Clocking can produce benefit has become a common viewpoint in turbomachinery field. However, there still is a question, that is “why the benefit of two-dimensional (2D) clocking model is always larger than that of three-dimensional (3D) clocking model?”. A general way of maximizing 3D clocking benefit by edge matching (EM) is put forward. On the basis of experience and knowledge accumulated in investigations on clocking effects, a further simplified method is presented and emphasized. Aachen 1.5 stage low speed subsonic axial turbine is used as an example of maximizing 3D clocking benefits by applying EM. Results show that 3D clocking benefit can be maximized by routinely using EM with relatively low computational resource requirements, and the benefit is considerable enough to be paid more attention.
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ASME Turbo Expo 2007: Power for Land, Sea, and Air
May 14–17, 2007
Montreal, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
0-7918-4795-0
PROCEEDINGS PAPER
Maximizing 3D Clocking Effect by the Guidance of Edge Matching
LuCheng Ji,
LuCheng Ji
Chinese Academy of Sciences, Beijing, China
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Jiang Chen,
Jiang Chen
Beijing University of Aeronautics and Astronautics, Beijing, China
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Zhao Yan,
Zhao Yan
China Aerospace Science and Industry Corporation, Beijing, China
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WeiLin Yi
WeiLin Yi
Chinese Academy of Sciences, Beijing, China
Search for other works by this author on:
LuCheng Ji
Chinese Academy of Sciences, Beijing, China
Jiang Chen
Beijing University of Aeronautics and Astronautics, Beijing, China
Zhao Yan
China Aerospace Science and Industry Corporation, Beijing, China
WeiLin Yi
Chinese Academy of Sciences, Beijing, China
Paper No:
GT2007-27619, pp. 1725-1731; 7 pages
Published Online:
March 10, 2009
Citation
Ji, L, Chen, J, Yan, Z, & Yi, W. "Maximizing 3D Clocking Effect by the Guidance of Edge Matching." Proceedings of the ASME Turbo Expo 2007: Power for Land, Sea, and Air. Volume 6: Turbo Expo 2007, Parts A and B. Montreal, Canada. May 14–17, 2007. pp. 1725-1731. ASME. https://doi.org/10.1115/GT2007-27619
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