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35 条记录 (耗时 0.013 秒)

    Shaped part for forming a guide ring
    1.
    发明授权
    Shaped part for forming a guide ring 失效
    形成导向环的成形部分

    公开(公告)号：US06676370B2

    公开(公告)日：2004-01-13

    申请号：US10117612

    申请日：2002-04-04

    申请人： Peter Tiemann

    发明人： Peter Tiemann

    IPC分类号： F01D1108

    CPC分类号： F23M5/085 ,  F01D11/08 ,  F01D25/12 ,  F02C7/16 ,  F05D2260/205 ,  F05D2260/2322 ,  F23R2900/03044

    摘要： A shaped part (30) for forming a guide ring (21) for a gas turbine (1) is, on the one hand, to be produced with particularly little outlay and, on the other hand, is to be designed so that it can be cooled particularly effectively with steam as the coolant. For this purpose, according to the invention the shaped part (30) comprises a base plate (34) which, together with an associated metal guide plate (38, 44, 52), forms a flow passage (36) for a coolant which, in cross section, extends substantially over its entire width, with respect to the axial direction (x) of the guide ring (20, 21).

    摘要翻译： 一方面，用于形成用于燃气轮机（1）的导向环（21）的成形部件（30）一方面被制造成具有特别小的花费，另一方面，被设计成使得它可以 用蒸汽作为冷却剂特别有效地冷却。 为此，根据本发明，成形部件（30）包括与相关联的金属导板（38,44,52）一起形成用于冷却剂的流动通道（36）的基板（34） 在横截面中，相对于导向环（20,21）的轴向（x）基本上在其整个宽度上延伸。

    Turbomachine with double-faced rotor-shroud seal structure
    3.
    发明授权
    Turbomachine with double-faced rotor-shroud seal structure 有权
    涡轮机具有双面转子 - 护罩密封结构

    公开(公告)号：US06508624B2

    公开(公告)日：2003-01-21

    申请号：US09865983

    申请日：2001-05-02

    申请人： Sylvain Nadeau ,  William Holmes

    发明人： Sylvain Nadeau ,  William Holmes

    IPC分类号： F01D1108

    CPC分类号： F16J15/3288 ,  F01D5/225 ,  F01D11/08 ,  F04D29/164 ,  F04D29/326 ,  F05D2240/56

    摘要： A turbomachine for moving air includes a shroud 12 disposed about an axis A. The shroud 12 has a pair of opposing faces 14 and 16 defining a gap 18 therebetween. The opposing faces are disposed generally transversely with respect to the axis. A rotor assembly 13 is mounted for rotation about the axis. The rotor assembly has a plurality of blades 22 with tips of the blades being coupled to an annular band 30. At least a portion 32 of the annular band is disposed in the gap 18. Seal structure 36 extends from each opposing face of the shroud and into the gap to reduce swirl and minimize air leakage across the gap.

    摘要翻译： 用于移动空气的涡轮机包括围绕轴线A设置的护罩12.护罩12具有在其间限定间隙18的一对相对面14和16。 相对的面相对于轴线大致横向设置。 转子组件13安装成围绕轴线旋转。 转子组件具有多个叶片22，叶片的尖端联接到环形带30.环形带的至少一部分32设置在间隙18中。密封结构36从护罩的每个相对面延伸，并且 进入间隙以减少涡流，并最大限度地减少跨越间隙的空气泄漏。

    Shroud assembly having C-clip retainer
    4.
    发明授权
    Shroud assembly having C-clip retainer 有权
    护罩组件具有C形夹固定器

    公开(公告)号：US06435820B1

    公开(公告)日：2002-08-20

    申请号：US09383132

    申请日：1999-08-25

    申请人： John H. Overberg

    发明人： John H. Overberg

    IPC分类号： F01D1108

    CPC分类号： F01D25/246

    摘要： Disengagement of the C-clip in turbine shroud assemblies is prevented by providing a C-clip retainer. The shroud assembly includes a shroud support having a hook and at least one shroud having a mounting flange. A C-clip overlaps the hook and the mounting flange to clamp the shroud to the shroud support, and the retainer is secured to the shroud support and located so as to engage the C-clip. The retainer engages the C-clip in such a manner so as to limit aft axial movement of the C-clip, thereby eliminating C-clip back-off.

    摘要翻译： 通过提供C形夹保持器来防止涡轮机罩组件中的C形夹的脱离。 护罩组件包括具有钩的护罩支撑件和至少一个具有安装凸缘的护罩。 C形夹与钩和安装法兰重叠，以将护罩夹紧到护罩支撑件上，并且保持器固定到护罩支撑件并且定位成与C形夹接合。 保持器以这样的方式接合C形夹，以限制C形夹的后轴向运动，从而消除C形夹子的退回。

    Methods and apparatus for minimizing thermal gradients within turbine shrouds
    5.
    发明授权
    Methods and apparatus for minimizing thermal gradients within turbine shrouds 有权
    用于最小化涡轮机罩内热梯度的方法和装置

    公开(公告)号：US06341938B1

    公开(公告)日：2002-01-29

    申请号：US09522564

    申请日：2000-03-10

    申请人： Frederick J. Zegarski ,  John S. Carpenter

    发明人： Frederick J. Zegarski ,  John S. Carpenter

    IPC分类号： F01D1108

    CPC分类号： F01D11/127 ,  F01D25/14 ,  F01D25/26 ,  F05D2260/94 ,  F05D2260/941 ,  Y02T50/672 ,  Y02T50/675

    摘要： A low pressure turbine shroud includes a backplate and abradable material attached to said backplate. The backplate includes an upstream end, a downstream end, and a body extending between the upstream end and the downstream end. The body includes a first portion and a second portion. The body first portion has a first thickness greater than a body second portion second thickness. The abradable material attaches to an inner surface of the backplate and includes at least one segment having a thickness greater than remaining segments of abradable material.

