Recovery tip turbine blade

作者: Craig Miller Kuhne , Joseph Steven Bubnick , Alisha Vachhani

DOI:

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摘要: A turbine blade includes an airfoil having first and second tip ribs extending along the opposite pressure suction sides thereof. baffle bifurcates into two pockets, with a pocket being laterally open at its aft end to recover leakage flow, closed.

参考文章(36)
Ching-Pang Lee, Tapered tip turbine blade ,(1998)
Robert F. Manning, Victor H. S. Correia, Cool tip blade ,(1999)
Robert J. Corsmeier, Richard H. Andersen, William A. Litzinger, Tip cap apparatus and method of installation ,(1976)
Richard H. Andersen, Tip cooling for turbine blades ,(1977)
Hiroki Fukuno, Yasuoki Tomita, Kazuo Uematsu, Kiyoshi Suenaga, Masaaki Matsuura, Sunao Aoki, Gas turbine blade ,(1998)
Nicholas Charles Palmer, Eugene Thomas Vaughn, Ching Pang Lee, Diffusion-cooled blade tip cap ,(1988)
Thomas A. Auxier, Kenneth B. Hall, Robert J. Mcclelland, Cooled blades for a gas turbine engine ,(1990)
Arthur G. Corfe, Brian G. Cooper, David Stroud, Jonathan P. W. Towill, Film cooled components ,(1989)