发明授权
- 专利标题: Compound cooling flow turbulator for turbine component
- 专利标题(中): 用于涡轮机部件的复合式冷却流动紊流器
-
申请号: US12884464申请日: 2010-09-17
-
公开(公告)号: US08894367B2公开(公告)日: 2014-11-25
- 发明人: Ching-Pang Lee , Nan Jiang , John J. Marra , Ronald J. Rudolph
- 申请人: Ching-Pang Lee , Nan Jiang , John J. Marra , Ronald J. Rudolph
- 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: F01D5/18
- IPC分类号: F01D5/18
摘要:
Multi-scale turbulation features, including first turbulators (46, 48) on a cooling surface (44), and smaller turbulators (52, 54, 58, 62) on the first turbulators. The first turbulators may be formed between larger turbulators (50). The first turbulators may be alternating ridges (46) and valleys (48). The smaller turbulators may be concave surface features such as dimples (62) and grooves (54), and/or convex surface features such as bumps (58) and smaller ridges (52). An embodiment with convex turbulators (52, 58) in the valleys (48) and concave turbulators (54, 62) on the ridges (46) increases the cooling surface area, reduces boundary layer separation, avoids coolant shadowing and stagnation, and reduces component mass.
公开/授权文献
- US20110033312A1 COMPOUND COOLING FLOW TURBULATOR FOR TURBINE COMPONENT 公开/授权日:2011-02-10
信息查询