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公开(公告)号：US08721273B2
公开(公告)日：2014-05-13
申请号：US13351475
申请日：2012-01-17
CPC分类号： F01D5/143 , F01D5/145 , F05D2250/184 , Y02T50/673
摘要： An arrangement with a ring diffuser for an axial turbomachine, for example for a gas turbine, is provided. The ring diffuser includes an outer wall and with an inner wall coaxial thereto, between which a diffuser duct extends in ring form along an axial extent so as to diverge from an inflow-side end to an outflow-side end, the inner wall and the outer wall in each case including a wall surface delimiting the diffuser duct. In order to specify a diffuser duct which is adapted to an inflow uneven along the circumference and by means of which a specially efficient conversion of kinetic energy into static energy is possible, the wall surface which delimits the diffuser duct on the inlet side is rotationally asymmetrical.
摘要翻译： 提供了一种用于轴向涡轮机的环形扩散器的装置，例如用于燃气轮机。 环形扩散器包括外壁和与其同轴的内壁，扩散管之间沿轴向延伸成环形，从而从流入侧端部流出到流出侧端部，内壁和 在每种情况下的外壁包括限定扩散管的壁面。 为了指定适于沿着圆周不均匀的流入物的扩散器管道，并且通过该扩散管道将动能特别有效地转换成静态能量，限定入口侧的扩散管道的壁面是旋转不对称的 。
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2.发明申请Axial turbine for a gas turbine with limited play between blades and housing 审中-公开用于燃气轮机的轴向涡轮机，叶片和壳体之间的间隙有限公开(公告)号：US20110188999A1
公开(公告)日：2011-08-04
申请号：US13054162
申请日：2009-07-08
申请人： Stefan Braun , Christian Cornelius , Annika Emde , Andreas Heilos , Olaf Hein , Thomas Hofbauer , Christian Lerner , Silvio-Ulrich Martin , Thorsten Mattheis , Ralf Müsgen , Eckart Schumann , Rostislav Teteruk , Adam Zimmermann
发明人： Stefan Braun , Christian Cornelius , Annika Emde , Andreas Heilos , Olaf Hein , Thomas Hofbauer , Christian Lerner , Silvio-Ulrich Martin , Thorsten Mattheis , Ralf Müsgen , Eckart Schumann , Rostislav Teteruk , Adam Zimmermann
IPC分类号： F01D11/00
摘要： An axial turbine for a gas turbine including a rotor blade cascade is provided. The rotor blade cascade is formed from rotor blades each including, a front edge, a blade tip, and an annular space wall that surrounds the rotor blade cascade and includes an annular space inner side, enabling the annular space wall to be arranged directly adjacent to the blade tip forming a radial gap between the covering of the blade tip and the annual space inner side. When the turbine is in operation, the area of the blade tip with the highest pressure load is disposed in the region of the front edges, and the rotor blades in the region of their front edges include a radial projection and the annular space wall includes on the annular space inner side, a peripheral radial recess that interacts with the radial projections such that a minimum is established in the direction of the main through-flow of the turbine.
