Gas turbine combustor and gas turbine generating apparatus
    7.
    发明授权
    Gas turbine combustor and gas turbine generating apparatus 失效
    燃气轮机燃烧器和燃气轮机发电装置

    公开(公告)号:US5349812A

    公开(公告)日:1994-09-27

    申请号:US10576

    申请日:1993-01-28

    IPC分类号: F23R3/26 F23R3/28 F02C9/50

    CPC分类号: F23R3/26

    摘要: A gas turbine combustor is capable of reducing NOx over a whole load range of a gas turbine. The combustor comprises two burner systems. It is possible to independently control a flow rate of combustion air supplied to a burner of the respective systems and a flow rate of bypass air jetted from through a bypass air port. The air supplied to the burners is mixed with fuel in a mixing chamber and then ejected into a combustion chamber so as to form a flame. The amount of bypass air is controlled in accordance with an operation load, a humidity of air and a heating value of fuel. It is therefore possible to prevent any blow off and reduce NOx over the whole load range of the gas turbine.

    摘要翻译: 燃气轮机燃烧器能够在燃气轮机的整个负载范围内减少NOx。 燃烧器包括两个燃烧器系统。 可以独立地控制供给到各个系统的燃烧器的燃烧空气的流量和从旁通空气口喷射的旁路空气的流量。 供给燃烧器的空气与混合室中的燃料混合,然后喷射到燃烧室中以形成火焰。 旁路空气的量根据操作负荷,空气湿度和燃料的热值来控制。 因此,可以防止在燃气轮机的整个负载范围内的任何吹出和减少NOx。

    Stabilizer for gas turbine combustors and gas turbine combustor equipped
with the stabilizer
    9.
    发明授权
    Stabilizer for gas turbine combustors and gas turbine combustor equipped with the stabilizer 失效
    配有稳定器的燃气轮机燃烧器和燃气轮机燃烧器稳定器

    公开(公告)号:US6026644A

    公开(公告)日:2000-02-22

    申请号:US700882

    申请日:1996-08-21

    摘要: A gas turbine combustor has a premixing burner for jetting out a premixed gas of fuel and air. A stabilizer forms a circulation of combustion gas generated by combustion of the premixed gas at the downstream side of the stabilizer to stabilize flame formed by the combustion of the premixed gas. Before the operation of the combustor, a relationship between a temperature of the stabilizer and combustion conditions of the premixed gas is checked. Thereafter during operation of the combustor, the temperature of the stabilizer is measured during combustion and the combustion conditions are checked according to only the measured temperature of the stabilizer and the aforesaid relationship. The stabilizer has a heat receiving surface at the most downstream side thereof. The temperature of a portion of the stabilizer around the heat receiving surfaces measured to allow an accurate assessment of the combustion conditions.

    摘要翻译: 燃气轮机燃烧器具有用于喷射燃料和空气的预混合气体的预混合燃烧器。 稳定剂在稳定剂的下游侧形成由预混气体燃烧产生的燃烧气体的循环,以稳定由预混气体燃烧形成的火焰。 在燃烧器的操作之前,检查稳定器的温度与预混合气体的燃烧条件之间的关系。 此后,在燃烧器的运行期间,在燃烧期间测量稳定器的温度,并且仅根据稳定器的测量温度和上述关系检查燃烧条件。 稳定器在其最下游侧具有受热面。 测量了受热表面周围的一部分稳定器的温度,以便准确地评估燃烧条件。