发明授权
- 专利标题: Turbomachine airfoil mounting assembly
- 专利标题(中): 涡轮机翼型安装组件
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申请号: US540714申请日: 1983-10-13
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公开(公告)号: US4832568A公开(公告)日: 1989-05-23
- 发明人: Robert H. Roth , Bruno G. Lampsat , Jack L. Readnour
- 申请人: Robert H. Roth , Bruno G. Lampsat , Jack L. Readnour
- 申请人地址: OH Cincinnati
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: OH Cincinnati
- 主分类号: F01D9/04
- IPC分类号: F01D9/04
摘要:
An assembly for mounting a plurality of circumferentially spaced and radially extending airfoils. In a preferred embodiment the assembly comprises a plurality of arcuate mounting fairings each including a central boss having at least one radially extending recess disposed in a radially inner surface thereof which contains an elastomeric boot for receiving an end of one of the plurality of airfoils. The mounting fairing further includes integral first and second flanges extending circumferentially outwardly from opposite sides of the boss portion which overlap complementary second and first flanges, respectively, of adjacent mounting fairings. Fastening means connect the first and second flanges of adjacent mounting fairings to form a continuous annular shroud.
公开/授权文献
- US5713030A Thermal management device and method for a computer processor 公开/授权日:1998-01-27
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