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公开(公告)号：US20100104426A1
公开(公告)日：2010-04-29
申请号：US11492590
申请日：2006-07-25
IPC分类号： F02C7/28
CPC分类号： F01D11/12 , F05D2230/60 , F05D2240/11
摘要： Aspects of the invention relate to a ring seal for a turbine engine. The ring seal can be made up of a plurality of circumferentially abutted ring seal segments. Each ring seal segment can comprise a plurality of individual channels. The channels can be generally U-shaped in cross-section with a forward span, and aft span and an extension connecting therebetween. The channels can be positioned such that the aft span of one channel can substantially abut the forward span of another channel. The plurality of separate channels can be detachably coupled to each other by, for example, a plurality of pins. The ring seal segment according to aspects of the invention can facilitate numerous advantageous characteristics including greater material selection, selective cooling, improved serviceability, and reduced blade tip leakage. Moreover, the configuration is well suited to handle the operational loads of the turbine.
摘要翻译： 本发明的方面涉及一种用于涡轮发动机的环形密封件。 环形密封件可以由多个周向邻接的环形密封段组成。 每个环形密封片段可以包括多个单独的通道。 通道可以具有大致U形的横截面，具有前跨距，后跨距和延伸部之间的连接。 通道可以被定位成使得一个通道的后跨距可以基本上抵靠另一通道的前跨。 多个单独的通道可以通过例如多个销可拆卸地彼此联接。 根据本发明的方面的环形密封段可以促进许多有利的特征，包括更大的材料选择，选择性冷却，改进的可使用性和减小的叶片尖端泄漏。 此外，该构造非常适合于处理涡轮机的操作负载。
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公开(公告)号：US07726936B2
公开(公告)日：2010-06-01
申请号：US11492590
申请日：2006-07-25
IPC分类号： F04D29/08
CPC分类号： F01D11/12 , F05D2230/60 , F05D2240/11
摘要： Aspects of the invention relate to a ring seal for a turbine engine. The ring seal can be made up of a plurality of circumferentially abutted ring seal segments. Each ring seal segment can comprise a plurality of individual channels. The channels can be generally U-shaped in cross-section with a forward span, and aft span and an extension connecting therebetween. The channels can be positioned such that the aft span of one channel can substantially abut the forward span of another channel. The plurality of separate channels can be detachably coupled to each other by, for example, a plurality of pins. The ring seal segment according to aspects of the invention can facilitate numerous advantageous characteristics including greater material selection, selective cooling, improved serviceability, and reduced blade tip leakage. Moreover, the configuration is well suited to handle the operational loads of the turbine.
摘要翻译： 本发明的方面涉及一种用于涡轮发动机的环形密封件。 环形密封件可以由多个周向邻接的环形密封段组成。 每个环形密封片段可以包括多个单独的通道。 通道可以具有大致U形的横截面，具有前跨距，后跨距和延伸部之间的连接。 通道可以被定位成使得一个通道的后跨距可以基本上抵靠另一通道的前跨。 多个单独的通道可以通过例如多个销可拆卸地彼此联接。 根据本发明的方面的环形密封段可以促进许多有利的特征，包括更大的材料选择，选择性冷却，改进的可使用性和减小的叶片尖端泄漏。 此外，该构造非常适合于处理涡轮机的操作负载。
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公开(公告)号：US20080025838A1
公开(公告)日：2008-01-31
申请号：US11492589
申请日：2006-07-25
申请人： Bonnie D. Marini , Douglas A. Keller , David C. Radonovich , Gary B. Merrill , Steven J. Vance , Anthony L. Schiavo
发明人： Bonnie D. Marini , Douglas A. Keller , David C. Radonovich , Gary B. Merrill , Steven J. Vance , Anthony L. Schiavo
IPC分类号： F01D5/20
CPC分类号： F01D25/246 , F05D2300/21 , F05D2300/6033
摘要： Aspects of the invention are directed to a ceramic matrix composite ring seal segment. The ring seal segment according to aspects of the invention includes a relatively simple body that is circumferentially curved. At least a portion of the hot gas path surface of the ring seal segment can be coated with a thermal insulating. material. In one embodiment, each ring seal segment can be operatively connected to a stationary support structure, such as by way of isolation rings. The ring seal segments and/or the isolation rings can be configured so as to restrain the ring seal segments in the axial, radial and/or circumferential directions. The ring seal segments can be attached to the isolation rings so that the support points act opposite the operating pressure loads. Thus, the ring seal segments carry these loads in compression, a strong direction of the CMC fibers.
