公开(公告)号：US20040240995A1

公开(公告)日：2004-12-02

申请号：US10779024

申请日：2004-02-13

发明人： Werner Bosen

IPC分类号： F03B011/00

CPC分类号： F04D29/059 ,  F04D29/5853 ,  H02K5/08 ,  H02K5/1735 ,  H02K7/14 ,  H02K7/1823 ,  H02K9/00 ,  H02K11/0094

摘要： A turbomachine has a turborotor made up of a shaft and a rotor disk, and an electric machine having an electric rotor. The rotor disk is arranged at one end of the shaft, in overhung manner, and the electric rotor is connected with the shaft of the turborotor. The electric rotor is arranged on the other end of the shaft, also in overhung manner, and the shaft is mounted on shaft bearings in a bearing housing that thermally separates the shaft bearings from the electric machine.

摘要翻译： 涡轮机具有由轴和转子盘构成的涡轮电动机和具有电动转子的电动机。 转子盘以悬臂方式布置在轴的一端，电动转子与涡轮转子的轴连接。 电动转子也布置在轴的另一端，也是悬臂式的，轴安装在轴承中，将轴承与电机热分离。

公开(公告)号：US20030185679A1

公开(公告)日：2003-10-02

申请号：US10403954

申请日：2003-03-31

申请人： Metaullics Systems Co., L.P.

发明人： George S. Mordue ,  Mark A. Bright

IPC分类号： F03B011/00

CPC分类号： F04D7/045 ,  F04D7/065

摘要： A molten material pump includes an impeller housed within a base member of the pump. A plurality of grooves are defined in a peripheral sidewall of the impeller for either drawing a molten material into the base member's chamber or pushing molten material out of the base member's chamber. The impeller is rotated by a rotatable shaft connected to an upper surface of the impeller. The rotatable shaft includes a non-circular shaped lower end dimensioned to be received within a cooperating opening in the impeller. The molten material pump further includes a connecting assembly for interconnecting components of the molten material pump. The connecting assembly includes a first mounting member attached to a first pump component that is dimensioned to be fitted within a cooperating recess of a second mounting member attached to a second pump component. In another embodiment of the invention, a stub shaft connects an upper shaft portion of the shaft to the impeller. The stub shaft includes a universal joint that is not rigidly connected to the upper shaft portion. In addition, the universal shaft is configured to allow the stub shaft and impeller to pivot. A floating deflector block weighs on an upper sealing block of the pump for enhancing the seal at the pump's bearing surfaces.

摘要翻译： 熔融材料泵包括容纳在泵的基座构件内的叶轮。 多个凹槽限定在叶轮的周边侧壁中，用于将熔融材料拉入基部构件的腔室或将熔融材料推出基座构件的腔室。 叶轮由与叶轮上表面连接的旋转轴旋转。 可旋转轴包括非圆形的下端，其尺寸适于容纳在叶轮中的协作开口内。 熔融材料泵还包括用于使熔融材料泵的部件相互连接的连接组件。 连接组件包括附接到第一泵部件的第一安装部件，该第一安装部件的尺寸适于安装在附接到第二泵部件的第二安装部件的配合凹部内。 在本发明的另一个实施例中，短轴将轴的上轴部分连接到叶轮。 短轴包括不与上轴部分刚性连接的万向接头。 此外，万向轴构造成允许短轴和叶轮枢转。 浮动偏转器块重量在泵的上密封块上，以增强泵的轴承表面处的密封。

公开(公告)号：US20020197154A1

公开(公告)日：2002-12-26

申请号：US10233536

申请日：2002-09-04

发明人： Hideto Nogiwa

IPC分类号： F03B011/00

CPC分类号： F04D27/0292 ,  F04D29/122 ,  F05D2270/101

摘要： Abnormality in an amount of a working gas leaked from between a rotating ring adapted to rotate with a rotor and a stationary ring of a turbo fluid machine is detected by a pressure switch and a flow meter, which are provided in a primary seal vent line, the working gas leaking from sealing surfaces of the labyrinth seal and the secondary dry gas seal, together with a purge gas purged to the space from outside is discharged outside the machine from a flow passage via a space. When abnormality generates in the secondary dry gas seal, a control valve provided in the purge gas line operates to secure a flow rate in the purge gas line, so that a flow rate detected by the flow meter provided in the purge gas line increases, and thus abnormality in the secondary dry gas seal is detected.

