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公开(公告)号：US08715208B2
公开(公告)日：2014-05-06
申请号：US13128834
申请日：2009-11-13
申请人： Diana Hodgins , Andrew Whalley
发明人： Diana Hodgins , Andrew Whalley
CPC分类号： A61B5/112 , A01K29/005 , A61B5/1123 , A61B5/6828 , A61B2503/40 , A61B2562/0219 , A61B2562/028
摘要： A method of monitoring or assessing the motion of the limbs of a body when performing repetitive cyclic activity uses inertial measurement units secured to each of the limbs to be monitored. The operation of all of the IMUs is synchronized by way of a pulse from a computer. On performing the repetitive cyclic activity such as walking, running, trotting or galloping, the outputs of the IMUs are assembled and analyzed in realtime, to determine the relative phase of the limb movements, from which an assessment of the gait may be made.
摘要翻译： 在执行重复循环活动时监测或评估身体肢体的运动的方法使用固定到待监测的每个肢体的惯性测量单元。 所有IMU的操作通过计算机的脉冲进行同步。 在执行重复的循环活动，如步行，跑步，跑步或跳动时，IMU的输出将被实时组装和分析，以确定肢体运动的相对相位，从中可以对步态进行评估。
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公开(公告)号：US06592326B2
公开(公告)日：2003-07-15
申请号：US09977195
申请日：2001-10-16
申请人： Peter Marx , Kynan Eng , Andrew Whalley
发明人： Peter Marx , Kynan Eng , Andrew Whalley
IPC分类号： F01D904
CPC分类号： F01D11/005 , F01D9/041 , F01D9/042
摘要： In a guide vane element for a gas turbine with a vane blade extending between a platform that is located radially inward in relation to the main housing of the gas turbine and a radially outward platform, a flange is provided on at least one edge of the platforms adjoining an adjacent second guide vane element in the circumferential direction and on the side of the platform facing away from the vane blade. The second guide vane element can be attached, via a second flange provided on a second platform on the second guide vane element. The connection of the platforms forms a cover band, or a connection between the guide vane elements that is tight, flush, and stress-free at different temperatures. The attachment of two adjoining platforms to each other in the area facing away from the vane blades is a connection that is in flush contact with the adjoining flange of an adjoining platform, while a gap remains between the adjoining platforms in the area facing the vane blade and the operating gases, when the temperature remains evenly distributed and high.
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公开(公告)号：US20110194943A1
公开(公告)日：2011-08-11
申请号：US13023651
申请日：2011-02-09
CPC分类号： F01D5/187 , F01D5/22 , F05D2260/221
摘要： A turbine blade assembly in a turbine engine. The turbine blade assembly includes a turbine blade and a first snubber structure. The turbine blade includes an internal cooling passage containing cooling air. The first snubber structure extends outwardly from a sidewall of the turbine blade and includes a hollow interior portion that receives cooling air from the internal cooling passage of the turbine blade.
摘要翻译： 涡轮发动机中的涡轮叶片组件。 涡轮叶片组件包括涡轮叶片和第一缓冲结构。 涡轮机叶片包括内部冷却通道，其包含冷却空气。 第一缓冲结构从涡轮机叶片的侧壁向外延伸并且包括从涡轮叶片的内部冷却通道接收冷却空气的中空内部部分。
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公开(公告)号：US08684692B2
公开(公告)日：2014-04-01
申请号：US13023651
申请日：2011-02-09
CPC分类号： F01D5/187 , F01D5/22 , F05D2260/221
摘要： A turbine blade assembly in a turbine engine. The turbine blade assembly includes a turbine blade and a first snubber structure. The turbine blade includes an internal cooling passage containing cooling air. The first snubber structure extends outwardly from a sidewall of the turbine blade and includes a hollow interior portion that receives cooling air from the internal cooling passage of the turbine blade.
摘要翻译： 涡轮发动机中的涡轮叶片组件。 涡轮叶片组件包括涡轮叶片和第一缓冲结构。 涡轮机叶片包括内部冷却通道，其包含冷却空气。 第一缓冲结构从涡轮机叶片的侧壁向外延伸并且包括从涡轮叶片的内部冷却通道接收冷却空气的中空内部部分。
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公开(公告)号：USRE43611E1
公开(公告)日：2012-08-28
申请号：US11181003
申请日：2005-07-14
申请人： Peter Marx , Kynan Eng , Andrew Whalley
发明人： Peter Marx , Kynan Eng , Andrew Whalley
IPC分类号： F01D9/04
CPC分类号： F01D11/005 , F01D9/041 , F01D9/042
摘要： In a guide vane element for a gas turbine with a vane blade extending between a platform that is located radially inward in relation to the main housing of the gas turbine and a radially outward platform, a flange is provided on at least one edge of the platforms adjoining an adjacent second guide vane element in the circumferential direction and on the side of the platform facing away from the vane blade. The second guide vane element can be attached, via a second flange provided on a second platform on the second guide vane element. The connection of the platforms forms a cover band, or a connection between the guide vane elements that is tight, flush, and stress-free at different temperatures. The attachment of two adjoining platforms to each other in the area facing away from the vane blades is a connection that is in flush contact with the adjoining flange of an adjoining platform, while a gap remains between the adjoining platforms in the area facing the vane blade and the operating gases, when the temperature remains evenly distributed and high.
