-
1.发明申请Continuous Fiber Reinforced Mesh Bond Coat for Environmental Barrier Coating System 有权用于环境屏障涂层系统的连续纤维增强网状粘结涂层公开(公告)号：US20130177440A1
公开(公告)日：2013-07-11
申请号：US13348212
申请日：2012-01-11
CPC分类号： F01D5/288 , C04B41/009 , C04B41/52 , C04B41/89 , F05D2230/90 , F05D2300/20 , F05D2300/6034 , F05D2300/614 , Y02T50/672 , C04B35/80 , C04B41/5096 , C04B14/46 , C04B41/4501 , C04B41/5024
摘要： A gas turbine blade may have a bond coat applied to its surface. A porous substrate may be applied to the bond layer and one or more protective layers may be applied to the bond layer such that the fiber mesh is embedded between the bond layer and the protective layer to prevent creep.
摘要翻译： 燃气轮机叶片可以具有施加到其表面的粘合涂层。 可以将多孔基材施加到接合层，并且可以将一个或多个保护层施加到接合层，使得纤维网嵌入在接合层和保护层之间以防止蠕变。
-
公开(公告)号：US09771811B2
公开(公告)日：2017-09-26
申请号：US13348212
申请日：2012-01-11
CPC分类号： F01D5/288 , C04B41/009 , C04B41/52 , C04B41/89 , F05D2230/90 , F05D2300/20 , F05D2300/6034 , F05D2300/614 , Y02T50/672 , C04B35/80 , C04B41/5096 , C04B14/46 , C04B41/4501 , C04B41/5024
摘要： A gas turbine blade may have a bond coat applied to its surface. A porous substrate may be applied to the bond layer and one or more protective layers may be applied to the bond layer such that the fiber mesh is embedded between the bond layer and the protective layer to prevent creep.
-
公开(公告)号：US20120237355A1
公开(公告)日：2012-09-20
申请号：US13049179
申请日：2011-03-16
CPC分类号： F01D5/284 , F01D5/147 , F05D2300/50212 , F05D2300/6033
摘要： A turbine blade assembly is disclosed. In one embodiment, the turbine blade assembly may generally include a turbine blade having a root portion and an airfoil. The airfoil may extend radially from the root portion to an airfoil tip. Additionally, the turbine blade assembly may include a composite rod extending within the turbine blade. The composite rod may include a first end coupled to the airfoil at the airfoil tip and a second end coupled to the root portion. Moreover, the coefficient of thermal expansion of the composite rod may be designed to be less than or equal to the coefficient of thermal expansion of the airfoil.
摘要翻译： 公开了一种涡轮叶片组件。 在一个实施例中，涡轮机叶片组件通常可以包括具有根部和翼型的涡轮叶片。 翼型件可以从根部径向延伸到翼型端头。 另外，涡轮机叶片组件可以包括在涡轮机叶片内延伸的复合杆。 复合杆可以包括在翼型端部处联接到翼型的第一端和联接到根部的第二端。 此外，复合棒的热膨胀系数可以设计成小于或等于翼型件的热膨胀系数。
-
公开(公告)号：US08475132B2
公开(公告)日：2013-07-02
申请号：US13049179
申请日：2011-03-16
IPC分类号： F01D5/14
CPC分类号： F01D5/284 , F01D5/147 , F05D2300/50212 , F05D2300/6033
摘要： A turbine blade assembly is disclosed. In one embodiment, the turbine blade assembly may generally include a turbine blade having a root portion and an airfoil. The airfoil may extend radially from the root portion to an airfoil tip. Additionally, the turbine blade assembly may include a composite rod extending within the turbine blade. The composite rod may include a first end coupled to the airfoil at the airfoil tip and a second end coupled to the root portion. Moreover, the coefficient of thermal expansion of the composite rod may be designed to be less than or equal to the coefficient of thermal expansion of the airfoil.
