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1. 发明授权

US09175402B2 Turbine repair process, repaired coating, and repaired turbine component 有权
标题翻译：涡轮修复过程，修理涂层和修理的涡轮机部件
公开(公告)号：US09175402B2
公开(公告)日：2015-11-03
申请号：US13561445
申请日：2012-07-30
申请人： Rupak Das , John McConnell Delvaux , Andres Jose Garcia-Crespo
发明人： Rupak Das , John McConnell Delvaux , Andres Jose Garcia-Crespo
IPC分类号： B23P6/00 , C23C24/08 , C23C30/00
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。

2. 发明申请

US20140112794A1 BLADE ATTACHMENT ASSEMBLY 有权
标题翻译：刀片附件装配
公开(公告)号：US20140112794A1
公开(公告)日：2014-04-24
申请号：US13494261
申请日：2012-06-12
申请人： Andres Jose Garcia-Crespo , John McConnell Delvaux , Diane Patricia Miller
发明人： Andres Jose Garcia-Crespo , John McConnell Delvaux , Diane Patricia Miller
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。

3. 发明授权

US08840374B2 Adaptor assembly for coupling turbine blades to rotor disks 有权
标题翻译：用于将涡轮叶片耦合到转子盘的适配器组件
公开(公告)号：US08840374B2
公开(公告)日：2014-09-23
申请号：US13271635
申请日：2011-10-12
申请人： Andres Jose Garcia-Crespo , John McConnell Delvaux
发明人： Andres Jose Garcia-Crespo , John McConnell Delvaux
IPC分类号： F04D29/34 , F01D5/30
CPC分类号： F01D5/3007 , F01D5/147 , F01D5/3084 , F05D2300/6033
摘要： An adaptor assembly for coupling a blade root of a turbine blade to a root slot of a rotor disk is described. The adaptor assembly includes a turbine blade having a blade root and an adaptor body having an adaptor root. The adaptor body defines a slot having an open end configured to receive the blade root of the turbine blade such that the adaptor root of the adaptor body and the blade root of the turbine blade are adjacent to one another when the blade root of the turbine blade is positioned within the slot. Both the adaptor root of the adaptor body and the blade root of the turbine blade are configured to be received within the root slot of the rotor disk.
摘要翻译：描述了一种用于将涡轮机叶片的叶片根部联接到转子盘的根部槽的适配器组件。适配器组件包括具有叶片根部的涡轮叶片和具有适配器根部的适配器主体。适配器主体限定了具有开口端的狭槽，该开口端构造成接收涡轮机叶片的叶片根部，使得当涡轮机叶片的叶根处于适配器主体的适配器根部和涡轮叶片的叶根部时彼此相邻位于槽内。适配器主体的适配器根部和涡轮叶片的叶片根部都配置成接收在转子盘的根槽内。

4. 发明授权

US08740573B2 Adaptor assembly for coupling turbine blades to rotor disks 有权
标题翻译：用于将涡轮叶片耦合到转子盘的适配器组件
公开(公告)号：US08740573B2
公开(公告)日：2014-06-03
申请号：US13094176
申请日：2011-04-26
申请人： John McConnell Delvaux , Andres Jose Garcia-Crespo , Kilmer Joseph Joyce , Allan Randall Tindell
发明人： John McConnell Delvaux , Andres Jose Garcia-Crespo , Kilmer Joseph Joyce , Allan Randall Tindell
IPC分类号： F01D5/30
CPC分类号： F01D5/3015 , F05D2230/51 , F05D2230/61
摘要： An adaptor assembly for coupling a blade root of a turbine blade to a root slot of a rotor disk is disclosed. The adaptor assembly may generally include an adaptor body having a root configured to be received within the root slot. The adaptor body may also define a slot having an open end configured to receive the blade root. The adaptor body may further define a channel. The adaptor assembly may also include a plate having an outwardly extending foot. The foot may be configured to be received within the channel. Additionally, the plate may be configured to cover at least a portion of the open end of the slot when the foot is received within the channel.
摘要翻译：公开了一种用于将涡轮叶片的叶片根部连接到转子盘的根槽的适配器组件。适配器组件通常可以包括适配器主体，其具有被配置为接收在根槽内的根。适配器主体还可以限定具有构造成接收叶片根部的开口端的狭槽。适配器主体还可以限定通道。适配器组件还可以包括具有向外延伸的脚的板。脚可以被配置为在通道内被接收。另外，当脚在通道内被接收时，该板可构造成覆盖槽的开口端的至少一部分。

