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公开(公告)号：US20140054863A1
公开(公告)日：2014-02-27
申请号：US13590846
申请日：2012-08-21
IPC分类号： F16J15/447
CPC分类号： F16J15/4472
摘要： A seal assembly for a turbine system includes a sealing strip having a forward surface and an aft surface, wherein the sealing strip is operably coupled to a first component and extends radially outwardly toward a second component for inhibiting a flow of fluid passing through a fluid path defined by the first component and the second component. Also included is at least one groove disposed within at least one of the forward surface and the aft surface of the sealing strip.
摘要翻译： 用于涡轮机系统的密封组件包括具有前表面和后表面的密封条，其中所述密封条可操作地联接到第一部件并且径向向外朝向第二部件延伸，以阻止流过流体路径 由第一部件和第二部件限定。 还包括设置在密封条的前表面和后表面中的至少一个中的至少一个凹槽。
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公开(公告)号：US20120219410A1
公开(公告)日：2012-08-30
申请号：US13035140
申请日：2011-02-25
IPC分类号： F01D9/02
CPC分类号： F01D5/141 , F01D5/3007 , F04D29/324 , F04D29/544 , F05D2250/74
摘要： An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE 1. X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances are joined smoothly with one another to form a complete airfoil shape.
摘要翻译： 具有基本上符合表1所示的X，Y和Z的笛卡尔坐标值的公称轮廓的制品.X和Y是以平滑的连续弧连接时以每英寸限定翼型轮廓部分的距离，以英寸为单位 Z英寸。 Z距离处的轮廓部分彼此平滑地连接以形成完整的翼型形状。
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公开(公告)号：US20110212943A1
公开(公告)日：2011-09-01
申请号：US13123983
申请日：2009-10-14
申请人： Gopalan Balasubramanian , Ponpandian Thanasekaran , Sridharan Rajagopal , Bharathimohan Kuppusamy , Virendra Kachhadia , Vignesh Radhakrishnan , Sivasudar Velaiah , Shridhar Narayanan , Mandar Bhonde , Praveen Rajendran , Sriram Rajagopal
发明人： Gopalan Balasubramanian , Ponpandian Thanasekaran , Sridharan Rajagopal , Bharathimohan Kuppusamy , Virendra Kachhadia , Vignesh Radhakrishnan , Sivasudar Velaiah , Shridhar Narayanan , Mandar Bhonde , Praveen Rajendran , Sriram Rajagopal
IPC分类号： A61K31/165 , C07C237/20 , C07D223/14 , C07C237/22 , C07D207/337 , C07D307/54 , C07C231/02 , C07C229/46 , A61K31/55 , A61K31/40 , A61K31/341 , C12N9/99 , A61P29/00 , A61P19/02 , A61P31/00 , A61P1/00 , A61P25/28 , A61P35/00 , A61P35/04
CPC分类号： C07C259/06 , C07C237/20 , C07C237/42 , C07C271/22 , C07C2603/74 , C07D207/337 , C07D471/18
摘要： Provided herein are novel bridged cyclic derivatives of the general formula (I), their analogs, tautomeric forms, stereoisomers, polymorphs, solvates, intermediates, pharmaceutically acceptable salts, pharmaceutical compositions, metabolites and prodrugs thereof. These compounds can inhibit HDACs and are useful as therapeutic or ameliorating agent for diseases that are involved in cellular growth such as malignant tumors, autoimmune diseases, skin diseases, infections, inflammation, neurode-generative disorders etc.
摘要翻译： 本文提供了通式（I）的新型桥连环衍生物，其类似物，互变异构形式，立体异构体，多晶型物，溶剂化物，中间体，药学上可接受的盐，药物组合物，代谢物和前药。 这些化合物可以抑制HDAC，并且可用作涉及细胞生长的疾病如恶性肿瘤，自身免疫疾病，皮肤疾病，感染，炎症，神经发生障碍等的治疗或改善剂。
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公开(公告)号：US20130170969A1
公开(公告)日：2013-07-04
申请号：US13343021
申请日：2012-01-04
IPC分类号： F01D9/04
CPC分类号： F01D5/146 , F01D5/14 , F01D5/145 , F05D2240/126
摘要： The present application provides a diffuser for use with a gas turbine. The diffuser may include hub, a number of struts extending from the hub, and a number of airfoils extending from the hub.
摘要翻译： 本申请提供了一种用于燃气轮机的扩散器。 扩散器可以包括轮毂，从轮毂延伸的多个支柱以及从轮毂延伸的多个翼型件。
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公开(公告)号：US08591193B2
公开(公告)日：2013-11-26
申请号：US13035140
申请日：2011-02-25
CPC分类号： F01D5/141 , F01D5/3007 , F04D29/324 , F04D29/544 , F05D2250/74
摘要： An article of manufacture having a nominal profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in TABLE 1. X and Y are distances in inches which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z in inches. The profile sections at the Z distances are joined smoothly with one another to form a complete airfoil shape.
摘要翻译： 具有基本上符合表1所示的X，Y和Z的笛卡尔坐标值的公称轮廓的制品.X和Y是以平滑的连续弧连接时以每英寸限定翼型轮廓部分的距离，以英寸为单位 Z英寸。 Z距离处的轮廓部分彼此平滑地连接以形成完整的翼型形状。
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