摘要翻译： 提供了一种用于包括转子叶片级联的燃气轮机的轴向涡轮机。 转子叶片级联由转子叶片形成，每个转子叶片包括前缘，叶片尖端和围绕转子叶片级联的环形空间壁，并且包括环形空间内侧，使得环形空间壁能够直接邻近 叶片尖端在叶片尖端的覆盖物和年度空间内侧之间形成径向间隙。 当涡轮机运行时，具有最高压力负载的叶片尖端的区域设置在前边缘的区域中，并且其前边缘区域中的转子叶片包括径向突起，并且环形空间壁包括在 环形空间内侧，与径向突起相互作用的周向径向凹部，使得在涡轮机的主通流方向上建立最小值。
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公开(公告)号：US06587320B1
公开(公告)日：2003-07-01
申请号：US09583141
申请日：2000-05-30
IPC分类号： H02H900
CPC分类号： H01L27/0288 , H01L23/60 , H01L27/0266 , H01L2924/0002 , H01L2924/3011 , H01L2924/00
摘要： A current ballasting circuit for an ESD protection device couples nonintersecting conductive strips between a common contact pad and the contact electrodes of the ESD protection device. The connecting strips form respective electrically isolated ballasting resistors between the external contact pad and the contact electrodes of the ESD device. In addition, lateral resistances are formed between the contact strips which enhance the operation of the multiple ballasting resistors. The conductive strips may be made from metal, polysilicon or by a vertically meandering series connection of polysilicon layers, metal layers and interconnecting vias. The lateral resistance between the parallel conductive paths may be enhanced by segmenting both the drain and source electrodes. In one example, the gate electrode of an MOS ESD device extends locally between each pair of strips to segment the drain and source regions. The lateral resistance between the conductive strips is further enhanced by defining an additional gate electrode, having a portion that is parallel to the gate electrode of the ESD device and further portions that extend between the conductive strips. Multiple ESD devices may be connected in parallel to provide additional paths for shunting ESD current.
摘要翻译： 用于ESD保护装置的电流镇流电路在公共接触焊盘和ESD保护装置的接触电极之间耦合不间断的导电条。 连接条在外部接触焊盘和ESD器件的接触电极之间形成相应的电隔离镇流电阻器。 此外，在增强多个镇流电阻器的操作的接触片之间形成横向电阻。 导电条可以由金属，多晶硅或通过多晶硅层，金属层和互连通孔的垂直曲折串联连接制成。 可以通过对漏极和源极两者进行分段来增强平行导电路径之间的横向电阻。 在一个示例中，MOS ESD器件的栅极电极在每对条之间局部延伸，以分隔漏极和源极区域。 导电条之间的横向电阻通过限定附加的栅电极进一步增强，栅电极具有平行于ESD器件的栅电极的部分以及在导电条之间延伸的另外部分。 多个ESD器件可以并联连接，以提供用于分流ESD电流的附加路径。
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公开(公告)号：US08911215B2
公开(公告)日：2014-12-16
申请号：US13393264
申请日：2010-08-10
CPC分类号： F04D29/324 , F01D5/141 , F05D2250/711 , F05D2250/712 , Y10S416/02 , Y10S416/05
摘要： A compressor blade for an axially permeated compressor, preferably of a stationary gas turbine is provided. The camber line of the blade tip side profile of the blade of the compressor blade includes at least two inflection points for reducing radial gap losses. By means of two inflection points, there is a concavely designed suction side contour segment in a segment from 35% to 50% for the suction side contour, and a convexly implemented pressure side contour segment for the pressure side contour. It is possible by means of the geometry to generate low-loss gap vortices, in order to increase the overall efficiency of an axial compressor including the compressor blades.
摘要翻译： 提供了用于轴向渗透的压缩机的压缩机叶片，优选地为固定式燃气轮机。 压缩机叶片的叶片的叶片侧面轮廓的弯度线包括用于减小径向间隙损失的至少两个拐点。 通过两个拐点，对于吸力侧轮廓，在凹部设计的吸力侧轮廓段中具有35％至50％的段，以及用于压力侧轮廓的凸形实施的压力侧轮廓段。 为了提高包括压缩机叶片在内的轴向压缩机的整体效率，可以通过几何形状产生低损耗间隙涡流。
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公开(公告)号：US08647054B2
公开(公告)日：2014-02-11
申请号：US13054190
申请日：2009-07-08
申请人： Marcel Aulich , Christian Cornelius , Georg Kröger
发明人： Marcel Aulich , Christian Cornelius , Georg Kröger
IPC分类号： F01D5/20
CPC分类号： F01D5/20 , F01D5/143 , F01D5/145 , F01D11/08 , F05D2250/71 , Y02T50/671 , Y02T50/673
摘要： An axial turbomachine including a rotor blade cascade is provided. The rotor blade cascade includes rotor blades each including front edge, a radially outer free blade tip and an annular enclosure enclosing the rotor blade cascade with an annulus inner side by means of which the annular enclosure is arranged directly adjacent to the blade tips to give a radial gap between the enveloping ends of the blade tips and the annulus inner side. The rotor blades include a radial projection in the region of the front edge on the blade tip and the annular enclosure has an annular radial recess in the annulus inner side, arranged at a radial distance from the ends of the blade tips, such that in the main flow direction of the axial turbomachine the line of the radial projections on the side facing the radial gap matches the line of the radial recess.