摘要翻译： 由适于与转子旋转的旋转环和涡轮流体机械的静止环之间的工作气体的泄漏量的异常通过设置在主密封排气管线中的压力开关和流量计来检测， 从迷宫式密封件和二次干燥气体密封件的密封表面泄漏的工作气体以及从外部吹扫到空间的吹扫气体经由空间从流动通道排出机器外部。 当在二次干燥气体密封件中产生异常时，设置在净化气体管线中的控制阀用于确保吹扫气体管线中的流量，使得由吹扫气体管线中设置的流量计检测到的流量增加， 因此检测到二次干燥气体密封件的异常。

公开(公告)号：US20020005274A1

公开(公告)日：2002-01-17

申请号：US09726424

申请日：2000-12-01

发明人： Alexander Beeck ,  Bernhard Bonhoff ,  Sacha Parneix ,  Bernhard Weigand

IPC分类号： F28F013/12 ,  F01D005/14 ,  F03B011/00 ,  F03D011/00 ,  F04D029/38

CPC分类号： F01D5/187 ,  F05D2260/22141 ,  F23R2900/03045 ,  F28F1/40 ,  F28F3/02 ,  F28F13/12 ,  Y10T137/2093

摘要： An arrangement for cooling a flow-passage wall surrounding a flow passage is described, having at least one rib element which induces flow vortices in a flow medium passing through the flow passage, is attached to that side of the flow-passage wall which faces the flow passage, and the shape and size of which are selected in accordance with a certain heat transfer coefficient and a certain pressure loss caused in the flow medium due to the latter flowing over the rib element. The invention is characterized in that the rib element, while largely retaining its original shape and/or size, has contours enlarging its surface facing the flow passage.

摘要翻译： 描述了用于冷却围绕流动通道的流动通道壁的布置，其具有至少一个在通过流动通道的流动介质中引起流动涡流的肋元件，其连接到流动通道壁的面向 流动通道，其形状和尺寸根据一定的传热系数和由于流体介质流过肋元件而在流动介质中引起的一定的压力损失来选择。 本发明的特征在于，肋元件在很大程度上保持其原始形状和/或尺寸的同时具有使其面向流动通道的表面扩大的轮廓。

公开(公告)号：US20010005555A1

公开(公告)日：2001-06-28

申请号：US09726521

申请日：2000-12-01

发明人： Erhard Kreis ,  Christof Pfeiffer ,  Ulrich Rathmann

IPC分类号： F01D005/08 ,  F03B011/00 ,  F04D029/58

CPC分类号： F01D11/08 ,  F01D11/12 ,  F01D25/14 ,  Y10T428/12361

摘要： In a heat shield (10), in particular for the stator of gas turbines, which heat shield (10) is composed of a plurality of individual segments (10a, b; 20a, b), whose end surfaces (15a, b) respectively abut one another so as to form a gap (12), and which have cooling holes (13a, b) for cooling purposes in the region of the end surfaces (15a, b), through which cooling holes (13a, b) a cooling fluid is blown out into the gap (12), cooling is ensured, even when the gap is closed, by a chamber (11), which is widened relative to the gap (12) and into which the cooling holes (13a, b) open, being arranged in the region of the gap (12).

