Combustor for gas turbine
    3.
    发明授权
    Combustor for gas turbine 失效
    燃气轮机燃烧器

    公开(公告)号:US4926645A

    公开(公告)日:1990-05-22

    申请号:US387146

    申请日:1989-07-31

    IPC分类号: F02C7/22 F23R3/40

    CPC分类号: F23R3/40

    摘要: A catalytic combustor for a gas turbine comprises catalyst layers arranged in two stages in a direction of gas flow. Fuel supply nozzles are disposed close to and upstream of the downstream catalyst layer. A substantially constant amount of fuel is supplied from the fuel supply nozzles to form pilot flames by the downstream catalyst layer, which are above 1000 degrees C. and below 1500 degrees C. Combustible component having passed through the upstream catalyst layer is burned by the pilot flames.

    摘要翻译: 用于燃气轮机的催化燃烧器包括沿气流方向分成两级的催化剂层。 燃料供给喷嘴设置在下游催化剂​​层附近和上游。 从燃料供给喷嘴供给大致恒定量的燃料,通过下游催化剂​​层形成先导火焰,该催化剂层高于1000℃,低于1500℃。通过上游催化剂层的可燃组分被飞行员 火焰

    Gas turbine combustor
    4.
    发明授权
    Gas turbine combustor 失效
    燃气轮机燃烧器

    公开(公告)号:US5836164A

    公开(公告)日:1998-11-17

    申请号:US593087

    申请日:1996-01-29

    摘要: A gas turbine combustor includes a diffusion combustor arranged at an axis portion of a combustion chamber for effecting diffusion combustion, a plurality of first premixing combustors arranged at an outer periphery of the diffusion combustor for effecting premixed combustion, each of the plurality of first premixing combustors being formed so that a mixture outlet end thereof projects more downstream than a fuel outlet end of the diffusion combustor, and a plurality of second premixing combustors each formed so that a mixture outlet thereof projects more downstream than the mixture outlet end of the first combustor, wherein the first premixing combustors and the second premixing combustors are arranged alternately at the outer periphery of the diffusion combustor, and wherein a swirler is provided on the first premixing combustor in the vicinity of the mixture outlet end thereof for swirling mixture.

    摘要翻译: 燃气轮机燃烧器包括布置在燃烧室的轴线部分以进行扩散燃烧的扩散燃烧器,多个第一预混合燃烧器,其布置在扩散燃烧室的外周处以实现预混合燃烧;多个第一预混合燃烧器 形成为使得其混合物出口端比扩散燃烧器的燃料出口端更下游突出,并且多个第二预混合燃烧器各自形成为使得其混合物出口比第一燃烧器的混合物出口端更下游突出, 其中所述第一预混合燃烧器和所述第二预混合燃烧器交替地布置在所述扩散燃烧器的外周,并且其中在所述第一预混合燃烧器的混合物出口端附近设置旋流器以进行旋转混合。

    Combustion apparatus and combustion method therein
    5.
    发明授权
    Combustion apparatus and combustion method therein 失效
    燃烧装置及其燃烧方法

    公开(公告)号:US5259182A

    公开(公告)日:1993-11-09

    申请号:US17174

    申请日:1993-02-12

    IPC分类号: F23R3/08 F23R3/14 F23R3/06

    摘要: A combustion apparatus comprises a combustor liner forming a combustion chamber, and a swirler for introducing a fuel gas into the combustion chamber in the form of a swirl. The combustor liner has an air film forming device provided on the wall thereof and capable of forming a film of cooling air on the inner peripheral wall of the combustor liner so as to protect the combustor liner from the hot combustion gas in the combustion chamber. The air film forming means is formed such that the flowing direction of the air forming the film becomes the same direction as the swirling direction of the combustion gas, so that the film of the cooling air is not broken by the hot combustion gas.

    摘要翻译: 燃烧装置包括形成燃烧室的燃烧器衬套和用于以涡流形式将燃料气体引入燃烧室的旋流器。 燃烧器衬套具有设置在其壁上并能够在燃烧器衬套的内周壁上形成冷却空气膜的空气膜形成装置,以保护燃烧器衬套免受燃烧室内的热燃烧气体的影响。 空气膜形成装置形成为使得形成膜的空气的流动方向与燃烧气体的旋转方向成相同的方向,使得冷却空气的膜不被热燃烧气体破坏。

    Method and device for controlling combustors for gasturbine
    7.
    发明授权
    Method and device for controlling combustors for gasturbine 失效
    用于控制燃气燃烧器的方法和装置

    公开(公告)号:US5461855A

    公开(公告)日:1995-10-31

    申请号:US193354

    申请日:1994-02-03

    CPC分类号: F01D17/085 F23R3/26

    摘要: A method for controlling a plurality of combustors supplying a pressurized gas to a gas turbine, with each of the combustors including a first air supply for supplying a combustion air into the combustor and a second air supply for adjusting an amount of air supplied into the combustor to change a combustion condition in the combustor. The method comprises the steps of measuring the combustion condition of each of the combustors, measuring a difference between the measured combustion condition of each of the combustors and a desired combustion condition, and changing a rate of the amount of air supplied into the combustor by the second air supply means in relation to an amount of combustion air supplied into the combustor by the first air supply in each of the combustors according to the measured difference of each of the combustors to change the combustion condition of each of the combustors so that the combustion conditions of the combustors are changed to the desired combustion condition.

    摘要翻译: 一种用于控制向燃气轮机供应加压气体的多个燃烧器的方法,其中每个燃烧器包括用于向燃烧器供应燃烧空气的第一空气供应器和用于调节供应到燃烧器中的空气量的第二空气供应器 以改变燃烧器中的燃烧状态。 该方法包括以下步骤:测量每个燃烧器的燃烧条件,测量每个燃烧器的测量的燃烧条件与期望的燃烧条件之间的差异,以及改变供应到燃烧器中的空气的量的速率 第二空气供给装置相对于通过每个燃烧器中的第一空气供应供应到燃烧器中的燃烧空气的量,根据每个燃烧器的测量差异来改变每个燃烧器的燃烧条件,使得燃烧 燃烧器的条件改变为期望的燃烧条件。

    Solenoid valve
    10.
    发明授权
    Solenoid valve 失效
    电磁阀

    公开(公告)号:US4546795A

    公开(公告)日:1985-10-15

    申请号:US662555

    申请日:1984-10-19

    IPC分类号: F16K31/06 F16K31/02

    摘要: A solenoid valve in which a pulse signal is applied to an electromagnet thereof to eliminate an electric hysteresis. The solenoid valve includes a piston-like valve slidably supported in a cylinder, and at least one aperture, for communicating with a fluid inlet and a fluid outlet, provided in at least one of the valve and cylinder, whereby the flow rate of a fluid may be continuously controlled and the collision between the valve and a valve seat may be avoided.

    摘要翻译: 电磁阀,其中脉冲信号被施加到其电磁体以消除电滞后。 电磁阀包括可滑动地支撑在气缸中的活塞状阀以及设置在阀和气缸中的至少一个中的至少一个用于与流体入口和流体出口连通的孔,由此流体的流速 可以连续地控制并且可以避免阀和阀座之间的碰撞。