5. 发明申请

US20120275920A1 ADAPTOR ASSEMBLY FOR COUPLING TURBINE BLADES TO ROTOR DISKS 有权
标题翻译：用于将涡轮叶片联接到转盘的适配器组件
公开(公告)号：US20120275920A1
公开(公告)日：2012-11-01
申请号：US13094176
申请日：2011-04-26
申请人： John McConnell Delvaux , Andres Jose Garcia-Crespo , Kilmer Joseph Joyce , Allan Randall Tindell
发明人： John McConnell Delvaux , Andres Jose Garcia-Crespo , Kilmer Joseph Joyce , Allan Randall Tindell
IPC分类号： F01D5/30
CPC分类号： F01D5/3015 , F05D2230/51 , F05D2230/61
摘要： An adaptor assembly for coupling a blade root of a turbine blade to a root slot of a rotor disk is disclosed. The adaptor assembly may generally include an adaptor body having a root configured to be received within the root slot. The adaptor body may also define a slot having an open end configured to receive the blade root. The adaptor body may further define a channel. The adaptor assembly may also include a plate having an outwardly extending foot. The foot may be configured to be received within the channel. Additionally, the plate may be configured to cover at least a portion of the open end of the slot when the foot is received within the channel.
摘要翻译：公开了一种用于将涡轮叶片的叶片根部连接到转子盘的根槽的适配器组件。适配器组件通常可以包括适配器主体，其具有被配置为接收在根槽内的根。适配器主体还可以限定具有构造成接收叶片根部的开口端的狭槽。适配器主体还可以限定通道。适配器组件还可以包括具有向外延伸的脚的板。脚可以被配置为在通道内被接收。另外，当脚在通道内被接收时，该板可构造成覆盖槽的开口端的至少一部分。

6. 发明申请

US20130094968A1 ADAPTOR ASSEMBLY FOR COUPLING TURBINE BLADES TO ROTOR DISKS 有权
标题翻译：用于将涡轮叶片联接到转盘的适配器组件
公开(公告)号：US20130094968A1
公开(公告)日：2013-04-18
申请号：US13271635
申请日：2011-10-12
申请人： Andres Jose Garcia-Crespo , John McConnell Delvaux
发明人： Andres Jose Garcia-Crespo , John McConnell Delvaux
IPC分类号： F01D5/30
CPC分类号： F01D5/3007 , F01D5/147 , F01D5/3084 , F05D2300/6033
摘要： An adaptor assembly for coupling a blade root of a turbine blade to a root slot of a rotor disk is described. The adaptor assembly includes a turbine blade having a blade root and an adaptor body having an adaptor root. The adaptor body defines a slot having an open end configured to receive the blade root of the turbine blade such that the adaptor root of the adaptor body and the blade root of the turbine blade are adjacent to one another when the blade root of the turbine blade is positioned within the slot. Both the adaptor root of the adaptor body and the blade root of the turbine blade are configured to be received within the root slot of the rotor disk.
摘要翻译：描述了一种用于将涡轮机叶片的叶片根部联接到转子盘的根部槽的适配器组件。适配器组件包括具有叶片根部的涡轮叶片和具有适配器根部的适配器主体。适配器主体限定了具有开口端的狭槽，该开口端构造成接收涡轮机叶片的叶片根部，使得当涡轮机叶片的叶根处于适配器主体的适配器根部和涡轮叶片的叶根部时彼此相邻位于槽内。适配器主体的适配器根部和涡轮叶片的叶片根部都配置成接收在转子盘的根槽内。

7. 发明授权

US09328622B2 Blade attachment assembly 有权
标题翻译：刀片附件总成
公开(公告)号：US09328622B2
公开(公告)日：2016-05-03
申请号：US13494261
申请日：2012-06-12
申请人： Andres Jose Garcia-Crespo , John McConnell Delvaux , Diane Patricia Miller
发明人： Andres Jose Garcia-Crespo , John McConnell Delvaux , Diane Patricia Miller
IPC分类号： F01D5/30 , F01D5/14
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。

8. 发明申请

US20120181370A1 SYSTEM AND METHOD FOR REINFORCING A SUBSTRATE 有权
标题翻译：用于增强基板的系统和方法
公开(公告)号：US20120181370A1
公开(公告)日：2012-07-19
申请号：US13007697
申请日：2011-01-17
申请人： Herbert Chidsey Roberts, III , John McConnell Delvaux , Andres Jose Garcia-Crespo
发明人： Herbert Chidsey Roberts, III , John McConnell Delvaux , Andres Jose Garcia-Crespo
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。

9. 发明申请

US20130177440A1 Continuous Fiber Reinforced Mesh Bond Coat for Environmental Barrier Coating System 有权
标题翻译：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
申请人： James Zhang , Rupak Das , Herbert Chidsey Roberts, III , John McConnell Delvaux
发明人： James Zhang , Rupak Das , Herbert Chidsey Roberts, III , John McConnell Delvaux
IPC分类号： F01D5/14 , B32B38/00
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。

10. 发明授权

US09771811B2 Continuous fiber reinforced mesh bond coat for environmental barrier coating system 有权
公开(公告)号：US09771811B2
公开(公告)日：2017-09-26
申请号：US13348212
申请日：2012-01-11
申请人： James Zhang , Rupak Das , Herbert Chidsey Roberts III , John McConnell Delvaux
发明人： James Zhang , Rupak Das , Herbert Chidsey Roberts III , John McConnell Delvaux
IPC分类号： F01D5/28 , C04B41/52 , C04B41/89 , C04B41/00
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.

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