摘要翻译： 在隔热罩（10）中，特别是对于燃气轮机的定子，该隔热罩（10）分别由多个单独的段（10a，b; 20a，b）组成，其各自的端面（15a，b）分别 彼此邻接以形成间隙（12），并且在端面（15a，b）的区域中具有用于冷却目的的冷却孔（13a，b），冷却孔（13a，b）通过冷却孔 流体被吹出到间隙（12）中，即使间隙闭合，也可以通过相对于间隙（12）加宽的腔室（11）来确保冷却，冷却孔（13a，b） 打开，布置在间隙（12）的区域中。

公开(公告)号：US20040265121A1

公开(公告)日：2004-12-30

申请号：US10877716

申请日：2004-06-25

发明人： Hsieh Kun Lee ,  DongYun Lee ,  Zhijie Zhang

IPC分类号： F03B011/00 ,  H05K007/20

CPC分类号： F04D29/601 ,  H01L23/467 ,  H01L2924/0002 ,  H01L2924/00

摘要： A combination of fan and heat sink includes a fan (10), a heat sink (20) and four fixtures (30). The fan defines four holes (12) in four comers thereof respectively. The heat sink has a plurality of parallel fins (24). Each fixture includes a post (32) inserted into the corresponding hole of the fan, a pressing portion (36) pressing the fan toward the heat sink and a locking leg (34) interlocking with outmost fins.

摘要翻译： 风扇和散热器的组合包括风扇（10），散热器（20）和四个固定装置（30）。 风扇分别在其四个角中限定四个孔（12）。 散热器具有多个平行翅片（24）。 每个固定器包括插入风扇的相应孔中的柱子（32），将风扇压向散热器的按压部分（36）和与最外侧翅片互锁的锁定腿部（34）。

公开(公告)号：US20040096319A1

公开(公告)日：2004-05-20

申请号：US10472900

申请日：2003-09-25

发明人： Tatsuro Uchida ,  Masataka Kikuchi

IPC分类号： F03B011/00

CPC分类号： F16J15/4472 ,  F05C2251/08

摘要： The so-called comb-type labyrinth sealing device (S1) is disposed in a gap between a rotor blade (2), i.e. a rotating member, and a labyrinth packing (9), i.e. a stationary member. The sealing device (S1) has a plurality of sealing fins (F1, F2) arranged on the opposite sides of the gap opposite to each other. The sealing fins are axially spaced apart at unequal pitches, and hence a possibility that some of the clearances between the opposite sealing fins (F1, F2) decrease when a casing holding the labyrinth packing (9) and a rotor (1) are axially displaced relative to each other due to the difference in thermal expansion between the rotator and the casing increases.

摘要翻译： 所谓的梳状迷宫式密封装置（S1）设置在转子叶片（2）即旋转构件与迷宫式密封件（9）即静止构件之间的间隙中。 密封装置（S1）具有布置在彼此相对的间隙的相对侧上的多个密封翅片（F1，F2）。 密封翅片以不等间距轴向间隔开，因此当保持迷宫式密封件（9）和转子（1）的壳体轴向移位时，相对的密封翅片（F1，F2）之间的一些间隙的可能性降低 由于转子与壳体之间的热膨胀差异而相对于彼此增加。

公开(公告)号：US20040050090A1

公开(公告)日：2004-03-18

申请号：US10311620

申请日：2003-09-11

发明人： Avraham Ophir ,  Henrich Rojanski ,  Arie Kanievski

IPC分类号： F25B013/00 ,  F01D005/08 ,  F01D005/18 ,  F01D011/00 ,  F03D011/00 ,  F03B011/00 ,  F01D025/08 ,  F01D025/16 ,  F01D025/18 ,  F04D029/04 ,  F04D029/08 ,  F04D029/58

CPC分类号： F04D29/441 ,  F04D17/12

摘要： A gasdynamic arrangement for a multi-stage centrifugal turbomachine, such as a two-stage compressor, comprising two coaxial impellers assembled on a common shaft with axial intake ports and radial peripheral discharge zones, the intake ports of the two impellers preferably pointing away from each other; a cylindrical vessel concentrically housing the impellers and the intake duct; a partition wall between the two impellers having a first and a second group of apertures; a first array of curved ducts conveying the flow from the first impeller discharge zone to the first group of apertures in the partition wall, the flow further passing through a chamber in the vessel to the intake port of the second impeller, and a second array of curved ducts conveying the flow from the second impeller discharge zone to the second group of apertures in the partition wall, the flow further going to the discharge port, the two flows bypassing each other in opposing directions at the partition wall.

