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公开(公告)号：US20100111684A1
公开(公告)日：2010-05-06
申请号：US12262333
申请日：2008-10-31
Applicant: Wei Ning , Michael E. Friedman , John F. Ryman
Inventor： Wei Ning , Michael E. Friedman , John F. Ryman
CPC classification number: F01D9/04 , F01D1/04 , F01D5/142 , F05D2240/12 , F05D2250/30 , Y02T50/673
Abstract: An assembly of airfoils in a turbine engine, the assembly comprising: at least three successive axially stacked rows of airfoils in one of a compressor and a turbine: a first airfoil row, a second airfoil row, and a third airfoil row; wherein the first airfoil row and the third airfoil row each comprise one of a row of rotor blades and a row of stator blades, and the second airfoil row comprises the other; and wherein at least a majority of the mid-channel points of the airfoils in the third airfoil row are positioned circumferentially within +/−25% pitch of the third airfoil row with respect to the location at which a wake flow during a selected operating condition from the first airfoil row is determined to enter the third airfoil row.
Abstract translation: 在涡轮发动机中的翼型件的组件，所述组件包括：在压缩机和涡轮机之一中的至少三个连续轴向堆叠的翼型排;第一翼型排，第二翼型排和第三翼型排; 其中所述第一翼型排和所述第三翼型排各自包括一排转子叶片和一排定子叶片中的一个，并且所述第二翼型排包括另一个; 并且其中所述第三翼型排中的翼型件的中间通道点的至少大部分相对于在所选择的操作条件期间的尾流的位置周向地定位在第三翼型排的+/- 25％间距内 从第一翼型排确定进入第三翼型排。
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公开(公告)号：US07670109B2
公开(公告)日：2010-03-02
申请号：US11743211
申请日：2007-05-02
Applicant: Ralf Greim , Said Havakechian
Inventor： Ralf Greim , Said Havakechian
CPC classification number: F01D1/06 , F01D1/04 , F01D5/28 , F05D2220/31 , Y10T29/4932
Abstract: A turbine (100) of a turbine installation, especially a steam turbine of a steam turbine installation, includes at least one radial or diagonal turbine stage (120) with radial or diagonal inflow and axial outflow, and also at least one axial turbine stage (121-125) with axial inflow and axial outflow. The at least one radial or diagonal turbine stage (120) forms the first stage of the turbine (100) and the at least one axial turbine stage (121-125) is arranged downstream of the radial or diagonal turbine stage (121) as an additional stage of the turbine. The at least one radial or diagonal turbine stage (120) has a higher temperature resistance than the at least one axial turbine stage (121-125). The turbine (100) makes it possible to significantly increase the process temperature of the steam turbine installation, wherein measures for increasing the temperature resistance need only to be adopted for components of the radial or diagonal turbine stage (120).
Abstract translation: 涡轮机设备的涡轮（100），特别是蒸汽涡轮机设备的蒸汽涡轮机，包括具有径向或对角线流入和轴向流出的至少一个径向或对角涡轮机台（120），并且还包括至少一个轴向涡轮机台（ 121-125）具有轴向流入和轴向流出。 至少一个径向或对角涡轮机台（120）形成涡轮机（100）的第一级，并且至少一个轴向涡轮机台（121-125）布置在径向或对角涡轮机台（121）的下游，作为 涡轮机的附加阶段。 至少一个径向或对角涡轮机台（120）具有比至少一个轴向涡轮机台（121-125）更高的耐温性。 涡轮（100）使得可以显着增加蒸汽轮机设备的过程温度，其中仅用于径向或对角涡轮机台（120）的部件的增加耐温性的措施。
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公开(公告)号：US20050175450A1
公开(公告)日：2005-08-11
申请号：US11052865
申请日：2005-02-09
Applicant: Takeshi Okubo , Toshiyuki Osada , Takeshi Sano , Yusuke Miyamoto , Kazuyoshi Miyagawa
Inventor： Takeshi Okubo , Toshiyuki Osada , Takeshi Sano , Yusuke Miyamoto , Kazuyoshi Miyagawa
CPC classification number: F01D1/04 , F04D3/00 , F04D29/181
Abstract: An axial-flow pump employs an increased boss ratio Dh/Dt, wherein Dh is the hub diameter of a rotary shaft of a rotor, and Dt is the tip diameter of impeller vanes of the rotor. Specifically, the boss ratio is 0.65 to 0.85, preferably 0.7 to 0.8.
