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1. 发明授权

US06305901B1 Steam turbine 有权
标题翻译：汽轮机
公开(公告)号：US06305901B1
公开(公告)日：2001-10-23
申请号：US09353611
申请日：1999-07-14
申请人： Ralf Bell , Ulrich Capelle , Armin Drosdziok , Jan-Erik Mühle , Mikhail Simkine , Ingo Stephan , Volker Simon
发明人： Ralf Bell , Ulrich Capelle , Armin Drosdziok , Jan-Erik Mühle , Mikhail Simkine , Ingo Stephan , Volker Simon
IPC分类号： F01D104
CPC分类号： F01D1/16
摘要： A steam turbine has a high-pressure turbine section and a medium-pressure turbine section fluidically connected to the high-pressure turbine section. The high-pressure turbine section is a chamber configuration and the medium-pressure turbine section is a drum configuration. Alternatively, the high-pressure turbine section is a drum configuration and the medium-pressure turbine section is a chamber configuration. Alternatively, or additionally, the high-pressure turbine section is a double-flow configuration and the medium-pressure turbine section is a double-flow configuration.
摘要翻译：蒸汽轮机具有与高压涡轮部分流体连接的高压涡轮部分和中压涡轮机部分。高压涡轮机部分是腔室构造，中压涡轮机部分是鼓构造。或者，高压涡轮机部分是鼓构造，中压涡轮机部分是腔室构造。或者或另外，高压涡轮机部分是双流配置，中压涡轮机部分是双流配置。

2. 发明授权

US06345952B1 Steam turbine 有权
标题翻译：汽轮机
公开(公告)号：US06345952B1
公开(公告)日：2002-02-12
申请号：US09352991
申请日：1999-07-14
申请人： Heinrich Oeynhausen , Wilfried Ulm , Ralf Bell , Ulrich Capelle , Jan-Erik Mühle , Mikhail Simkine , Ingo Stephan , Volker Simon
发明人： Heinrich Oeynhausen , Wilfried Ulm , Ralf Bell , Ulrich Capelle , Jan-Erik Mühle , Mikhail Simkine , Ingo Stephan , Volker Simon
IPC分类号： F01D104
CPC分类号： F01D5/142 , F01D1/16
摘要： A steam turbine has a turbine shaft directed along a turbine axis. A plurality of turbine stages, each include a guide-blade structure and a moving-blade configuration located axially downstream of the guide-blade structure. The guide-blade structure and the moving-blade configuration are provided along the turbine shaft. Each stage has an average reaction degree achievable between 5% and 70%. The reaction degree of at least two turbine stages is of different values.
摘要翻译：蒸汽轮机具有沿涡轮机轴线引导的涡轮机轴。多个涡轮级各自包括导向叶片结构和位于导向叶片结构的轴向下游的活动叶片构型。引导叶片结构和动叶片构造沿涡轮轴设置。每个阶段的平均反应程度可达5％至70％之间。至少两个涡轮级的反应程度是不同的值。

3. 发明授权

US06213711B1 Steam turbine and blade or vane for a steam turbine 有权
标题翻译：用于汽轮机的汽轮机和叶片或叶片
公开(公告)号：US06213711B1
公开(公告)日：2001-04-10
申请号：US09410828
申请日：1999-10-01
申请人： Karl-Heinrich Müller , Wilfried Ulm , Ralf Bell , Volker Simon
发明人： Karl-Heinrich Müller , Wilfried Ulm , Ralf Bell , Volker Simon
IPC分类号： F01D102
CPC分类号： F01D5/145 , F01D5/143 , F05D2240/31 , F05D2250/183 , F05D2250/294 , Y02T50/672 , Y02T50/673 , Y10S415/914
摘要： The invention relates to a steam turbine (1) which has a flow duct (2) with a wall (3). Blading (5) is arranged in blading rings (55) in the flow duct (2). The wall (3) of the flow duct (2) has a grooved structure (6) which purposefully influences the flow of an active fluid (13) through the flow duct (2). In particular, a spacing surface (31) with a grooved structure (6) is located between each two blades or vanes (5) of a blading ring (55). The invention also relates to a blade or vane for a steam turbine.
摘要翻译：本发明涉及一种具有带有壁（3）的流动管道（2）的蒸汽轮机（1）。叶片（5）布置在流动管道（2）中的叶片环（55）中。流动管道（2）的壁（3）具有有槽的结构（6），其有意地影响通过流动管道（2）的活性流体（13）的流动。特别地，具有开槽结构（6）的间隔表面（31）位于叶片环（55）的每个两个叶片（5）之间。本发明还涉及一种用于蒸汽轮机的叶片或叶片。