摘要翻译： 本发明的方面涉及一种陶瓷基复合环密封段。 根据本发明的方面的环形密封段包括周向弯曲的相对简单的主体。 环形密封段的热气体路径表面的至少一部分可以被涂覆绝热。 材料。 在一个实施例中，每个环形密封段可以可操作地连接到固定的支撑结构，例如通过隔离环。 环形密封段和/或隔离环可以构造成在轴向，径向和/或圆周方向上限制环形密封段。 环形密封段可以连接到隔离环，使得支撑点与操作压力负载相反。 因此，环形密封段承受这些负载在CMC纤维的强力方向的压缩。
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公开(公告)号：US20080206542A1
公开(公告)日：2008-08-28
申请号：US11709698
申请日：2007-02-22
申请人： Steven J. Vance , Gary B. Merrill
发明人： Steven J. Vance , Gary B. Merrill
IPC分类号： B32B3/26
CPC分类号： F01D11/122 , F05D2230/10 , F05D2230/13 , F05D2230/31 , F05D2300/21 , F05D2300/603 , Y10T428/249953
摘要： A ceramic matrix composite with an enhanced abradability has a patterned surface with an array of solid composite material and voids where the voids extend into but not through the composite. The flow of gas through the voids as the surface is traversed by an impinging component, such as a turbine blade tip, is inhibited by the shape and size of the voids which can be sealed by the passing blade tip. Separately or additionally the inhibition of gas flow can result from the filling of the voids with a ceramic material of higher abradability than the ceramic matrix composite.
摘要翻译： 具有增强的耐磨性的陶瓷基复合材料具有带有固体复合材料和空隙阵列的图案化表面，其中空隙延伸到复合材料中而不通过复合材料。 当表面被诸如涡轮机叶片尖端的冲击部件穿过时，通过空隙的气体的流动被可被通过的叶片尖端密封的空隙的形状和尺寸所抑制。 单独地或另外地，气体流动的抑制可以由具有比陶瓷基质复合材料更高磨损性的陶瓷材料填充空隙产生。
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5.发明授权Battery fault tolerant architecture for cell failure modes series bypass circuit 有权电池故障模式串联旁路电路容错架构公开(公告)号：US09024586B2
公开(公告)日：2015-05-05
申请号：US12904906
申请日：2010-10-14
CPC分类号： H02J7/0026 , B60L3/0046 , B60L3/0092 , B60L3/04 , B60L11/1866 , B60L2210/30 , B60L2210/40 , B60L2240/545 , B60L2250/10 , H01M10/0525 , H01M10/441 , H01M2220/20 , Y02E60/122 , Y02T10/7005 , Y02T10/7011 , Y02T10/7055 , Y02T10/7061 , Y02T10/7241
摘要： A battery cell by-pass circuit that has particular application for by-passing cells in a high voltage battery for a vehicle. The battery includes a plurality of battery cells electrically coupled in series. The by-pass circuit includes a first switch electrically coupled in series with one or more of the battery cells, a by-pass line electrically coupled around the one or more battery cells and a second switch electrically coupled in the by-pass line and in parallel with the one or more battery cells. During normal cell operation, the first switch is closed and the second switch is open so that current flows through the one or more battery cells. If the one or more battery cells fail or are failing, the first switch is opened and the second switch is closed so that current by-passes the one or more cells and they are removed from the battery circuit.
