公开(公告)号：US20130121839A1

公开(公告)日：2013-05-16

申请号：US13812207

申请日：2011-07-08

申请人： Stephen Batt ,  Scott Charlton

发明人： Stephen Batt ,  Scott Charlton

IPC分类号： F01D5/28

CPC分类号： F01D5/288 ,  F01D5/187 ,  F01D9/06 ,  F05D2230/90 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2250/292

摘要： A turbine airfoil including an airfoil body is disclosed. The airfoil includes a leading edge, a trailing edge, an exterior surface including a suction side extending from the leading edge to the trailing edge and a pressure side extending from the leading edge to a trailing end. The pressure side is located opposite to the suction side on the airfoil body. The complete pressure side of the exterior surface is coated by a thermal barrier coating with a thickness decreasing towards the trailing end.

摘要翻译： 公开了一种包括翼型体的涡轮机翼型。 翼型件包括前缘，后缘，包括从前缘延伸到后缘的吸力侧的外表面和从前缘延伸到后端的压力侧。 压力侧与翼型体上的吸力侧相对。 外表面的完整压力侧涂覆有厚度朝后端减小的热障涂层。

公开(公告)号：US4986263A

公开(公告)日：1991-01-22

申请号：US512858

申请日：1990-04-23

申请人： Jeffrey P. Dickerson ,  Scott Charlton

发明人： Jeffrey P. Dickerson ,  Scott Charlton

IPC分类号： A61F5/01

CPC分类号： A61F5/0109 ,  A61F2005/0176 ,  Y10S2/91 ,  Y10S2/911

摘要： An anatomical musculoskeletal therapeutic knee sleeve support especially adapted to be placed over the knee to provide support for the muscles and skeletal structure of the knee during physical activity, particularly sports activity. The sleeve comprises a single panel of flexible resilient material cut and joined in such a manner that there is a stitched seam at the upper half of the sleeve on one side of the knee posterior to the side of the knee and another stitched seam at the lower half of the sleeve on the other side of the knee posterior of the side of the knee and an open horizontal aperture at the rear flexure point of the knee between central points of the stitched seams.

摘要翻译： 一种解剖学上的肌肉骨骼治疗性膝关节支撑，特别适合放置在膝盖上，以在身体活动，特别是运动活动期间为膝盖的肌肉和骨骼结构提供支撑。 套筒包括一个单一的柔性弹性材料板，以这样一种方式切割和接合，使得在膝部的一侧的膝盖的上半部分在膝盖的上半部有一个缝合的接缝，另一个在下面的缝合接缝 在膝盖侧面的另一侧的袖子的一半，并且在缝合接缝的中心点之间的膝部的后弯曲点处具有敞开的水平孔。

公开(公告)号：US08545181B2

公开(公告)日：2013-10-01

申请号：US12311837

申请日：2007-08-31

申请人： Scott Charlton

发明人： Scott Charlton

IPC分类号： B63H1/16

CPC分类号： F01D11/006 ,  F05D2300/501 ,  Y10T29/49321

摘要： A turbine blade assembly, which can be used for a gas turbine is provided. The turbine blade assembly includes turbine blades with platforms, gaps between the platforms of adjacent turbine blades and seals. Each seal covers the gap between the platforms of two adjacent turbine blades wherein the platforms are provided with slots extending in the downstream flow direction. The turbine blades have root cavities, wherein the seal covers at least the whole length of the root cavities of two adjacent turbine blades. The seal is formed from a strip and the seal is placed in two opposed slots formed in each of the platforms of two adjacent turbine blades and open towards the respective downstream ends.

摘要翻译： 提供了可用于燃气轮机的涡轮机叶片组件。 涡轮机叶片组件包括具有平台的涡轮叶片，相邻涡轮机叶片的平台和密封件之间的间隙。 每个密封件覆盖两个相邻涡轮叶片的平台之间的间隙，其中平台设置有沿下游流动方向延伸的槽。 涡轮叶片具有根腔，其中密封件至少覆盖两个相邻的涡轮叶片的根部腔的整个长度。 密封由条带形成，并且密封件被放置在形成在两个相邻的涡轮叶片的每个平台中的两个相对的槽中并且朝向相应的下游端开口。

公开(公告)号：US20100178173A1

公开(公告)日：2010-07-15

申请号：US12311837

申请日：2007-08-31

申请人： Scott Charlton

发明人： Scott Charlton

IPC分类号： F01D11/00

CPC分类号： F01D11/006 ,  F05D2300/501 ,  Y10T29/49321

摘要： A turbine blade assembly, which can be used for a gas turbine is provided. The turbine blade assembly includes turbine blades with platforms, gaps between the platforms of adjacent turbine blades and seals. Each seal covers the gap between the platforms of two adjacent turbine blades wherein the platforms are provided with slots extending in the downstream flow direction. The turbine blades have root cavities, wherein the seal covers at least the whole length of the root cavities of two adjacent turbine blades. The seal is formed from a strip and the seal is placed in two opposed slots formed in each of the platforms of two adjacent turbine blades and open towards the respective downstream ends.

