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公开(公告)号:US10060262B2
公开(公告)日:2018-08-28
申请号:US14895139
申请日:2014-05-28
Applicant: United Technologies Corporation
Inventor: Robert Knowlton , Max Asterlin , Brandon M. Rapp , Parth Jariwala
CPC classification number: F01D5/10 , F01D5/081 , F01D5/18 , F01D5/26 , F01D11/006 , F05D2240/57 , F05D2260/96 , Y02T50/676
Abstract: A turbine blade vibration damper is described. The damper has an axially-extending main body defining an inner surface and opposed damping surface. The main body also has an edge spanning from the inner surface to the damping surface and slotted apertures extending through the main body. The slotted apertures extend between the inner surface and damping surface. Adjacent pairs of slotted apertures have elongated shapes defining longitudinal axes that intersect at a point off the surface of the damper.
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公开(公告)号:US20160102557A1
公开(公告)日:2016-04-14
申请号:US14895139
申请日:2014-05-28
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor: Robert Knowlton , Max Asterlin , Brandon M. Rapp , Parth Jariwala
CPC classification number: F01D5/10 , F01D5/081 , F01D5/18 , F01D5/26 , F01D11/006 , F05D2240/57 , F05D2260/96 , Y02T50/676
Abstract: A turbine blade vibration damper is described. The damper has an axially-extending main body defining an inner surface and opposed damping surface. The main body also has an edge spanning from the inner surface to the damping surface and slotted apertures extending through the main body. The slotted apertures extend between the inner surface and damping surface. Adjacent pairs of slotted apertures have elongated shapes defining longitudinal axes that intersect at a point off the surface of the damper.
Abstract translation: 描述了涡轮叶片减振器。 阻尼器具有轴向延伸的主体,其限定内表面和相对的阻尼表面。 主体还具有从内表面到阻尼表面的边缘,并且延伸穿过主体的开槽孔。 开槽孔在内表面和阻尼表面之间延伸。 相邻的开槽孔对形成了限定纵向轴线的细长形状,该轴线在阻尼器表面的一个点处相交。
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