Clearance control system
    1.
    发明授权
    Clearance control system 失效
    清关控制系统

    公开(公告)号:US4893984A

    公开(公告)日:1990-01-16

    申请号:US178721

    申请日:1988-04-07

    IPC分类号: F01D11/10 F01D11/24 F02C7/28

    CPC分类号: F01D11/24

    摘要: A system for controlling rotor blade tip clearances in a gas turbine engine supplies both heating air and cooling air to the rotor bore. The heating air flow is controlled by a valve and the cooling air flow is not controlled.

    摘要翻译: 用于控制燃气涡轮发动机中的转子叶片尖端间隙的系统将加热空气和冷却空气提供给转子孔。 加热气流由阀控制,冷却空气流不受控制。

    Flow measurement system
    2.
    发明授权
    Flow measurement system 失效
    流量测量系统

    公开(公告)号:US4715213A

    公开(公告)日:1987-12-29

    申请号:US839840

    申请日:1986-03-13

    IPC分类号: G01F1/704 F16J15/447 G01M3/20

    CPC分类号: G01M3/20 F16J15/4472

    摘要: A method and apparatus for measuring the leakage flow rate through a labyrinth seal is disclosed. This is achieved by first injecting a tracer gas through a spray tube at an upstream region of the seal. The tracer gas mixes with the gas stream to form a mixed flow stream. The concentration of the tracer gas in the mixed flow stream is then measured, allowing the leakage flow rate to be calculated.

    摘要翻译: 公开了一种用于测量通过迷宫式密封件的泄漏流量的方法和装置。 这是通过在密封件的上游区域首先通过喷射管注入示踪气体来实现的。 示踪气与气流混合形成混合流。 然后测量混合流动流中示踪气体的浓度,从而计算泄漏流量。

    Apparatus for thrust balancing and frame heating
    3.
    发明授权
    Apparatus for thrust balancing and frame heating 失效
    用于推力平衡和框架加热的装置

    公开(公告)号:US5154048A

    公开(公告)日:1992-10-13

    申请号:US590730

    申请日:1990-10-01

    IPC分类号: F01D3/04 F01D5/08 F01D9/06

    摘要: An industrial gas turbine engine includes in serial flow relationship a first compressor, a second compressor, a combustor, a first turbine, and a second turbine. The first compressor and the second turbine are fixedly joined together by a first shaft, and a turbine rear frame having a hub is disposed downstream of the second turbine for rotatably supporting the first shaft. A balance piston is fixedly joined to the first shaft, and means for channeling a fluid first to the balance piston for balancing thrust force on the first shaft and then to the turbine rear frame for heating the hub are provided. The apparatus is effective for carrying out a method including channeling a fluid first to the balance piston for thrust balancing the first shaft and then channeling the fluid to the turbine rear frame for heating the frame hub.

    摘要翻译: 工业燃气涡轮发动机以串联流动关系包括第一压缩机,第二压缩机,燃烧器,第一涡轮机和第二涡轮机。 第一压缩机和第二涡轮机通过第一轴固定在一起,并且具有轮毂的涡轮机后框架设置在第二涡轮机的下游,用于可旋转地支撑第一轴。 平衡活塞固定地连接到第一轴,并且提供了用于将流体首先引导到平衡活塞以用于平衡第一轴上的推力然后再到涡轮机后框架以加热轮毂的装置。 该装置对于执行包括将流体首先引导到平衡活塞以推力平衡第一轴然后将流体引导到涡轮机后框架以加热框架毂的方法是有效的。

    Clearance control system
    4.
    发明授权
    Clearance control system 失效
    清关控制系统

    公开(公告)号:US4893983A

    公开(公告)日:1990-01-16

    申请号:US178734

    申请日:1988-04-07

    IPC分类号: F01D11/10 F01D11/24 F02C7/28

    CPC分类号: F01D11/24

    摘要: A method and system for controlling rotor blade tip clearances in a gas turbine engine is disclosed. A flow of heat transfer fluid is supplied to the rotor. The temperature of the flow is controlled as a function of the heat carrying capacity of the fluid.