4. 发明授权

US07074009B2 Casing assembly for the turbine of an exhaust turbochanger 失效
标题翻译：一种排气涡轮增压器涡轮机的套管组件
公开(公告)号：US07074009B2
公开(公告)日：2006-07-11
申请号：US10296134
申请日：2001-06-06
申请人： Ruediger Allmang , Hartmut Claus , Volker Simon
发明人： Ruediger Allmang , Hartmut Claus , Volker Simon
IPC分类号： F01D25/08
CPC分类号： F01D25/145 , F01D9/026 , F05D2220/40
摘要： A spiral casing for a turbine of a turbocharger is made from thin (0,2 to 2 mm thick) sheet metal. The spiral casing can be made from two matching parts and can be insulated.
摘要翻译：用于涡轮增压器的涡轮机的螺旋壳体由薄（0.2至2mm厚）的金属片制成。螺旋套管可以由两个匹配的部件制成，可以绝缘。

5. 发明授权

US06827556B2 Moving blade for a turbomachine and turbomachine 失效
标题翻译：用于涡轮机和涡轮机的移动叶片
公开(公告)号：US06827556B2
公开(公告)日：2004-12-07
申请号：US10379987
申请日：2003-03-05
申请人： Volker Simon
发明人： Volker Simon
IPC分类号： F01D528
CPC分类号： F01D5/147 , B22F2998/00 , F01D5/28 , F05C2201/0463 , F05C2201/0466 , F05D2260/203 , F05D2300/612 , B22F7/006
摘要： A novel blade configuration does not exceed the permitted stresses for particular loads, especially as a result of centrifugal forces and which at the same time, allows the turbomachine to function with a high degree of efficiency. To this end, a moving blade for the turbomachine contains at least partially a cellular material, especially a foamed metal. The cellular material can be provided e.g. in the hollowed-out part of the moving blade.
摘要翻译：新颖的叶片结构不会超过特定载荷的允许应力，特别是由于离心力而同时允许涡轮机以高效率起作用。为此，用于涡轮机的移动叶片至少部分地包含多孔材料，特别是泡沫金属。细胞材料可以例如提供。在动叶片的中空部分。

6. 发明授权

US06945046B2 Turbine casing for an exhaust turbocharger made by casting 失效
标题翻译：用于铸造制造的排气涡轮增压器的涡轮机外壳
公开(公告)号：US06945046B2
公开(公告)日：2005-09-20
申请号：US10296135
申请日：2001-06-06
申请人： Ruediger Allmang , Hartmut Claus , Volker Simon
发明人： Ruediger Allmang , Hartmut Claus , Volker Simon
IPC分类号： F01D9/02 , F01D25/24 , F01D1/02 , F02B39/00 , F02D23/00
CPC分类号： F01D9/026 , F01D25/24 , F05D2220/40 , F05D2230/21 , F05D2230/232 , Y10S415/915
摘要： The invention concerns a casing aggregate for the turbine of an exhaust turbocharger.The invention is identified by the following characteristics: a spiral casing adapted for surround the running wheel of the turbine; a tongue-like wall part (tongue) in the inside of the spiral casing; an inlet connection; an outlet connection; a flange to connect to a bearing casing; wherein the casing aggregate is manufactured of thin-walled precision casting; wherein the casing aggregate is made of at least two parts, so that at least one separation joint is present; and the separation joint is arranged as follows: it runs in an axially perpendicular level; it runs along the apex line of the spiral casing; it extends over an arc of a circle of approximately 270 degrees; it lies outside of the area of the tongue.
摘要翻译：本发明涉及一种用于排气涡轮增压器的涡轮的壳体聚集体。本发明通过以下特征来确定：适于围绕涡轮机的行驶轮的螺旋壳体; 在螺旋壳体内部的舌状壁部分（舌头）; 入口连接出口连接; 连接到轴承箱的法兰; 其中所述壳体聚集体由薄壁精密铸造制成; 其中所述壳体聚集体由至少两个部分制成，使得存在至少一个分离接头; 分离接头的布置如下：其沿轴向垂直运动; 它沿着螺旋壳体的顶线延伸; 它延伸在大约270度的圆弧上; 它位于舌头之外。

7. 发明授权

US06607352B1 Turbo machine with an inner housing and an outer housing 失效
标题翻译：具有内壳和外壳的涡轮增压机
公开(公告)号：US06607352B1
公开(公告)日：2003-08-19
申请号：US09684248
申请日：2000-10-06
申请人： Laurence Crane , Edwin Gobrecht , Joe Hannon , Volker Simon
发明人： Laurence Crane , Edwin Gobrecht , Joe Hannon , Volker Simon
IPC分类号： F01D2526
CPC分类号： F01D25/26
摘要： A turbo machine, especially a steam turbine, has a main axis, an inner housing, an outer housing, a top region, and a bottom region. Between the outer housing and the inner housing a radial gap is formed, which has a narrow part in the bottom region.
摘要翻译：涡轮机，特别是汽轮机，具有主轴，内壳，外壳，顶部区域和底部区域。在外壳和内壳之间形成有在底部区域中具有窄部分的径向间隙。