摘要翻译： 提供了可用于燃气轮机的涡轮机叶片组件。 涡轮机叶片组件包括具有平台的涡轮叶片，相邻涡轮机叶片的平台和密封件之间的间隙。 每个密封件覆盖两个相邻涡轮叶片的平台之间的间隙，其中平台设置有沿下游流动方向延伸的槽。 涡轮叶片具有根腔，其中密封件至少覆盖两个相邻的涡轮叶片的根部腔的整个长度。 密封由条带形成，并且密封件被放置在形成在两个相邻的涡轮叶片的每个平台中的两个相对的槽中并且朝向相应的下游端开口。

公开(公告)号：US09416669B2

公开(公告)日：2016-08-16

申请号：US13812207

申请日：2011-07-08

申请人： Stephen Batt ,  Scott Charlton

发明人： Stephen Batt ,  Scott Charlton

IPC分类号： F01D5/18 ,  F01D9/06 ,  F01D5/28

CPC分类号： F01D5/288 ,  F01D5/187 ,  F01D9/06 ,  F05D2230/90 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2250/292

摘要： A turbine airfoil including an airfoil body is disclosed. The airfoil includes a leading edge, a trailing edge, an exterior surface including a suction side extending from the leading edge to the trailing edge and a pressure side extending from the leading edge to a trailing end. The pressure side is located opposite to the suction side on the airfoil body. The complete pressure side of the exterior surface is coated by a thermal barrier coating with a thickness decreasing towards the trailing end.

摘要翻译： 公开了一种包括翼型体的涡轮机翼型。 翼型件包括前缘，后缘，包括从前缘延伸到后缘的吸力侧的外表面和从前缘延伸到后端的压力侧。 压力侧与翼型体上的吸力侧相对。 外表面的完整压力侧涂覆有厚度朝后端减小的热障涂层。

公开(公告)号：US08096776B2

公开(公告)日：2012-01-17

申请号：US12312048

申请日：2007-08-31

申请人： Richard Bluck ,  Scott Charlton

发明人： Richard Bluck ,  Scott Charlton

IPC分类号： B63H1/20 ,  B63H13/00

CPC分类号： F01D5/3015 ,  F05D2250/182 ,  F05D2250/70 ,  F05D2260/30

摘要： A turbine blade assembly, in particular of a gas turbine, is provided. The turbine blade assembly includes a turbine disc with rotor blades inserted into notches of the turbine disc and locking plates that are placed inside circular grooves with rims in the turbine disc and in the rotor blade. The edges of the locking plates that are oriented towards the center of the turbine disc are castellated by providing teeth and accordingly a part of the rim of the circular groove of the turbine disc is also castellated by providing gaps and whereby the gaps of the rim match the teeth of the locking plates. The locking plates have a spring-back force to provide both locking and sealing capabilities during engine operation.

摘要翻译： 提供了一种涡轮叶片组件，特别是一种燃气轮机。 涡轮机叶片组件包括涡轮盘，其具有插入到涡轮盘的凹口中的转子叶片和锁定板，所述锁定板放置在具有轮缘在涡轮盘和转子叶片中的圆形槽内。 通过提供齿，锁定板的朝向涡轮盘的中心的边缘被铸造，因此，涡轮盘的圆形槽的边缘的一部分也通过提供间隙而被浇注，由此轮缘的间隙匹配 锁板的齿。 锁定板具有回弹力，以在发动机操作期间提供锁定和密封能力。

公开(公告)号：US20100047073A1

公开(公告)日：2010-02-25

申请号：US12312048

申请日：2007-08-31

申请人： Richard Bluck ,  Scott Charlton

发明人： Richard Bluck ,  Scott Charlton

IPC分类号： F01D5/32

CPC分类号： F01D5/3015 ,  F05D2250/182 ,  F05D2250/70 ,  F05D2260/30

摘要： A turbine blade assembly, in particular of a gas turbine, is provided. The turbine blade assembly includes a turbine disc with rotor blades inserted into notches of the turbine disc and locking plates that are placed inside circular grooves with rims in the turbine disc and in the rotor blade. The edges of the locking plates that are oriented towards the center of the turbine disc are castellated by providing teeth and accordingly a part of the rim of the circular groove of the turbine disc is also castellated by providing gaps and whereby the gaps of the rim match the teeth of the locking plates. The locking plates have a spring-back force to provide both locking and sealing capabilities during engine operation.

摘要翻译： 提供了一种涡轮叶片组件，特别是一种燃气轮机。 涡轮机叶片组件包括涡轮盘，其具有插入到涡轮盘的凹口中的转子叶片和锁定板，所述锁定板放置在具有轮缘在涡轮盘和转子叶片中的圆形槽内。 通过提供齿，锁定板的朝向涡轮盘的中心的边缘被铸造，因此，涡轮盘的圆形槽的边缘的一部分也通过提供间隙而被浇注，由此轮缘的间隙匹配 锁板的齿。 锁定板具有回弹力，以在发动机操作期间提供锁定和密封能力。