Gas turbine engine flow path member
作者： Okey Kwon , Jeffrey F. Rhodes
DOI:
关键词: Engineering 、 Path (graph theory) 、 Cooling fluid 、 Flow (mathematics) 、 Gas turbines 、 Mechanical engineering 、 Engineering drawing 、 Turbine
摘要: A gas turbine engine flow path member is disclosed which includes an extending end portion capable of contacting a surface the engine. The openings to pass cooling fluid cool portion. member, furthermore, can be made using variety approaches. To set forth just two non-limiting examples, cast and it laminated construction.
lens.org 参考文章(26)
George Liang, Turbine blade with TBC removed from blade tip region ,(2006)
Ching-Pang Lee, Turbine blade squealer tip peripheral end wall with cooling passage arrangement ,(1992)
Robert F. Manning, Victor H. S. Correia, Cool tip blade ,(1999)
Andrew Narcus, James Downs, Turbine blade tip cooling construction ,(2002)
Satoshi Hada, Taku Ichiryu, Turbine blade and gas turbine ,(2002)
Daniel Edward Demers, Richard Ludwig Schmidt, Philip Francis Stec, Turbine blade with recessed squealer tip and shelf ,(2003)
George Liang, Multi-metered film cooled blade tip ,(2003)
Paul Hadley Vitt, Kevin Samuel Klasing, Brian David Keith, Ching-Pang Lee, Fluted tip turbine blade ,(2005)
Ronald Scott Bunker, Turbine blade tip with offset squealer ,(1999)
Kenichiro Takeishi, Masaaki Matsuura, Ryoma Nogami, Tsuyoshi Kitamura, Turbine cooling vane of gas turbine engine ,(2004)