Apparatus and method for cooling airfoil tip for turbine engine

作者: Feldmann Kevin Robert , Hoffman James Michael , Dooley Weston Nolan , Groves Ii Robert Charles

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摘要: The application provides an apparatus and method for cooling airfoil tip a turbine engine, which can include airfoil, such as cooled blade, having rail extending beyond tipwall enclosing interior the at tip. A plurality of holes be provided in rail. flow fluid through from to cool airfoil.

参考文章(11)
David A. Kemp, Ching-Pang Lee, Paul H. Vitt, John J. Marra, Cooled airfoil in a turbine engine ,(2012)
Campbell Christian X, TURBINE BLADE TIP ,(2012)
Haiping Wang, Xiuzhang James Zhang, James William Vehr, Rotor blade cooling flow ,(2014)
Ralph Warren Mathews, George Liang, Cooling of turbine blade suction tip rail ,(2006)
Craig Miller Kuhne, Joseph Steven Bubnick, Alisha Vachhani, Recovery tip turbine blade ,(2009)
Michael J. Kline, Anthony Louis Giglio, Camilo Andres Sampayo, Turbine Blade Tip With Tip Shelf Diffuser Holes ,(2012)
Benjamin Paul Lacy, Anthony Louis Giglio, Bucket assembly for turbine system and corresponding turbine system ,(2012)
Zhou Chao, Wang Lei, Zhong Fangpan, Adopt leaf top rib wing structure's turbine blade ,(2016)