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1. 发明授权

US08186056B2 Turbine vane restoration system 有权
标题翻译：涡轮叶片修复系统
公开(公告)号：US08186056B2
公开(公告)日：2012-05-29
申请号：US11823767
申请日：2007-06-28
申请人： Robert S. Willis , Scott P. Irwin , Stacy Fang , Thomas H. Milidantri, Jr. , Adam J. Taetsch , Martin C. Gosling , Georg Bostanjoglo , Dan Shipman , Orville Morgan , Gerry Milidantri
发明人： Robert S. Willis , Scott P. Irwin , Stacy Fang , Thomas H. Milidantri, Jr. , Adam J. Taetsch , Martin C. Gosling , Georg Bostanjoglo , Dan Shipman , Orville Morgan , Gerry Milidantri
IPC分类号： B23P6/00
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/80 , Y10T29/49318 , Y10T29/4975
摘要： A system and method for reconfiguring a turbine vane. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by fixing portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane, restricting other portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane to only move rotationally about a centerline of the inner or outer shrouds, and applying a load to various portions of the inner and outer shrouds and the airfoil to return the turbine vane to be within predetermined specifications.
摘要翻译：一种用于重新配置涡轮叶片的系统和方法。在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。翼片可以通过固定涡轮叶片的内护罩和外护罩的前钩和后钩的部分而被拉直，限制涡轮叶片的内护罩和外护罩的前钩和后钩的其它部分仅仅围绕涡轮叶片旋转移动内部或外部护罩的中心线，并且将负载施加到内部和外部护罩和翼型件的各个部分以将涡轮叶片返回到预定规格内。

2. 发明申请

US20090000102A1 Turbine vane restoration system 有权
标题翻译：涡轮叶片修复系统
公开(公告)号：US20090000102A1
公开(公告)日：2009-01-01
申请号：US11823767
申请日：2007-06-28
申请人： Robert S. Willis , Scott P. Irwin , Stacy Fang , Thomas H. Milidantry, JR. , Adam J. Taetsch , Martin C. Gosling , Georg Bostanjoglo , Dan Shipman , Orville Morgan , Gerry Milidantri
发明人： Robert S. Willis , Scott P. Irwin , Stacy Fang , Thomas H. Milidantry, JR. , Adam J. Taetsch , Martin C. Gosling , Georg Bostanjoglo , Dan Shipman , Orville Morgan , Gerry Milidantri
IPC分类号： B21D1/00
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/80 , Y10T29/49318 , Y10T29/4975
摘要： A system and method for reconfiguring a turbine vane. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by fixing portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane, restricting other portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane to only move rotationally about a centerline of the inner or outer shrouds, and applying a load to various portions of the inner and outer shrouds and the airfoil to return the turbine vane to be within predetermined specifications.
摘要翻译：一种用于重新配置涡轮叶片的系统和方法。在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。翼片可以通过固定涡轮叶片的内护罩和外护罩的前钩和后钩的部分而被拉直，限制涡轮叶片的内护罩和外护罩的前钩和后钩的其它部分仅仅围绕涡轮叶片旋转移动内部或外部护罩的中心线，并且将负载施加到内部和外部护罩和翼型件的各个部分，以将涡轮叶片返回到预定规格内。

3. 发明授权

US07730756B2 Turbine vane airfoil reconfiguration method 失效
标题翻译：涡轮叶片翼型重构方法
公开(公告)号：US07730756B2
公开(公告)日：2010-06-08
申请号：US12372168
申请日：2009-02-17
申请人： Martin C. Gosling , Jefferson Davis , Yong Kang
发明人： Martin C. Gosling , Jefferson Davis , Yong Kang
IPC分类号： B21D53/78 , B21D3/16 , B23P6/00
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/80 , Y10T29/37 , Y10T29/49316 , Y10T29/49318 , Y10T29/49325 , Y10T29/49336 , Y10T29/49716 , Y10T29/49718 , Y10T29/53
摘要： A system and method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.
摘要翻译：一种用于重新配置涡轮叶片段的翼型的系统和方法。在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。可以通过沿与涡轮叶片段的外护罩大致相切的方向向内护罩施加负载来使翼型矫直。孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。在完成该过程之后，可以密封孔。

