber therebetween are disclosed, the method including heating the first catalytic reactor to a temperature at least equal to the ignition temperature of the first catalytic reactor, introducing air and fuel mixture to the first catalytic reactor whereby catalytic combustion is initiated in the first catalytic reactor, and increasing the mass flow through the first catalytic reactor whereby combustion of the air and fuel mixture takes place in the gas phase in the intermediate chamber and the end surface of the second catalytic reactor is heated to a temperature at least equal to the ignition temperature of the second catalytic reactor and ignition takes place in the second catalytic reactor.

    摘要翻译: 公开了用于操作催化燃烧室的方法,所述催化燃烧室包括与其间的中间室串联设置的第一和第二催化反应器,所述方法包括将所述第一催化反应器加热至至少等于所述第一催化反应器的着火温度的温度, 燃料混合物到第一催化反应器,由此在第一催化反应器中引发催化燃烧,并且增加通过第一催化反应器的质量流,由此空气和燃料混合物的燃烧在中间室和端面中的气相中发生 的第二催化反应器被加热到​​至少等于第二催化反应器的着火温度的温度,并且在第二催化反应器中发生点燃。

    Dry, low NOx pilot
    13.
    发明授权
    Dry, low NOx pilot 失效
    干,低NOx飞行员

    公开(公告)号:US06270337B1

    公开(公告)日:2001-08-07

    申请号:US09097176

    申请日:1998-06-12

    IPC分类号: F23D340

    摘要: This invention relates to an apparatus and method for increasing the reactivity of a fuel/air mixture prior to homogenous combustion of the mixture. More specifically, this invention is a pilot for a gas turbine combustor which utilizes the heat of combustion within the pilot to increase the reactivity of a portion of the fuel/air mixture utilized by the pilot.

    摘要翻译: 本发明涉及在混合物均匀燃烧之前提高燃料/空气混合物的反应性的装置和方法。 更具体地,本发明是用于燃气轮机燃烧器的先导,其利用飞行员内的燃烧热来增加飞行员利用的燃料/空气混合物的一部分的反应性。

    Combustion apparatus
    14.
    发明授权
    Combustion apparatus 失效
    燃烧装置

    公开(公告)号:US06224370B1

    公开(公告)日:2001-05-01

    申请号:US09109947

    申请日:1998-07-06

    IPC分类号: F23D340

    摘要: A combustion apparatus has a fuel supply section; an air blowing section for supplying combustion air; a mixing section for mixing the fuel with the combustion air; a plurality of first catalyst bodies which are arranged substantially in parallel with each other to divide the downstream location in the flow direction of mixture into a plurality of flow paths; and a first heat receiving section configured by a plurality of heat receiving fins arranged in flow paths divided by said first catalyst bodies and a cooling path penetrating the heat receiving fins, the opposed heat receiving fin and first catalyst body being characterized in that the area of the heat receiving fin on the upstream side of said cooling path is smaller than the area of the first catalyst body on the upstream side of the cooling path.

    摘要翻译: 燃烧装置具有燃料供给部; 用于供应燃烧空气的空气吹送部分; 用于将燃料与燃烧空气混合的混合部分; 多个第一催化剂体,其彼此大致平行配置,以将混合物的流动方向上的下游位置分成多个流路; 以及第一受热部,其由设置在由所述第一催化剂体分割的流路中的多个受热翅片和贯穿所述受热翅片的冷却路径构成,所述相对的受热翅片和所述第一催化剂体的特征在于, 所述冷却路径上游侧的受热翅片小于冷却路径上游侧的第一催化剂体的面积。