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1. 发明授权

US07507071B2 Cooling arrangement 有权
标题翻译：冷却布置
公开(公告)号：US07507071B2
公开(公告)日：2009-03-24
申请号：US11262754
申请日：2005-11-01
申请人： Michiel Kopmels , Michael Jago , Keith Sadler , Peter Goodman
发明人： Michiel Kopmels , Michael Jago , Keith Sadler , Peter Goodman
IPC分类号： F01D5/08 , F01D5/18
CPC分类号： F01D5/187 , F05D2260/201
摘要： A cooling arrangement is provided in which an incident coolant flow is presented to a passage such that a proportion of that flow is diverted in order to create a standing relative overpressure in a chamber compared to the actual static pressure of the flow in the passage. In such circumstances through flow transfer apertures in the walls of the chamber forced coolant flows are presented for impingement upon surfaces and therefore greater heat transfer. Generally, coolant flow is presented to both ends of the chamber in order to create the relative standing overpressure in the chamber relative to the current static pressure presented in the passage through the incident flow. In such circumstances through utilizing the dynamic rotation or other motion of a component incorporating the arrangement a higher relative pressure is achieved for greater force coolant flow projection compared to the incident or actual static pressure of the incident coolant flow in the.
摘要翻译：提供了一种冷却装置，其中入口冷却剂流被提供给通道，使得该流量的一部分被转向，以便与通道中的流动的实际静压力相比在腔室中产生静止的相对超压。在这种情况下，通过腔室壁中的流动传递孔强制冷却剂流被施加以冲击在表面上，因此更大的热传递。通常，冷却剂流动被呈现到室的两端，以便相对于在通过入射流的通道中呈现的当前静压力而在腔室中产生相对静止的超压。在这种情况下，通过利用结合了该装置的部件的动态旋转或其他运动，可获得较高的相对压力，以便与在其中的入射冷却剂流的入射或实际静压相比更大的力冷却剂流量投影。

2. 发明申请

US20060104814A1 Heat transfer arrangement 有权
标题翻译：传热装置
公开(公告)号：US20060104814A1
公开(公告)日：2006-05-18
申请号：US11272969
申请日：2005-11-15
申请人： Michiel Kopmels , Keith Sadler
发明人： Michiel Kopmels , Keith Sadler
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2250/231 , F05D2250/241 , F05D2250/313 , F05D2250/314 , F05D2260/201
摘要： A heat transfer arrangement comprises a target member (28 or 30), and an impingement member (32). The impingement member (32) defines a fluid path (38 or 40) there through to direct fluid onto the target member. The arrangement includes a fluid directing formation (42) on the impingement member (32). The fluid path (38 or 40) extends through the fluid directory formation (42) such that the fluid path directs fluid to exit there from at an exit angle that is substantially orthogonal to the fluid directing formation.
摘要翻译：传热装置包括目标构件（28或30）和冲击构件（32）。冲击构件（32）在其上限定流体路径（38或40）以将流体引导到目标构件上。该装置包括在冲击构件（32）上的流体引导构件（42）。流体路径（38或40）延伸穿过流体目录形成（42），使得流体路径引导流体从基本上垂直于流体引导结构的出射角度离开该流体路径。

3. 发明授权

US07648340B2 First stage turbine airfoil 有权
标题翻译：第一级涡轮机翼型
公开(公告)号：US07648340B2
公开(公告)日：2010-01-19
申请号：US11643091
申请日：2006-12-21
申请人： Keith Sadler , Andrew Thomas Napper
发明人： Keith Sadler , Andrew Thomas Napper
IPC分类号： F01D5/14
CPC分类号： F01D5/141 , F05D2250/70 , F05D2250/74 , Y10S416/02
摘要： The present invention provides an airfoil for a first stage turbine blade having an external surface with first and second sides. The external surface extends spanwise between a hub and a tip and streamwise between a leading edge and a trailing edge of the airfoil. The external surface includes a contour substantially defined by Table 1 as listed in the specification.
摘要翻译：本发明提供一种用于第一级涡轮机叶片的翼型件，其具有带有第一和第二侧面的外表面。外表面在毂和尖端之间的翼展方向延伸，并且在翼型的前缘和后缘之间流动地延伸。外表面包括基本上由说明书中列出的表1所定义的轮廓。