8. 发明申请

US20100150701A1 VARIABLE GEOMETRY TURBOCHARGER 审中-公开
标题翻译：可变几何涡轮机
公开(公告)号：US20100150701A1
公开(公告)日：2010-06-17
申请号：US12663891
申请日：2008-06-26
申请人： Volker Simon , Mathias Weber , Paul Anschel
发明人： Volker Simon , Mathias Weber , Paul Anschel
IPC分类号： F04D29/56
CPC分类号： F01D5/146 , F01D11/16 , F01D17/165 , F04D29/462 , F05D2220/40 , F05D2240/12 , F05D2250/36 , F05D2250/411
摘要： A variable geometry turbocharger is provided. The turbocharger improves efficiency by controlling flow to the rotor (230) via movable vanes (260). The vanes (260) can be rotated using a pin (380, 480) and groove (385, 485) system. The vanes (260) can be multiple structures (710, 730) that are movable with respect to each other to increase the length of each of the vanes (260). The turbocharger also improves efficiency by creating a better seal in the area between the vanes (260) and the adjustment ring (240). The seal can be provided by biasing the adjustment ring (240) towards each of the vanes (260). The seal can be provided by expanding each of the vanes (260). The seal can be provided by having a movable portion (1150) of the adjustment ring (240) that is actuated by a pressure source or the like and axially moves towards the vanes (260). The plurality of vanes (260) can be low solidity vanes.
摘要翻译：提供了可变几何涡轮增压器。涡轮增压器通过经由可移动叶片（260）控制流到转子（230）来提高效率。叶片（260）可以使用销（380,480）和凹槽（385,485）系统旋转。叶片（260）可以是可相对于彼此移动以增加每个叶片（260）的长度的多个结构（710,730）。涡轮增压器还通过在叶片（260）和调节环（240）之间的区域中产生更好的密封来提高效率。可以通过朝向每个叶片（260）偏置调节环（240）来提供密封。可以通过使每个叶片（260）膨胀来提供密封。密封件可以通过具有由压力源等致动并且朝向叶片（260）轴向移动的调节环（240）的可移动部分（1150）来提供。多个叶片（260）可以是低固体叶片。

9. 发明授权

US06994518B2 Pre-whirl generator for radial compressor 有权
标题翻译：用于径向压缩机的涡旋发生器
公开(公告)号：US06994518B2
公开(公告)日：2006-02-07
申请号：US10712125
申请日：2003-11-13
申请人： Volker Simon , Mathias Weber , Christian Holzschuh
发明人： Volker Simon , Mathias Weber , Christian Holzschuh
IPC分类号： F01D17/01
CPC分类号： F02B37/225 , F01D17/141 , F01D17/162 , F04D27/0246 , F04D29/4213 , F05D2220/40 , F05D2250/51 , F05D2260/4031 , F05D2260/74 , F05D2260/76 , Y02T10/144
摘要： A pre-whirl generating apparatus (26) is provided that employs deformable air deflecting vanes (46) adjacent the inlet (18) of a radial air compressor (12-22), which vanes (46) can be mechanically deformed to generate positive, neutral, or negative pre-whirl flow to the compressor. A minimum number of parts are used to position one or more thin, deformable vanes (46) in the intake channel (34) leading to the compressor inlet (18). In their undeformed position, the vanes (46) do not deflect the incoming air, thereby causing little or no flow restriction. To achieve the desired positive or negative pre-whirl of flow to the compressor (12-22), the trailing edge (62) of the vanes (46) are deflected transverse to the direction of flow in the channel (34) in either the positive or negative direction.
摘要翻译：提供一种预涡旋发生装置（26），其采用与径向空气压缩机（12-22）的入口（18）相邻的可变形的空气偏转叶片（46），该叶片（46）可被机械地变形以产生正向，中性或负向预旋转流到压缩机。使用最少数量的部件将一个或多个薄的，可变形的叶片（46）定位在通向压缩机入口（18）的进气通道（34）中。在其未变形的位置，叶片（46）不会使进入的空气偏转，从而导致很少的或没有流动的限制。为了获得流向压缩机12-12的期望的正向或反向的预旋转，叶片46的后缘62横向于通道34中的流动方向偏转，正或负方向。

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