摘要翻译： 公开了一种涡轮叶片组件。 在一个实施例中，涡轮机叶片组件通常可以包括具有根部和翼型的涡轮叶片。 翼型件可以从根部径向延伸到翼型端头。 另外，涡轮机叶片组件可以包括在涡轮机叶片内延伸的复合杆。 复合杆可以包括在翼型端部处联接到翼型的第一端和联接到根部的第二端。 此外，复合棒的热膨胀系数可以设计成小于或等于翼型件的热膨胀系数。
-
公开(公告)号：US20120181370A1
公开(公告)日：2012-07-19
申请号：US13007697
申请日：2011-01-17
IPC分类号： B65H81/00
CPC分类号： B29C70/887 , B29C53/32 , B32B2305/08
摘要： A system for reinforcing a substrate includes a rotary device, a first guide connected to the rotary device, and a form positioned against the first guide. A reinforcement is supplied to wind around the form and against the first guide. A method for reinforcing a substrate includes connecting a first guide to a rotary device and positioning a form on a first side of the first guide. The method further includes winding a reinforcement around the form and against the first side of the first guide.
摘要翻译： 用于加强基板的系统包括旋转装置，连接到旋转装置的第一引导件和抵靠第一引导件定位的形式。 供应钢筋以围绕形式缠绕在第一导轨上。 一种用于加强基板的方法包括将第一引导件连接到旋转装置并将形式定位在第一引导件的第一侧上。 所述方法还包括围绕所述形式缠绕加强件并抵靠所述第一导向件的第一侧。
-
6.发明申请Compositional Bond Coat for Hindering/Reversing Creep Degradation in Environmental Barrier Coatings 审中-公开用于阻挡/扭转环境阻挡涂层蠕变降解的组合粘合剂涂层公开(公告)号：US20130177441A1
公开(公告)日：2013-07-11
申请号：US13348252
申请日：2012-01-11
申请人： Rupak Das , John McConnell Delvaux , James Zhang
发明人： Rupak Das , John McConnell Delvaux , James Zhang
CPC分类号： F01D5/288 , C23C4/067 , F05B2230/80 , F05B2230/90 , Y02T50/672 , Y02T50/6765
摘要： A gas turbine blade may have a bond coat applied to its surface. The bond coat may include silicon and a reactive material. The reactive material may react with thermally grown oxide generated at the bond layer to prevent and reverse creep. One or more protective layers may be applied to the bond layer.
摘要翻译： 燃气轮机叶片可以具有施加到其表面的粘合涂层。 粘合涂层可以包括硅和反应性材料。 反应性材料可以与在结合层产生的热生长氧化物反应，以防止和反向蠕变。 可以将一个或多个保护层施加到接合层。
-
公开(公告)号：US20130177439A1
公开(公告)日：2013-07-11
申请号：US13348182
申请日：2012-01-11
申请人： James Zhang , Rupak Das , John McConnell Delvaux
发明人： James Zhang , Rupak Das , John McConnell Delvaux
CPC分类号： F01D5/288 , F05D2300/20 , Y02T50/672 , Y10T156/10
摘要： A gas turbine blade having a surface may have a bond layer applied to a first section of the surface, wherein the bond layer is not applied to a second section of the surface. One or more protective layers may be applied such that the protective layers cover and overlap the bond layer making direct contact with an area of the surface immediately outside the first section of the surface and forming a mechanical constraint geometry about the edge of the bond layer.
