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公开(公告)号:US20080112803A1
公开(公告)日:2008-05-15
申请号:US11598450
申请日:2006-11-13
IPC分类号: F01D5/02
CPC分类号: F01D25/246 , F05D2230/642 , F05D2260/30 , F05D2300/143 , F05D2300/21 , F05D2300/2283
摘要: An assembly for mounting a ceramic turbine vane ring onto a turbine support casing comprises a first metal clamping ring and a second metal clamping ring. The first metal clamping ring is configured to engage with a first side of a tab member of the ceramic turbine vane ring. The second metal clamping ring is configured to engage with a second side of the tab member such that the tab member is disposed between the first and second metal clamping rings.
摘要翻译: 用于将陶瓷涡轮叶片环安装到涡轮机支撑壳体上的组件包括第一金属夹紧环和第二金属夹紧环。 第一金属夹紧环构造成与陶瓷涡轮叶片环的突片构件的第一侧接合。 第二金属夹紧环构造成与突片构件的第二侧接合,使得突片构件设置在第一和第二金属夹紧环之间。
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公开(公告)号:US11000899B2
公开(公告)日:2021-05-11
申请号:US13360753
申请日:2012-01-29
IPC分类号: B22F5/04 , C22C14/00 , F01D5/14 , F01D5/28 , B22F10/20 , C23C22/73 , B23P15/04 , B33Y50/02 , C23C28/02 , F01D25/00 , C23C26/02 , B29C64/153 , C23C22/70 , C23C14/28 , C23C22/72 , B21D53/78 , C23C24/10 , B29C64/386 , B33Y10/00 , B33Y80/00
摘要: A method of forming an airfoil includes the steps of depositing material to form an airfoil in a first layer, and then depositing material in a second layer on the first layer. The first and second layers have distinct densities. An airfoil is also disclosed. The method provides powerful design advantages.
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3.
公开(公告)号:US20130195671A1
公开(公告)日:2013-08-01
申请号:US13360753
申请日:2012-01-29
CPC分类号: B22F5/04 , B22F3/1055 , B33Y10/00 , B33Y80/00 , C22C14/00 , F01D5/147 , F01D5/286 , F05D2220/36 , F05D2230/22 , F05D2230/31 , Y02P10/295
摘要: A method of forming an airfoil includes the steps of depositing material to form an airfoil in a first layer, and then depositing material in a second layer on the first layer. The first and second layers have distinct densities. An airfoil is also disclosed. The method provides powerful design advantages.
摘要翻译: 形成翼型的方法包括以下步骤:在第一层中沉积材料以形成翼型,然后在第一层上的第二层中沉积材料。 第一层和第二层具有不同的密度。 还公开了一种翼型件。 该方法提供了强大的设计优势。
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公开(公告)号:US07762768B2
公开(公告)日:2010-07-27
申请号:US11598450
申请日:2006-11-13
IPC分类号: F01D9/00
CPC分类号: F01D25/246 , F05D2230/642 , F05D2260/30 , F05D2300/143 , F05D2300/21 , F05D2300/2283
摘要: An assembly for mounting a ceramic turbine vane ring onto a turbine support casing comprises a first metal clamping ring and a second metal clamping ring. The first metal clamping ring is configured to engage with a first side of a tab member of the ceramic turbine vane ring. The second metal clamping ring is configured to engage with a second side of the tab member such that the tab member is disposed between the first and second metal clamping rings.
摘要翻译: 用于将陶瓷涡轮叶片环安装到涡轮机支撑壳体上的组件包括第一金属夹紧环和第二金属夹紧环。 第一金属夹紧环构造成与陶瓷涡轮叶片环的突片构件的第一侧接合。 第二金属夹紧环构造成与突片构件的第二侧接合,使得突片构件设置在第一和第二金属夹紧环之间。
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