摘要翻译： 提供了包括转子叶片级联的轴向涡轮机。 转子叶片级联包括转子叶片，每个转子叶片包括前边缘，径向外部自由叶片尖端和围绕转子叶片的环形壳体，其具有环形内侧，环形外壳直接布置在叶片尖端附近，以产生 叶片尖端和环形内侧的包络端之间的径向间隙。 转子叶片包括位于叶片尖端上的前边缘区域中的径向突出部分，并且环形壳体在环形内侧具有环形径向凹部，该叶片内侧面布置成距离叶片尖端端部的径向距离，使得在 轴向涡轮机的主流动方向在面向径向间隙的一侧上的径向突起的线匹配径向凹槽的线。
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公开(公告)号：US20110250055A1
公开(公告)日：2011-10-13
申请号：US13132641
申请日：2009-11-19
IPC分类号： F04D29/40
CPC分类号： F01D5/143 , F01D5/145 , F05D2250/184 , Y02T50/673
摘要： A ring diffuser for an axial turbomachine is provided. The ring diffuser includes an outer wall and an inner wall coaxial thereto, between which a diffuser channel extends in a ring shape along an axial extension from an inflow-side end diverging to an outflow-side end, wherein the inner wall and the outer wall each include a wall surface bounding the diffuser channel. In order to specify a diffuser channel that is tailored to an inflow that is uneven along the circumference and that facilitates a particularly efficient conversion of kinetic energy into static energy, a rotationally asymmetric wall surface bounding the diffuser channel on the inlet side is provided.
摘要翻译： 提供了一种用于轴向涡轮机的环形扩散器。 环形扩散器包括外壁和与其同轴的内壁，扩散器通道之间沿着从扩散到流出侧端部的流入侧端部的轴向延伸部以环形形状延伸，其中内壁和外壁 每个包括围绕扩散器通道的壁表面。 为了指定适于沿着圆周不均匀的流入物的扩散器通道，并且有助于将动能特别有效地转换成静态能量，提供了限制入口侧的扩散器通道的旋转非对称壁面。
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7.发明申请Diffuser arranged between the compressor and the combustion chamber of a gas turbine 有权布置在燃气轮机的压缩机和燃烧室之间的扩散器公开(公告)号：US20100257869A1
公开(公告)日：2010-10-14
申请号：US10568736
申请日：2004-07-16
摘要： The invention relates to a gas turbine, comprising an annular combustion chamber and an upstream diffuser, with a throughflow essentially parallel to a turbine longitudinal axis, at a distance from said axis at least partly less than the annular combustion chamber, in which a compressed gas may be divided into several partial flows at a branching point, whereby at least one of the partial flows is a cooling gas flow. A main deflection region is provided in said diffuser, directed at an angle to the turbine longitudinal axis towards the annular combustion chamber.
摘要翻译： 本发明涉及一种燃气轮机，其包括环形燃烧室和上游扩散器，其具有基本上平行于涡轮纵向轴线的通流，所述通流至少部分地小于环形燃烧室，所述通气流至少部分地小于环形燃烧室，其中压缩气体 可以在分支点处分成几个部分流，由此部分流中的至少一个是冷却气体流。 主偏转区域设置在所述扩散器中，朝向环形燃烧室与涡轮纵向轴线成一定角度。
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公开(公告)号：US07634968B2
公开(公告)日：2009-12-22
申请号：US10491260
申请日：2002-10-01
申请人： Christian Cornelius
发明人： Christian Cornelius
IPC分类号： A47B3/00
CPC分类号： A47B3/0803 , A47B3/0818 , A47B7/02
摘要： A pivotable board with at least one leg is provided. The leg is connected to the board with a pivotable fitting. The pivotable fitting has a pivoting axis which is disposed in a slanted position with respect to the board and on which the leg or the board are pivotally mounted.