摘要翻译： 一种电池单元旁路电路，其具有用于在车辆的高压电池中旁路电池的特定应用。 电池包括串联电耦合的多个电池单元。 旁路电路包括与一个或多个电池单元串联电耦合的第一开关，围绕一个或多个电池单元电耦合的旁路线和在旁路线中电耦合的第二开关， 与一个或多个电池单元平行。 在正常单元操作期间，第一开关闭合，并且第二开关断开，使得电流流过一个或多个电池单元。 如果一个或多个电池单元出现故障或发生故障，则第一开关断开并且第二开关闭合，使得电流旁路一个或多个电池并且从电池电路中移除。
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公开(公告)号：US07819625B2
公开(公告)日：2010-10-26
申请号：US11800787
申请日：2007-05-07
申请人： Gary B. Merrill , Steven J. Vance
发明人： Gary B. Merrill , Steven J. Vance
IPC分类号： F01D11/08
CPC分类号： F01D9/06 , F01D11/122
摘要： A pattern of depressions (36) in a sealing surface (34) on a CMC wall (32) of gas turbine ring segment (30) allows minimum clearance against turbine blades tips, and thus maximizes working gas sealing. An array of depressions (36) on the surface (34) increases abradability of the surface (34) by blade tip contact during zero clearance conditions and reduces blade tip damage. The depressions (36) are unconnected, preventing bypass of the working gas around the blade tips. A desired abradable surface geometry may be formed in a stacked laminate wall construction (40-43, 52) by staggered laminate edge profiles (50, 52) or by machining of depressions (36, 54) after construction.
摘要翻译： 在燃气轮机环段（30）的CMC壁（32）上的密封表面（34）中的凹陷（36）的图案允许对涡轮叶片尖端的最小间隙，从而使工作气体密封最大化。 在零间隙条件下，表面（34）上的凹陷（36）的阵列通过叶片尖端接触增加了表面（34）的耐磨性，并且减少了叶片尖端损伤。 凹陷（36）是未连接的，防止围绕叶片尖端的工作气体旁路。 期望的可磨损表面几何形状可以通过交错的层压边缘轮廓（50,52）或通过在构造之后机械加工凹陷（36,54）而形成在堆叠的层叠壁结构（40-43,52）中。
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公开(公告)号：US20080025846A1
公开(公告)日：2008-01-31
申请号：US11494176
申请日：2006-07-27
申请人： Steven J. Vance , Jay A. Morrison
发明人： Steven J. Vance , Jay A. Morrison
IPC分类号： B64C11/24
CPC分类号： F01D5/282 , F01D5/147 , F01D5/187 , F01D5/284 , F05D2300/21 , F05D2300/603
摘要： A CMC airfoil (20) formed with CMC stitches (37) interconnected between opposed walls (26, 28) of the airfoil to restrain outward flexing of the walls resulting from pressurized cooling air within the airfoil. The airfoil may be formed of a ceramic fabric infused with a ceramic matrix and dried, and may be partially to fully cured. Then holes (32, 34) are formed in the opposed walls of the airfoil, and a ceramic stitching element such as ceramic fibers (36) or a ceramic tube (44) is threaded through the holes. The stitching element is infused with a wet ceramic matrix before or after threading, and is flared (38) or otherwise anchored to the walls (26, 28) to form a stitch (37) there between. The airfoil and stitch are then cured. If the airfoil is cured before stitching, a pre-tension is formed in the stitch due to relative curing shrinkage.