Abstract translation: 轴流泵采用增加的凸台比Dh / Dt，其中Dh是转子的旋转轴的毂直径，Dt是转子的叶轮叶片的尖端直径。 具体而言，凸台比为0.65〜0.85，优选为0.7〜0.8。
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公开(公告)号：US06368057B1
公开(公告)日：2002-04-09
申请号：US09494347
申请日：2000-01-31
Applicant: Toru Takahashi , Kenichi Imai , Ryou Oda , Yoichi Tsuda
Inventor： Toru Takahashi , Kenichi Imai , Ryou Oda , Yoichi Tsuda
IPC: F01D102
CPC classification number: F01D1/04 , F05D2260/231
Abstract: A steam turbine includes a turbine high pressure section, a turbine intermediate pressure section and a turbine low pressure section, in which at least two or more of these pressure sections are combined together, and a turbine rotor which is subjected to a gradient thermal treatment at different thermal treating temperatures at respective pressure sections is rotatably supported by bearings and accommodated in a turbine casing, and in a case where an axial distance from a setting position of a turbine movable blade of a final stage of the turbine low pressure section to a setting position of a partition plate disposed at a time when the gradient thermal treatment is performed to each of the pressure sections at different thermal treating temperature is defined as A, a blade length of the turbine movable blade is defined as B, and an axial distance from a prior stage of the final stage of the turbine low pressure section to the setting position of the partition plate is defined as C, the setting position of the partition plate is set in a range of (A/B)≧0.9 and C≧300 mm.
Abstract translation: 蒸汽涡轮机包括涡轮机高压部分，涡轮中间压力部分和涡轮机低压部分，其中这些压力部分中的至少两个或更多个组合在一起，以及涡轮转子，其经受梯度热处理 各个压力部分的不同的热处理温度由轴承可旋转地支撑并容纳在涡轮机壳体中，并且在从涡轮机低压部分的最后级的涡轮可动叶片的设定位置到轴向距离的设置 将在不同的热处理温度下对每个压力部进行梯度热处理时设置的隔板的位置定义为A，将涡轮机动叶片的叶片长度定义为B，将轴距离 涡轮机低压部分的最后阶段到分隔板的设定位置的前一阶段被定义为C，t 分隔板的设定位置设定在（A / B）> 0.9，C> = 300mm的范围内。
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公开(公告)号：US6046509A
公开(公告)日：2000-04-04
申请号：US141130
申请日：1998-08-27
Applicant: William P. LaBaire
Inventor： William P. LaBaire
CPC classification number: F01D1/026 , F01D1/04 , F01D15/10 , F05D2240/241
Abstract: A steam turbine-driven generator for generating electric power is comprised of an electric generator having a vertical shaft journalled for rotation between bearings contained in a generator housing. An axial flow impulse turbine wheel with peripheral vanes is secured to an unsupported upper end of the shaft protruding from the top of the generator housing. The turbine wheel is enclosed within a turbine housing secured to the top of the generator housing. The turbine housing includes an inlet and an outlet for accommodating a through flow of steam, with internally arranged nozzles for directing the steam flow against the vanes of the turbine wheel.
Abstract translation: 一种用于产生电力的汽轮机驱动发电机包括一个发电机，该发电机具有一个垂直轴，该垂直轴在轴承座内容纳在发电机壳体中。 具有外围叶片的轴向流动脉冲涡轮机叶片固定到从发电机壳体的顶部突出的轴的未支撑的上端。 涡轮机叶轮封闭在固定到发电机壳体顶部的涡轮机壳体内。 涡轮壳体包括用于容纳蒸汽通道的入口和出口，其具有用于将蒸汽流引导到涡轮机叶轮的内部布置的喷嘴。
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Patent Agency Ranking46.发明授权Turbomachine, such as a steam turbine with high steam inlet temperature, especially 失效涡轮机，如具有高蒸汽入口温度的汽轮机，特别是
公开(公告)号：US4027996A
公开(公告)日：1977-06-07
申请号：US597300
申请日：1975-07-18
Applicant: Herbert Keller , Bruno Krieg , Ludwig Romer
Inventor： Herbert Keller , Bruno Krieg , Ludwig Romer
Abstract: A turbomachine having a stationary housing and a rotatable rotor mounted therein and including a series of rotor blade rings carried by the rotor and a series of guide vane rings carried by the housing, the guide vane rings and the rotor blade rings being disposed in mutually alternating relationship, further includes means defining an annular space located forward of the first rotor blade ring of the series of rotor blade rings, flow medium supply means communicating with the annular space for supplying flow medium thereto, the annular space extending radially outwardly and along the entire periphery of the turbomachine for producing a torsional flow of the flow medium, the rotor having a shaft formed with a collar, and the series of rotor blade rings including a first blade ring mounted on the collar directly behind the annular space and having a diameter greater than that of the succeeding blade rings of the series, whereby the flow medium supplied to the annular space axially impinges directly on the first blade ring without being initially guided by any guide vane rings.