摘要翻译： 提供具有至少一条腿的可枢转板。 腿部与枢轴支架连接。 可枢转配件具有枢转轴线，该枢转轴线相对于板设置在倾斜位置，并且腿或板可枢转地安装在该枢转轴线上。
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9.发明申请Annular Flow Duct for a Turbomachine Through which a Main Flow can Flow in the Axial Direction 有权一个涡轮机的环形流道，主流通过该流道可以在轴向流动公开(公告)号：US20090290974A1
公开(公告)日：2009-11-26
申请号：US12227928
申请日：2007-05-29
CPC分类号： F01D5/145 , F01D5/143 , F04D29/526 , F04D29/685
摘要： Disclosed is an annular flow duct for a turbomachine, the flow duct arranged concentrically about a machine axis running in the axial direction and defined by a boundary wall of circular cross section for directing a main flow, wherein the boundary wall has a plurality of return flow passages distributed over its circumference and through which in each case a partial flow is detached from the main flow at a bleed position and returned to the main flow at a feed position situated upstream of the bleed position, and having aerofoils, arranged radically in the flow duct, of a blade ring, the aerofoil tips of which lie opposite the boundary wall, with a gap formed in each case, wherein the aerofoils are movable in a predetermined rotation direction along the circumference of the boundary wall. Furthermore, a compressor which is insensitive to pumping and flow separations, as viewed in rotation direction, the bleed position of each return flow passage lies upstream of the corresponding feed position.
摘要翻译： 公开了一种用于涡轮机的环形流动管道，该流动管道围绕沿着轴向运动的机器轴线同心地布置并且由用于引导主流量的圆形横截面的边界壁限定，其中边界壁具有多个回流 分布在其圆周上的通道，并且在每种情况下，部分流动在出口位置处与主流体分离，并且在位于排放位置上游的进给位置处返回到主流体，并且具有从根本上排列在流体中的机翼 一个叶片环的管道，其机翼尖头与边界壁相对，在每种情况下形成间隙，其中翼型件可沿着边界壁的圆周沿预定的旋转方向移动。 此外，从旋转方向观察对泵送和流动分离不敏感的压缩机，每个返回流动通道的排放位置位于相应进给位置的上游。
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公开(公告)号：US06618233B1
公开(公告)日：2003-09-09
申请号：US09627090
申请日：2000-07-27
IPC分类号： H02H322
CPC分类号： H01L27/0262 , H01L27/0248 , H03K17/0403 , H03K17/0814
摘要： An ESD protection circuit includes a SCR and a switching means, such as a MOS transistor connected to the SCR so that the SCR is turned on by the switching means to allow an ESD pulse to pass from a Pad line to a grounded VSS line and thereby dissipate the ESD pulse. The SCR is connected between the Pad line and the VSS line. One MOS switching means is connected between the Pad line and the SCR and has a gate which is connected to a VDD line which maintains the switch in open condition during normal VDD bias conditions. An ESD pulse applied to the Pad line, the switch is preconditioned in ON mode allowing the SCR to be predisposed to conduction to allow the ESD pulse to flow to the VSS line.
摘要翻译： ESD保护电路包括SCR和诸如连接到SCR的MOS晶体管的开关装置，使得SCR由开关装置导通，以允许ESD脉冲从Pad线路传递到接地VSS线路，从而 耗散ESD脉冲。 SCR连接在Pad线和VSS线之间。 一个MOS开关装置连接在Pad线和SCR之间，并且具有连接到VDD线的栅极，其在正常VDD偏置条件期间将开关保持在断开状态。 施加到Pad线的ESD脉冲，开关在ON模式下被预处理，允许SCR倾向于导通，以允许ESD脉冲流向VSS线。
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