摘要翻译： 具有表面的燃气轮机叶片可以具有施加到表面的第一部分的接合层，其中接合层不施加到表面的第二部分。 可以施加一个或多个保护层，使得保护层覆盖和重叠结合层，使得与表面的第一部分正前方的表面的区域直接接触，并且围绕接合层的边缘形成机械约束几何形状。
-
8.发明授权公开(公告)号：US09175402B2
公开(公告)日：2015-11-03
申请号：US13561445
申请日：2012-07-30
CPC分类号： C23C24/08 , C23C30/00 , Y10T29/49238 , Y10T428/20
摘要： A turbine repair process, a repaired coating, and a repaired turbine component are disclosed. The turbine repair process includes providing a turbine component having a higher-pressure region and a lower-pressure region, introducing particles into the higher-pressure region, and at least partially repairing an opening between the higher-pressure region and the lower-pressure region with at least one of the particles to form a repaired turbine component. The repaired coating includes a silicon material, a ceramic matrix composite material, and a repaired region having the silicon material deposited on and surrounded by the ceramic matrix composite material. The repaired turbine component a ceramic matrix composite layer and a repaired region having silicon material deposited on and surrounded by the ceramic matrix composite material.
摘要翻译： 公开了涡轮机修复过程，修理的涂层和修理的涡轮机部件。 涡轮机修复过程包括提供具有较高压力区域和较低压力区域的涡轮机部件，将颗粒引入高压区域，并且至少部分地修复高压区域和低压区域之间的开口 与至少一个颗粒形成修复的涡轮机部件。 被修复的涂层包括硅材料，陶瓷基复合材料，以及具有沉积在陶瓷基复合材料上并被陶瓷基复合材料包围的硅材料的修复区域。 所修复的涡轮机部件是陶瓷基体复合层和具有沉积在陶瓷基复合材料上并被陶瓷基质复合材料包围的硅材料的修补区域。
-
公开(公告)号：US09267378B2
公开(公告)日：2016-02-23
申请号：US13535319
申请日：2012-06-27
CPC分类号： F01D5/005 , F01D5/28 , F01D21/003 , F05D2260/80 , F05D2260/94 , F05D2260/941 , F05D2270/114 , G01B15/06 , Y02T50/672
摘要： In an embodiment, a system includes a turbomachine having a first turbomachine component including a first mechanoluminescent material. The first turbomachine component is configured to produce a first light emission upon exposure to a mechanical stimulus sufficient to cause mechanoluminescence by the first mechanoluminescent material. The system also includes a turbomachine monitoring system configured to monitor the structural health of the first component based on detection of the first light emission.
摘要翻译： 在一个实施例中，系统包括具有包括第一机械发光材料的第一涡轮机组件的涡轮机。 第一涡轮机组件被配置为在暴露于足以通过第一机械发光材料引起机械发光的机械刺激时产生第一光发射。 该系统还包括涡轮机监测系统，其配置为基于第一光发射的检测来监测第一部件的结构健康。
-
公开(公告)号：US20140112794A1
公开(公告)日：2014-04-24
申请号：US13494261
申请日：2012-06-12
IPC分类号： F01D5/30
CPC分类号： F01D5/3015 , F01D5/147 , F01D5/3007 , F01D5/303 , F01D5/3084 , F05D2300/6033
摘要： An assembly and method for affixing a turbomachine rotor blade to a rotor wheel are disclosed. In an embodiment, an adaptor member is provided disposed between the blade and the rotor wheel, the adaptor member including an adaptor attachment slot that is complementary to the blade attachment member, and an adaptor attachment member that is complementary to the rotor wheel attachment slot. A coverplate is provided, having a coverplate attachment member that is complementary to the rotor wheel attachment slot, and a hook for engaging the adaptor member. When assembled, the coverplate member matingly engages with the adaptor member, and retains the blade in the adaptor member, and the assembly in the rotor wheel.
摘要翻译： 公开了一种用于将涡轮机转子叶片固定到转子轮的组件和方法。 在一个实施例中，设置在叶片和转子轮之间的适配器构件，适配器构件包括与叶片附接构件互补的适配器附接槽和与转子轮附接槽互补的适配器附接构件。 提供了一种盖板，其具有与转子轮附接槽互补的盖板附接构件和用于接合适配器构件的钩。 当组装时，盖板构件与适配器构件配合地接合，并将叶片保持在适配器构件中，并且组件在转子轮中。
-
-
-
-
-
-
-
-
-
搜索结果
32 条记录 (耗时 0.024 秒)