4. 发明申请

US20090260206A1 TURBINE VANE AIRFOIL RECONFIGURATION METHOD 失效
标题翻译：涡轮风力发电机重构方法
公开(公告)号：US20090260206A1
公开(公告)日：2009-10-22
申请号：US12372168
申请日：2009-02-17
申请人： Martin C. Gosling , Jefferson Davis , Yong Kang
发明人： Martin C. Gosling , Jefferson Davis , Yong Kang
IPC分类号： B23P6/00
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/80 , Y10T29/37 , Y10T29/49316 , Y10T29/49318 , Y10T29/49325 , Y10T29/49336 , Y10T29/49716 , Y10T29/49718 , Y10T29/53
摘要： A system and method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.
摘要翻译：一种用于重新配置涡轮叶片段的翼型的系统和方法。在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。可以通过沿与涡轮叶片段的外护罩大致相切的方向向内护罩施加负载来使翼型矫直。孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。在完成该过程之后，可以密封孔。

5. 发明授权

US07536783B2 Turbine vane airfoil reconfiguration method 有权
标题翻译：涡轮叶片翼型重构方法
公开(公告)号：US07536783B2
公开(公告)日：2009-05-26
申请号：US11591908
申请日：2006-11-02
申请人： Jefferson Davis , Martin C. Gosling , Yong Kang
发明人： Jefferson Davis , Martin C. Gosling , Yong Kang
IPC分类号： B21D53/78 , B23P6/00
CPC分类号： F01D5/005 , B23P6/002 , F05D2230/80 , Y10T29/49316 , Y10T29/49318 , Y10T29/4932 , Y10T29/49325 , Y10T29/49336 , Y10T29/49716 , Y10T29/49721
摘要： A method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the method may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by heating the airfoil to no more than 750 degrees F. while applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. The load is up to 6000 lbf. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.
摘要翻译：一种用于重新配置涡轮叶片段的翼型的方法。在至少一个实施例中，该方法可以用于矫直涡轮叶片段的翼型以去除倾斜，扭转或翻倒，或其任何组合。通过将翼型件加热至不超过750华氏度，同时在与涡轮叶片段的外护罩大致相切的方向上向内护罩施加负载的情况下，翼型件可被矫直。负载高达6000 lbf。孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。在完成该过程之后，可以密封孔。

6. 发明授权

US07503113B2 Turbine vane airfoil reconfiguration system 有权
标题翻译：涡轮叶片翼型重构系统
公开(公告)号：US07503113B2
公开(公告)日：2009-03-17
申请号：US11249791
申请日：2005-10-13
申请人： Martin C. Gosling , Jefferson Davis , Yong Kang
发明人： Martin C. Gosling , Jefferson Davis , Yong Kang
IPC分类号： B21D53/78
CPC分类号： B23P6/002 , F01D5/005 , F05D2230/80 , Y10T29/37 , Y10T29/49316 , Y10T29/49318 , Y10T29/49325 , Y10T29/49336 , Y10T29/49716 , Y10T29/49718 , Y10T29/53
摘要： A system and method for reconfiguring an airfoil of a turbine vane segment. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by applying a load to an inner shroud in a direction that is generally tangential to an outer shroud of the turbine vane segment. Orifices may be cut into the airfoil suction side, inboard of the outer shroud, to facilitate the straightening process. The orifices may be sealed upon completion of the process.
摘要翻译：一种用于重新配置涡轮叶片段的翼型的系统和方法。在至少一个实施例中，该系统可以用于矫直涡轮叶片段的翼型件以去除倾斜，扭转或翻倒，或其任何组合。可以通过沿与涡轮叶片段的外护罩大致相切的方向向内护罩施加负载来使翼型矫直。孔可以被切入机翼吸入侧，在外护罩的内侧，以便矫直过程。在完成该过程之后，可以密封孔。

7. 发明授权

US4183714A Lubricant sealing means for a compressor shaft 失效
标题翻译：用于压缩机轴的润滑剂密封装置
公开(公告)号：US4183714A
公开(公告)日：1980-01-15
申请号：US851351
申请日：1977-11-14
申请人： Martin C. Gosling
发明人： Martin C. Gosling
IPC分类号： F04D29/10 , F04D29/08
CPC分类号： F04D29/104
摘要： A compressor comprises one or more stages each including an impeller mounted for rotation on a shaft and rotatable in an impeller housing. A transmission is drivingly connected to the shaft and a bearing is provided supporting the shaft. Lubrication means are provided for the bearing which provide a continuous lubricant seal around the shaft between the shaft and the bearing to prevent air leaking through the bearing. A chamber is located between the impeller housing and the bearing for collecting excess lubricant and has an outlet for draining lubricant.
摘要翻译：压缩机包括一个或多个阶段，每个阶段包括叶轮，叶轮安装成可在轴上旋转并可在叶轮壳体中旋转。变速器驱动地连接到轴，并且设置支撑轴的轴承。为轴承提供润滑装置，其在轴和轴承之间围绕轴提供连续的润滑剂密封，以防止空气通过轴承泄漏。腔室位于叶轮壳体和轴承之间，用于收集多余的润滑剂，并具有用于排出润滑剂的出口。

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