摘要翻译： 在用于具有叶片叶片的燃气轮机的导向叶片元件中，叶片叶片相对于燃气轮机的主壳体径向向内定位的平台和径向向外的平台之间延伸，在平台的至少一个边缘上设置有凸缘 邻接第二导向叶片元件沿圆周方向和平台背离叶片叶片的一侧。 第二导叶元件可以通过设置在第二导叶元件上的第二平台上的第二凸缘来附接。 平台的连接形成盖带，或在不同温度下紧固，齐平和无应力的导向叶片元件之间的连接。 在背离叶片叶片的区域中，两个邻接的平台相互连接在一起，与邻接的平台的相邻的凸缘齐平，而在与叶片叶片相对的区域中相邻的平台之间留有间隙 和工作气体，当温度保持均匀分布和高度。
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6.发明申请公开(公告)号：US20090129915A1
公开(公告)日：2009-05-21
申请号：US11941162
申请日：2007-11-16
申请人： Andrew Whalley
发明人： Andrew Whalley
IPC分类号： F01D5/14
CPC分类号： F01D5/186 , F05D2240/122 , F05D2240/304 , F05D2260/202
摘要： A cooling system for a turbine airfoil of a turbine engine having a trailing edge cooling slot positioned within the generally elongated, hollow airfoil and extending from the trailing edge chordwise into the generally elongated, hollow airfoil toward the leading edge such that a secondary trailing edge is offset upstream from the trailing edge. As such, the trailing edge cooling slot reduces stress formation at the trailing edge of the turbine airfoil.
摘要翻译： 一种用于涡轮发动机的涡轮机翼型的冷却系统，其具有位于所述大致细长的中空翼型件内的后缘冷却槽，并且从所述尾缘向后延伸到所述大致细长的中空翼型件中，使得第二后缘为 偏离后缘的上游。 因此，后缘冷却槽减少了在涡轮机翼缘的后缘处的应力形成。
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公开(公告)号：US20110218463A1
公开(公告)日：2011-09-08
申请号：US13128834
申请日：2009-11-13
申请人： Diana Hodgins , Andrew Whalley
发明人： Diana Hodgins , Andrew Whalley
IPC分类号： A61B5/103
CPC分类号： A61B5/112 , A01K29/005 , A61B5/1123 , A61B5/6828 , A61B2503/40 , A61B2562/0219 , A61B2562/028
摘要： A method of monitoring or assessing the motion of the limbs of a body when performing repetitive cyclic activity uses inertial measurement units secured to each of the limbs to be monitored. The operation of all of the IMUs is synchronised by way of a pulse from a computer. On performing the repetitive cyclic activity such as walking, running, trotting or galloping, the outputs of the IMUs are assembled and analysed in realtime, to determine the relative phase of the limb movements, from which an assessment of the gait may be made.
摘要翻译： 在执行重复循环活动时监测或评估身体肢体的运动的方法使用固定到待监测的每个肢体的惯性测量单元。 所有IMU的操作通过计算机的脉冲进行同步。 在执行重复的循环活动，如步行，跑步，跑步或跳动时，IMU的输出将被实时组装和分析，以确定肢体运动的相对相位，从中可以对步态进行评估。
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8.发明授权公开(公告)号：US08002525B2
公开(公告)日：2011-08-23
申请号：US11941162
申请日：2007-11-16
申请人： Andrew Whalley
发明人： Andrew Whalley
IPC分类号： F01D5/08
CPC分类号： F01D5/186 , F05D2240/122 , F05D2240/304 , F05D2260/202
摘要： A cooling system for a turbine airfoil of a turbine engine having a trailing edge cooling slot positioned within the generally elongated, hollow airfoil and extending from the trailing edge chordwise into the generally elongated, hollow airfoil toward the leading edge such that a secondary trailing edge is offset upstream from the trailing edge. As such, the trailing edge cooling slot reduces stress formation at the trailing edge of the turbine airfoil.
摘要翻译： 一种用于涡轮发动机的涡轮机翼型的冷却系统，其具有位于所述大致细长的中空翼型件内的后缘冷却槽，并且从所述尾缘向后延伸到所述大致细长的中空翼型件中，使得第二后缘为 偏离后缘的上游。 因此，后缘冷却槽减少了在涡轮机翼缘的后缘处的应力形成。
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