Thermally insulated cmc structure with internal cooling
作者： Douglas A. Keller , Gary B. Merrill , Malberto F. Gonzalez
DOI:
关键词:
摘要: An insulated CMC structure (20A) formed of a layer (22A), thermal insulation (24A) applied to front surface (30A) the and cooling channels (28A) along interface (26A) between layer, thus directly thermally critical area interface. Embodiments include in direct contact with both layers (FIG. 1); one tangent other (FIGs. 4, 5 9); an intervening wall (36D, 36E) that bulges into for improved bonding thereof 6, 7); ceramic tubes (38F FIG. 8).
google.fr 参考文章(22)
Steven C. Butner, Jay Edgar Lane, Harry A. Albrecht, Yevgeniy P. Shteyman, Jay A. Morrison, Scott M. Widrig, Gary Brian Merrill, Composite structure formed by cmc-on-insulation process ,(2002)
Daniel G. Thompson, Jay A. Morrison, Steven James Vance, Stacked laminate CMC turbine vane ,(2004)
Steve H. Halfmann, David R. Pack, Craig A. Wilson, Yong W. Kim, Milton Ortiz, Mark C. Morris, High effectiveness cooled turbine vane or blade ,(2001)
Todd Jessen, Channeled ceramic structure and process for making same ,(1996)
Steven C. Butner, Harry A. Albrecht, Jay Morrison, Yevgeuiy Shteyman, Christian X. Campbell, Ceramic matrix composite structure having integral cooling passages and method of manufacture ,(2002)
James L. Hadder, Tube cooled combustor ,(2003)
Robert Edward Schafrik, Ching-Pang Lee, Ramgopal Darolia, Directly cooled thermal barrier coating system ,(2000)
Daniel George Thompson, Jay Edgar Lane, Harry A. Albrecht, Yevgeniy P. Shteyman, Jay A. Morrison, Chris Campbell, Gary Brian Merrill, Ceramic matrix composite gas turbine vane ,(2003)
Milton Ortiz, Kin Poon, Vincent Chung, Thin wall cooling system ,(2001)
James Albert Riedell, Method and system of thermal protection ,(2002)