    摘要翻译: 公开了一种用于控制燃气涡轮发动机中的转子叶片尖端间隙的方法和系统。 传热流体流向转子供应。 流体的温度作为流体的承载能力的函数被控制。

    Compressor bore cooling manifold
    5.
    发明授权
    Compressor bore cooling manifold 失效
    压缩机孔冷却歧管

    公开(公告)号:US5271711A

    公开(公告)日:1993-12-21

    申请号:US880826

    申请日:1992-05-11

    IPC分类号: F01D5/08 F04D29/58 F03B11/02

    摘要: To control disc temperature, provide blade tip clearance control, and purge the rotor bore of a high pressure compressor in a gas turbine engine, an axially elongated manifold is disposed coaxially in the rotor bore to distribute cooling air bleed from the compressor inlet airstream to selected cavities between successive rotor discs in amounts tailored to the particular cooling needs of the neighboring discs.

    摘要翻译: 为了控制盘温度,提供叶片顶端间隙控制,并吹扫燃气轮机中的高压压缩机的转子孔,轴向细长的歧管同轴地布置在转子孔中,以将冷却空气从压缩机入口气流排出到选定的 连续的转子盘之间的空腔的量适合相邻盘的特定冷却需要。

    Method for thrust balancing and frame heating
    6.
    发明授权
    Method for thrust balancing and frame heating 失效
    推力平衡和框架加热方法

    公开(公告)号:US5167484A

    公开(公告)日:1992-12-01

    申请号:US856277

    申请日:1992-03-23

    IPC分类号: F01D3/04 F01D5/08 F01D9/06

    摘要: An industrial gas turbine engine includes in serial flow relationship a first compressor, a second compressor, a combustor, a first turbine, and a second turbine. The first compressor and the second turbine are fixedly joined together by a first shaft, and a turbine rear frame having a hub is disposed downstream of the second turbine for rotatably supporting the first shaft. A balance piston is fixedly joined to the first shaft, and means for channeling a fluid first to the balance piston for balancing thrust force on the first shaft and then to the turbine rear frame for heating the hub are provided. The apparatus is effective for carrying out a method including channeling a fluid first to the balance piston for thrust balancing the first shaft and then channeling the fluid to the tubine rear frame for heating the frame hub.

    摘要翻译: 工业燃气涡轮发动机以串联流动关系包括第一压缩机,第二压缩机,燃烧器,第一涡轮机和第二涡轮机。 第一压缩机和第二涡轮机通过第一轴固定在一起,并且具有轮毂的涡轮机后框架设置在第二涡轮机的下游,用于可旋转地支撑第一轴。 平衡活塞固定地连接到第一轴,并且提供了用于将流体首先引导到平衡活塞以用于平衡第一轴上的推力然后再到涡轮机后框架以加热轮毂的装置。 该装置对于执行包括将流体首先引导到平衡活塞以推力平衡第一轴然后将流体引导到摇杆后框架以加热框架毂的方法是有效的。

    High pressure compressor flowpath bleed valve extraction slot
    7.
    发明授权
    High pressure compressor flowpath bleed valve extraction slot 失效
    高压压缩机流路泄放阀提取槽

    公开(公告)号:US5209633A

    公开(公告)日:1993-05-11

    申请号:US839275

    申请日:1992-02-25

    IPC分类号: F04D27/02

    CPC分类号: F04D29/542 F04D27/023

    摘要: A high pressure compressor flowpath bleed extraction slot is provided wherein an articulated portion of the outer band of the compressor forms a slot for providing efficient conversion of core air to diffuser air while retaining substantial pressure and velocity energies. The diffuser slot can be applied to an earlier compressor stage with improved performance.

    摘要翻译: 提供了一种高压压缩机流路泄放提取槽,其中压缩机的外带的铰接部分形成用于提供核心空气到扩散空气的有效转换的槽,同时保持大量的压力和速度能量。 扩散器槽可以应用于具有改进性能的较早的压缩机级。