Abstract translation: 一种具有固定壳体和可旋转转子的涡轮机，其安装在其中并且包括由转子承载的一系列转子叶片环和由壳体承载的一系列导叶环，引导叶片环和转子叶片环相互交替设置 关系，还包括限定位于一系列转子叶片环的第一转子叶片环之前的环形空间的装置，与环形空间连通的用于向其供应流动介质的流动介质供应装置，环形空间径向向外延伸并沿着整个 所述涡轮机的周边用于产生所述流动介质的扭转流，所述转子具有形成有轴环的轴，并且所述一系列转子叶片环包括安装在所述轴环上的第一叶片环，所述第一叶片环直接位于所述环形空间的后面，并且具有更大的直径 比随后的该系列的叶片环的流动介质的流动介质提供给环形空间 直接在第一叶片环上，而不是最初由任何导向叶片环引导。
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公开(公告)号：US3932064A
公开(公告)日：1976-01-13
申请号：US513159
申请日：1974-10-08
Applicant: Colin Andrew Millar Tayler
Inventor： Colin Andrew Millar Tayler
Abstract: A multiple re-entry compressor of the kind set forth in USA Patent application Ser. No. 335,162 now U.S. Pat. No. 3,869,220 is described having inter cooling between successive passes of the rotor blading. A further improvement is described in which variable aperture arcuate segmented flowpaths are provided.
Abstract translation: 美国专利申请系列中提出的多重再入式压缩机。 现在美国专利第335,162号 描述了在转子叶片的连续通过之间具有相互冷却的3,869,220号。
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公开(公告)号：US3869220A
公开(公告)日：1975-03-04
申请号：US33516273
申请日：1973-02-23
Applicant: SECR DEFENCE BRIT
Inventor： TAYLER COLIN ANDREW MILLER
Abstract: A rotary machine comprising at least one row of rotor blades circumferentially distributed on a rotor and disposed in a rotor blade passage between at least one row of upstream stator blades and at least one row of downstream rotor blades is provided with partitions in the upstream and downstream stator blades to provide a plurality of arcuate segmented flowpaths through the rotor blading. A confined flowpath between a machine inlet and a machine outlet intersects the rotor blading at each arcuate segmented flowpath in turn from the upstream side to the downstream side. This invention when applied to a compressor provides a machine in which several stages of compression of a fluid may be achieved using a single row of rotor blades.
Abstract translation: 一种旋转机械，包括沿圆周方向分布在转子上并且设置在至少一排上游定子叶片与至少一排下游转子叶片之间的转子叶片通道中的至少一排转子叶片，其在上游和下游设置有隔板 定子叶片以提供穿过转子叶片的多个弧形分段的流动路径。 机器入口和机器出口之间的限制流动路径从每个弧形分段流动路径依次从上游侧到下游侧相交。 当应用于压缩机时，本发明提供了一种机器，其中可以使用单排转子叶片来实现流体的几个压缩阶段。
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公开(公告)号：US2351328A
公开(公告)日：1944-06-13
申请号：US43286742
申请日：1942-02-28
Applicant: BELL TELEPHONE LABOR INC
Inventor： GENT EDGAR W
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50.发明授权High-pressure steam turbine and method of utilizing high-pressure steam therein 失效高压蒸汽轮机及其中使用高压蒸汽的方法
公开(公告)号：US1632907A
公开(公告)日：1927-06-21
申请号：US3146325
申请日：1925-05-19
Applicant: FRANZ LOSEL
Inventor： FRANZ LOSEL
IPC: F01D1/04
CPC classification number: F01D1/04
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