Fatigue Characterization of a Melt-Infiltrated Woven HI-NIC-S/BN/SIC Ceramic Matrix Composite (CMC) Using a Unique Combustion Test Facility

2009 ◽  
pp. 103-115 ◽  
Author(s):  
Ted T. Kim ◽  
Shankar Mall ◽  
Larry P. Zawada
Keyword(s):  
Matrix Composite ◽  
Ceramic Matrix Composite ◽  
Ceramic Matrix ◽  
Test Facility ◽  
Sic Ceramic

scholarly journals Sustainable Machining of Cf/SiC Ceramic Matrix Composite Using Green Cutting Fluids

Procedia CIRP ◽  
2021 ◽  
Vol 98 ◽  
pp. 151-156
Author(s):  
Shyam ◽  
M. Shanmuka Srinivas ◽  
Kishor Kumar Gajrani ◽  
A. Udayakumar ◽  
M. Ravi Sankar
Keyword(s):  
Matrix Composite ◽  
Ceramic Matrix Composite ◽  
Ceramic Matrix ◽  
Cutting Fluids ◽  
Sustainable Machining ◽  
Sic Ceramic

Synthesis and characterization of diopside glass–ceramic matrix composite reinforced with aluminum titanate

2009 ◽  
Vol 35 (4) ◽  
pp. 1447-1452 ◽  
Author(s):  
M. Yousefi ◽  
P. Alizadeh ◽  
B. Eftekhari Yekta ◽  
F. Molaie ◽  
N. Ghafoorian ◽  
...  
Keyword(s):  
Matrix Composite ◽  
Glass Ceramic ◽  
Ceramic Matrix Composite ◽  
Ceramic Matrix ◽  
Synthesis And Characterization ◽  
Aluminum Titanate

Combustion Test Results of an Uncooled Combustor With Ceramic Matrix Composite Liner

2001 ◽  
Author(s):  
Yasufumi Suzuki ◽  
Toyoichi Satoh ◽  
Manabu Kawano ◽  
Naofumi Akikawa ◽  
Yoshihiro Matsuda
Keyword(s):  
Matrix Composite ◽  
Reverse Flow ◽  
Ceramic Matrix Composite ◽  
Three Dimensional ◽  
Ceramic Matrix ◽  
High Heat ◽  
Combustion Efficiency ◽  
Test Facility ◽  
Annular Combustor ◽  
Release Ratio

A reverse-flow annular combustor with its casing diameter of 400 mm was developed using an uncooled liner made of three-dimensional-woven ceramic-matrix composite. The combustor was tested using the TRDI high-pressure combustor test facility at the combustor maximum inlet and exit temperature of 723K and 1623K respectively. Although both the material and combustion characteristics were evaluated in the test, this report focused on the combustion performance. As the results of the test, the high combustion efficiency and high heat release ratio of 99.9% and 1032 W/m3/Pa were obtained at the design point. The latter figure is approximately twice as high as that of existing reverse–flow annular combustors. Pattern factor was sufficiently low and was less than 0.1. Surface temperatures of the liner wall were confirmed to be higher than the limit of the combustor made of existing heat-resistant metallic materials.

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