发明授权
US08770930B2 Joining mechanism and method for interlocking modular turbine engine component with a split ring
有权
用于将模块化涡轮发动机部件与分离环联动的联接机构和方法
- 专利标题： Joining mechanism and method for interlocking modular turbine engine component with a split ring
- 专利标题（中）： 用于将模块化涡轮发动机部件与分离环联动的联接机构和方法
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申请号： US13023721申请日： 2011-02-09
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公开(公告)号： US08770930B2公开(公告)日： 2014-07-08
- 发明人: Gary B. Merrill , Allister W. James , Iain A. Fraser
- 申请人： Gary B. Merrill , Allister W. James , Iain A. Fraser
- 申请人地址： US FL Orlando US VA Charlottesville
- 专利权人： Siemens Energy, Inc.,Mikro Systems, Inc.
- 当前专利权人： Siemens Energy, Inc.,Mikro Systems, Inc.
- 当前专利权人地址： US FL Orlando US VA Charlottesville
- 主分类号： F01D9/00
- IPC分类号： F01D9/00
摘要：
A modular airfoil assembly (200) and related method for interlocking components of an airfoil structure (210) including a platform (220), an airfoil (210) having a shoulder (230) and a stem (232) extending outward from the shoulder. A ring element (100) positioned against the stem (232) secures the shoulder (230) against the platform (210). First and second members (100a, 100b) of the ring element (100) are bonded together with a portion (128j) of a surface (112a) of the second member (100b) extending within and bonded to a portion (128i) of a surface (112b) of the first member (100a).
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