4. 发明申请

US20060140763A1 Cooling arrangement 有权
标题翻译：冷却布置
公开(公告)号：US20060140763A1
公开(公告)日：2006-06-29
申请号：US11262754
申请日：2005-11-01
申请人： Michiel Kopmels , Michael Jago , Keith Sadler , Peter Goodman
发明人： Michiel Kopmels , Michael Jago , Keith Sadler , Peter Goodman
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2260/201
摘要： A cooling arrangement 11 is provided in which an incident coolant flow 23 is presented to a passage 14 such that a proportion of that flow is diverted in order to create a standing relative overpressure in a chamber 24 compared to the actual static pressure of the flow 23 in the passage 14. In such circumstances through flow transfer apertures in the walls of the chamber 24 forced coolant flows are presented for impingement upon surfaces 26, 27 and therefore greater heat transfer. Generally, coolant flow is presented to both ends of the chamber 24 in order to create the relative standing overpressure in the chamber 24 relative to the current static pressure presented in the passage 14 through the incident flow 23. In such circumstances through utilising the dynamic rotation or other motion of a component incorporating the arrangement 11a higher relative pressure is achieved for greater force coolant flow 22 projection compared to the incident or actual static pressure of the incident coolant flow 23 in the passage 14.
摘要翻译：提供了冷却装置11，其中入口冷却剂流23被提供到通道14，使得该流量的一部分被转向以便在腔室24中产生与流23的实际静压力相比的静止相对超压在这种情况下，通过腔室24的壁中的流动传递孔被迫使冷却剂流动被施加以冲击在表面26,27上并且因此更大的热传递。通常，冷却剂流动被呈现到腔室24的两端，以便相对于通过入射流23在通道14中呈现的当前静压力而在腔室24中产生相对站立的超压。在这种情况下，通过利用动态旋转或者与通道14中的入射冷却剂流23的入射或实际静压相比，能够实现更大的力冷却剂流22的投影，或者包含结构11的部件的其它运动具有较高的相对压力。

5. 发明申请

US20060039787A1 Component having a cooling arrangement 有权
标题翻译：具有冷却装置的部件
公开(公告)号：US20060039787A1
公开(公告)日：2006-02-23
申请号：US11199180
申请日：2005-08-09
申请人： Peter Goodman , Keith Sadler , Michiel Kopmels
发明人： Peter Goodman , Keith Sadler , Michiel Kopmels
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F05D2260/202
摘要： A component such as a turbine blade for a gas turbine engine has a cooling arrangement comprising a supply passage 18 within the blade from which extend cooling passages 28 of a first array which open at discharge openings 29, for example at a trailing edge of the blade. Cooling passages 30 of a second array extend into the blade from discharge openings 31, and intersect the passages 28. The passages 30 terminate short of the supply passage 18. As a result of this arrangement, the limiting flow area for cooling air is defined by the cooling passages 28 of the first array, and is not affected by the accuracy with which the cooling passages 30 of the second array intersect the cooling passages 28 of the first array.
摘要翻译：诸如用于燃气涡轮发动机的涡轮机叶片的部件具有冷却装置，该冷却装置包括在叶片内的供应通道18，在其中延伸第一阵列的冷却通道28，其在排出开口29处例如在叶片的后缘处打开。第二阵列的冷却通道30从排出口31延伸到叶片中，并与通道28相交。通道30终止于供应通道18的末端。由于这种布置，冷却空气的限制流动面积由第一阵列的冷却通道28不受第二阵列的冷却通道30与第一阵列的冷却通道28相交的精度的影响。

6. 发明授权

US2817524A Orthopaedic exercising device 失效
标题翻译：矫形器械
公开(公告)号：US2817524A
公开(公告)日：1957-12-24
申请号：US45086054
申请日：1954-08-19
申请人： KEITH SADLER HELEN
发明人： KEITH SADLER HELEN
IPC分类号： A63B21/00 , A63B21/015 , A63B23/12
CPC分类号： A63B23/12 , A63B21/015 , A63B21/4035 , A63B21/4047 , A63B21/4049 , A63B23/03508

7. 外观设计

USD639158S1 Container 有权
公开(公告)号：USD639158S1
公开(公告)日：2011-06-07
申请号：US29362419
申请日：2010-05-25
申请人： Daniel T. Whitehead , H. Keith Sadler
设计人： Daniel T. Whitehead , H. Keith Sadler

8. 发明申请

US20070183897A1 First stage turbine airfoil 有权
标题翻译：第一级涡轮机翼型
公开(公告)号：US20070183897A1
公开(公告)日：2007-08-09
申请号：US11643091
申请日：2006-12-21
申请人： Keith Sadler , Andrew Napper
发明人： Keith Sadler , Andrew Napper
IPC分类号： B64C27/46
CPC分类号： F01D5/141 , F05D2250/70 , F05D2250/74 , Y10S416/02
摘要： The present invention provides an airfoil for a first stage turbine blade having an external surface with first and second sides. The external surface extends spanwise between a hub and a tip and streamwise between a leading edge and a trailing edge of the airfoil. The external surface includes a contour substantially defined by Table 1 as listed in the specification.
摘要翻译：本发明提供一种用于第一级涡轮机叶片的翼型件，其具有带有第一和第二侧面的外表面。外表面在毂和尖端之间的翼展方向延伸，并且在翼型的前缘和后缘之间流动地延伸。外表面包括基本上由说明书中列出的表1所定义的轮廓。

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