摘要翻译： 形成有CMC螺纹（37）的CMC翼型件（20），其连接在翼型件的相对壁（26,28）之间，以限制由翼型内的加压冷却空气引起的壁的向外弯曲。 翼型件可以由注入陶瓷基体的陶瓷织物形成并干燥，并且可以部分地完全固化。 然后，在翼面的相对的壁上形成孔（32,34），并且陶瓷纤维（36）或陶瓷管（44）之类的陶瓷缝合元件穿过孔。 缝合元件在穿线之前或之后用湿陶瓷基体注入，并且被张开（38）或以其它方式锚固到壁（26,28），以在其间形成线圈（37）。 然后将翼型和线迹固化。 如果机翼在缝合之前固化，则由于相对固化收缩，在针迹中形成预张力。
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公开(公告)号：US6106959A
公开(公告)日：2000-08-22
申请号：US273383
申请日：1999-03-22
IPC分类号： F02C7/00 , C23C4/06 , C23C4/10 , C23C28/00 , C23C30/00 , B32B15/01 , B21D53/78 , B32B15/04 , B32B15/20
CPC分类号： C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/36 , Y10T428/12549 , Y10T428/12618 , Y10T428/12743 , Y10T428/12854 , Y10T428/12931 , Y10T428/12944
摘要： The present invention generally describes multilayer thermal barrier coating systems and methods of making the multilayer thermal barrier coating systems. The thermal barrier coating systems comprise a first ceramic layer, a second ceramic layer, a thermally grown oxide layer, a metallic bond coating layer and a substrate. The thermal barrier coating systems have improved high temperature thermal and chemical stability for use in gas turbine applications.
摘要翻译： 本发明总体上描述了多层热障涂层系统和制备多层热障涂层系统的方法。 热障涂层系统包括第一陶瓷层，第二陶瓷层，热生长氧化物层，金属粘合涂层和基底。 热障涂层系统具有改进的用于燃气轮机应用的高温热和化学稳定性。
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9.发明授权Battery fault tolerant architecture for cell failure modes parallel bypass circuit 有权电池故障模式并联旁路电路的电池容错架构公开(公告)号：US08471529B2
公开(公告)日：2013-06-25
申请号：US12904913
申请日：2010-10-14
CPC分类号： H02J7/0026 , B60L11/1855 , B60L11/1879 , H02J7/0024 , Y02T10/7011 , Y02T10/705 , Y02T10/7055
摘要： A by-pass circuit for a battery system that disconnects parallel connected cells or modules from a battery circuit or controls the current through the parallel connected cells or modules. If a cell has failed or is potentially failing in the system, then the by-pass circuit can disconnect the cell or module from other cells or modules electrically coupled in parallel. If a cell or module has a lower capability than another cell or module, then the by-pass circuit can control the current to the cell or module to maximize the performance of the system and prevent the system from creating a walk-home condition.
摘要翻译： 用于电池系统的旁路电路，其将并联连接的电池或模块与电池电路断开或通过并联连接的电池或模块控制电流。 如果单元故障或系统中潜在的故障，则旁路电路可以将单元或模块与其他电池或并联电耦合的模块断开连接。 如果单元或模块具有比另一个单元或模块更低的能力，则旁路电路可以控制到单元或模块的电流，以使系统的性能最大化，并防止系统创建走家条件。
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公开(公告)号：US08033790B2
公开(公告)日：2011-10-11
申请号：US12239016
申请日：2008-09-26
申请人： Steven J. Vance
发明人： Steven J. Vance
IPC分类号： F01D5/30
CPC分类号： F01D5/147 , F01D5/18 , F01D5/28 , F05D2230/50 , F05D2230/51
摘要： A multiple piece turbine airfoil having an outer shell with an airfoil tip that is attached to a root with an internal structural spar is disclosed. The root may be formed from first and second sections that include an internal cavity configured to receive and secure the one or more components forming the generally elongated airfoil. The internal structural spar may be attached to an airfoil tip and place the generally elongated airfoil in compression. The configuration enables each component to be formed from different materials to reduce the cost of the materials and to optimize the choice of material for each component.
摘要翻译： 公开了一种具有外壳的多件涡轮机翼型件，其外壳具有翼形件末端，该外壳具有内部结构梁的根部。 根部可以由第一部分和第二部分形成，其包括构造成接收和固定形成大致细长的翼型的一个或多个部件的内部空腔。 内部结构翼梁可以附接到翼型端头并将大致细长的翼型件压缩。 该配置使得每个组件能够由不同的材料形成以降低材料的成本并优化每个部件的材料选择。
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