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72 条记录 (耗时 0.018 秒)

    Gas turbine engine with concave pocket with knife edge seal
    26.
    发明申请
    Gas turbine engine with concave pocket with knife edge seal 有权
    带凹口的燃气轮机，带刀口密封

    公开(公告)号：US20080124215A1

    公开(公告)日：2008-05-29

    申请号：US11605678

    申请日：2006-11-29

    申请人： Roger E. Paolillo ,  Ioannis Alvanos ,  Cheng-Zhang Wang

    发明人： Roger E. Paolillo ,  Ioannis Alvanos ,  Cheng-Zhang Wang

    IPC分类号： F01D25/00

    CPC分类号： F01D11/001 ,  F01D11/02 ,  F05D2250/712

    摘要： A gas turbine engine is provided with turbine sealing structures including knife edge seals which extend at an angle relative to an axial center line of the engine. Each knife edge seal is associated with a concave pocket defined between a radially inner surface and a spaced radially outer surface. The concave pockets and their associated knife edge seals create a pair of vortices which prevent leakage into radially inner portions of the turbine section.

    摘要翻译： 燃气涡轮发动机设置有涡轮机密封结构，其包括相对于发动机的轴向中心线以一定角度延伸的刀刃密封件。 每个刀刃密封件与限定在径向内表面和间隔开的径向外表面之间的凹槽相关联。 凹口袋及其相关的刀刃密封件产生一对涡流，防止泄漏到涡轮部分的径向内部。

    Fluid brush seal with segment seal land
    27.
    发明申请
    Fluid brush seal with segment seal land 审中-公开
    流体刷密封带段密封垫

    公开(公告)号：US20080095616A1

    公开(公告)日：2008-04-24

    申请号：US11584062

    申请日：2006-10-20

    申请人： Ioannis Alvanos ,  John P. Virtue

    发明人： Ioannis Alvanos ,  John P. Virtue

    IPC分类号： F01D11/00

    CPC分类号： F01D11/001 ,  F01D5/3007 ,  F05D2240/56

    摘要： A turbine rotor for a turbine engine includes multiple rotor disks having rotor blades mounted about the circumference of each of the rotor disks. A fluid seal extends about the circumference of each rotor disk in close proximity to a stationary component of the rotor to separate the space between the rotor blades and a stationary component into separate cavities. The fluid seal includes a seal land on the rotor disk and a brush seal extending from the stationary component. A plurality of disk land segments and a plurality of blade land segments form the seal land. The disk seal segments are located on the rotor disk between the rotor blades. The blade land segments are located on the rotor blades. After the rotor blades are assembled, the blade land segments and the disk land segments fit together to form a segmented ring-like seal land around the circumference of the rotor disk.

    摘要翻译： 用于涡轮发动机的涡轮转子包括具有安装在每个转子盘周围的转子叶片的多个转子盘。 流体密封件围绕每个转子盘的圆周延伸，靠近转子的固定部件，以将转子叶片和固定部件之间的空间分离成单独的空腔。 流体密封件包括转子盘上的密封区域和从静止部件延伸的刷子密封件。 多个盘片区段和多个刀片区域段形成密封区域。 圆盘密封段位于转子叶片之间的转子盘上。 刀片区段位于转子叶片上。 在组装转子叶片之后，刀片接合段和盘片区段装配在一起以在转子盘周围形成分段的环状密封环。

    Gas turbine engine buffer cooling system
    29.
    发明授权
    Gas turbine engine buffer cooling system 有权
    燃气轮机发动机缓冲冷却系统

    公开(公告)号：US09347374B2

    公开(公告)日：2016-05-24

    申请号：US13405514

    申请日：2012-02-27

    申请人： Gabriel L. Suciu ,  Ioannis Alvanos

    发明人： Gabriel L. Suciu ,  Ioannis Alvanos

    IPC分类号： F02C6/08 ,  F01D5/08 ,  F01D9/06 ,  F02C7/18

    CPC分类号： F02C6/08 ,  F01D5/081 ,  F01D9/065 ,  F02C7/18 ,  F02C7/185 ,  F05B2260/205 ,  Y02T50/676

    摘要： A gas turbine engine includes a heat exchanger, a mid-turbine frame, a passageway that extends through at least a portion of the mid-turbine frame and a first nozzle assembly. The heat exchanger exchanges heat with a bleed airflow to provide a conditioned airflow. The mid-turbine frame is in fluid communication with the heat exchanger. The conditioned airflow is communicated through the passageway and is received by the first nozzle assembly to condition gas turbine engine hardware.

    摘要翻译： 燃气涡轮发动机包括热交换器，中涡轮机架，延伸穿过中涡轮机框架的至少一部分的通道和第一喷嘴组件。 热交换器与放气气流交换热量以提供调节气流。 中涡轮机架与热交换器流体连通。 调节气流通过通道连通并被第一喷嘴组件接收以调节燃气涡轮发动机硬件。

    Turbomachinery seal
    30.
    发明授权
    Turbomachinery seal 有权
    涡轮机械密封

    公开(公告)号：US09109458B2

    公开(公告)日：2015-08-18

    申请号：US13294787

    申请日：2011-11-11

    申请人： Ioannis Alvanos ,  Gabriel L. Suciu

    发明人： Ioannis Alvanos ,  Gabriel L. Suciu

    IPC分类号： F01D11/00 ,  F01D11/12

    CPC分类号： F01D11/001 ,  F01D11/122 ,  F01D11/127 ,  F05D2230/64 ,  F05D2250/184 ,  F05D2260/38

    摘要： A seal for sealing a rotor of a rotary machine to a stator thereof which circumscribes the rotor and is separated therefrom by a gap comprises a nonrotational sealing element received within an annular slot in the stator and radially translatable with respect thereto, and extending into the gap for sealing to rotational sealing element carried by the rotor. A resilient biasing element received between the nonrotational sealing element and a floor of the slot biases the nonrotational sealing element radially inwardly toward the rotational sealing element and limits radially outward movement of the nonrotational sealing element. A guide extending into said gap from the slot engages the nonrotational sealing element to prevent axial misalignment thereof with the machine's rotor.

    摘要翻译： 用于将旋转机械的转子密封到其定子上的用于将转子环绕并通过间隙分离的密封件包括：非旋转密封元件，其接收在定子的环形槽内并且可相对于其径向平移并延伸到间隙 用于密封转子承载的旋转密封元件。 容纳在非旋转密封元件和狭槽的底板之间的弹性偏置元件将非旋转密封元件径向向内朝向旋转密封元件偏压并且限制非旋转密封元件的径向向外移动。 从狭槽延伸到所述间隙中的引导件接合非旋转密封元件以防止其与机器转子的轴向不对准。