    摘要翻译： 低压涡轮机罩包括附接到所述背板的背板和可磨损材料。 背板包括上游端，下游端和在上游端和下游端之间延伸的本体。 主体包括第一部分和第二部分。 主体第一部分具有大于主体第二部分第二厚度的第一厚度。 耐磨材料附着在背板的内表面上并且包括至少一个具有大于可磨损材料的剩余段的厚度的段。

    Turbomachinery seal
    7.
    发明授权
    Turbomachinery seal 失效
    涡轮机械密封

    公开(公告)号：US06808179B1

    公开(公告)日：2004-10-26

    申请号：US09127372

    申请日：1998-07-31

    申请人： Abhijit Bhattacharyya ,  William D. Marscher

    发明人： Abhijit Bhattacharyya ,  William D. Marscher

    IPC分类号： F01D1108

    CPC分类号： F01D11/00 ,  F05D2240/56 ,  F16J15/3288

    摘要： A turbomachinery seal (20) attached to annular member (30) which surrounds and rotatably engages a shaft (34). The seal is capable of sealing pressure differentials between a high pressure region (24) and a low pressure region (26) well in excess of 300 psi at relatively low leakage rates. One embodiment (120) of the seal includes a plurality of confronting plates (128) arranged so as to form an annular structure. Another embodiment (220) includes a plurality of bristle packs (252), each positioned between annular plates (256) having an axial taper (278) adjacent radially inner ends (274). In another embodiment (320) bristles 334′ and 334″ extend in axial positive and negative directions so as to create an interleaved bristle structure. In yet another embodiment (720), a plurality of elongate members (450) are embedded within bristles (434). A turbomachine (550) includes seals 520′ and 520″ of the invention.

    摘要翻译： 附接到环形构件（30）的涡轮机械密封件（20），其围绕并可旋转地接合轴（34）。 密封件能够以相对低的泄漏速率密封高压区域（24）和低压区域（26）之间的压力差超过300psi。 密封件的一个实施例（120）包括布置成形成环形结构的多个相对的板（128）。 另一实施例（220）包括多个刷毛包（252），每个刷毛包被定位在邻近径向内端（274）的具有轴向锥形（278）的环形板（256）之间。 在另一个实施例（320）中，刷毛334'和334“在轴向正向和负向方向上延伸，以便产生交织的刷毛结构。 在另一个实施例（720）中，多个细长构件（450）嵌入刷毛（434）内。 涡轮机（550）包括本发明的密封件520'和520“。

    Bucket tip brush seals in steam turbines and methods of installation
    10.
    发明授权
    Bucket tip brush seals in steam turbines and methods of installation 失效
    蒸汽涡轮机中的铲头刷密封件和安装方法

    公开(公告)号：US06431827B1

    公开(公告)日：2002-08-13

    申请号：US09741742

    申请日：2000-12-21

    申请人： Christopher Edward Wolfe ,  Norman Arnold Turnquist ,  Frederick George Baily ,  David Robert Skinner

    发明人： Christopher Edward Wolfe ,  Norman Arnold Turnquist ,  Frederick George Baily ,  David Robert Skinner

    IPC分类号： F01D1108

    CPC分类号： F16J15/3288 ,  F01D11/127 ,  F05D2240/56 ,  Y10T29/49297

    摘要： A diaphragm has an annular groove formed of deep and shallow grooves with the deep groove opening into the shallow groove. A combination spill strip/brush seal is disposed in the groove. The brush seal comprises a pair of flexible bars secured to the proximal ends of the brush bristles by welding and is received in the shallow groove and a recess in an axial face of the spill strip. The spill strip has base portions extending into the deep groove. The combination spill strip/brush seal is secured in the annular groove by peening material of the diaphragm into the spill strip/brush seal combination. The brush seal may be used with different diameters of spill strips and diaphragm grooves.

    摘要翻译： 隔膜具有由深而浅的槽形成的环形槽，深槽通向浅槽。 组合式溢流条/刷密封件设置在凹槽中。 刷子密封件包括通过焊接固定到刷毛的近端的一对柔性杆，并且容纳在浅槽中和在溢出条的轴向面中的凹部。 溢出带具有延伸到深槽中的基部。 通过将隔膜的材料喷丸到溢流带/刷子密封组合中，组合的溢出带/刷子密封件固定在环形槽中。 刷密封件可以与不同直径的溢流带和隔膜槽一起使用。