摘要翻译： 用于多级离心涡轮机的气体动力装置，例如两级压缩机，包括组装在具有轴向进气口和径向周向排放区域的公共轴上的两个同轴叶轮，两个叶轮的进气口优选地指向每个 其他; 同心地容纳叶轮和进气管的圆柱形容器; 两个叶轮之间的分隔壁具有第一和第二组孔; 第一阵列的弯曲管道，其将来自第一叶轮排出区的流动传递到分隔壁中的第一组孔，该流动进一步通过容器中的室至第二叶轮的进气口，第二阵列 将来自第二叶轮排放区的流量传送到分隔壁中的第二组孔的弯曲管道，该流动进一步进入排出口，两个流在分隔壁处相反地相互绕过彼此。

公开(公告)号：US20030231955A1

公开(公告)日：2003-12-18

申请号：US10173009

申请日：2002-06-17

发明人： Vincent Anthony Barry ,  Thomas Edward Demarche

IPC分类号： F01D005/14 ,  F03B011/00

CPC分类号： F01D5/186 ,  F01D5/288 ,  F05D2230/90 ,  F05D2260/202 ,  F23R2900/03041 ,  F23R2900/03042 ,  F23R2900/03044 ,  Y02T50/67 ,  Y02T50/676

摘要： A flowpath wall is provided for bounding hot combustion gases in a gas turbine engine. The wall includes opposite outer and inner surfaces and a plurality of cooling holes extending therebetween. A thermal barrier coating is bonded to the outer surface and covers blind the holes thereat.

摘要翻译： 提供了用于在燃气涡轮发动机中限制热燃烧气体的流路壁。 该壁包括相对的外表面和内表面以及在它们之间延伸的多个冷却孔。 隔热涂层结合到外表面并覆盖盲孔。

公开(公告)号：US20030082050A1

公开(公告)日：2003-05-01

申请号：US10268422

申请日：2002-10-10

发明人： Emil Aschenbruck ,  Hildegard Ebbing ,  Andreas Kleinefeldt ,  Klaus Dieter Mohr

IPC分类号： F03B011/00

CPC分类号： F01D11/001 ,  F01D11/025

摘要： A device for sealing between the guide vanes (1) and the rotor (17) of turbomachines, especially gas turbines has inner rings (3) suspended on the vane footing (14) of the guide vanes (1) in a thermally elastic manner with soldered honeycomb seal (4) and labyrinth tips (5) arranged on the rotor (17). First flow channels, which are connected to the cavities (21) of the cooled guide vanes (1), through which said cavities cooling air flows, are led through the vane footings (14). The first flow channels are connected to at least one of second flow channels led through the inner ring (3) to the vicinity of the honeycomb seal (4). The second flow channels open into at least one of third flow channels that are open at the rear edge of the inner ring (3) or are led to an annular groove (10) open toward the honeycomb seal (4) on the underside of the inner ring (3).

摘要翻译： 一种用于在导叶（1）和涡轮机（特别是燃气轮机）的转子（17）之间进行密封的装置，其具有以热弹性方式悬挂在导叶（1）的叶片基脚（14）上的内环（3） 焊接的蜂窝状密封件（4）和布置在转子（17）上的迷宫尖端（5）。 连接到冷却的导向叶片（1）的空腔（21）的第一流动通道（冷却空气流过的空腔）被引导通过叶片基座（14）。 第一流动通道连接到通过内环（3）引导到蜂窝密封件（4）附近的至少一个第二流动通道。 第二流动通道打开到在内圈（3）的后边缘处开口的第三流动通道中的至少一个，或者被引导到朝向蜂窝状密封件（4）的下侧的开口的环形槽（10） 内圈（3）。