发明授权
- 专利标题: Integrated bridge turbine blade
- 专利标题(中): 集成桥式涡轮叶片
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申请号: US10616023申请日: 2003-07-09
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公开(公告)号: US06832889B1公开(公告)日: 2004-12-21
- 发明人: Ching-Pang Lee , Richard Clay Haubert , Harvey Michael Maclin
- 申请人: Ching-Pang Lee , Richard Clay Haubert , Harvey Michael Maclin
- 主分类号: F03D1100
- IPC分类号: F03D1100
摘要:
A turbine blade includes a hollow airfoil integrally joined to a dovetail. The airfoil includes a perforate first bridge defining a flow channel behind the airfoil leading edge. A second bridge is spaced behind the first bridge and extends from a pressure sidewall of the airfoil short of the airfoil trailing edge. A third bridge has opposite ends joined to the pressure sidewall and the second bridge to define with the first bridge a supply channel for the leading edge channel, and defines with the second bridge a louver channel extending aft along the second bridge to its distal end at the pressure sidewall.
公开/授权文献
- US20050008487A1 INTEGRATED BRIDGE TURBINE BLADE 公开/授权日:2005-01-13
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