Optimizing the fiber push‐out method to evaluate interfacial failure in SiC/BN/SiC ceramic matrix composites

نویسندگان

چکیده

The investigation of several parameters during fiber push-out micromechanical tests on the interfacial shear strength (ISS) BN interphase in SiCf/SiC ceramic matrix composites (CMC) was undertaken to optimize experimental work. composites—candidate materials for jet engine components—were manufactured with varying types and interlayer thicknesses. Experimental explored included analyzing effect sample thickness success rate tests, local environment whether at tow-level (intra-tow variability ISS) or CMC architecture-level (inter-tow variability), nanoindenter flat-punch tip size, itself. Over 1000 push-outs were performed analyzed this work—with data presented as cumulative distribution functions compare contrast samples. It found that ISS measured strongly statistically influenced by underlying roughness (interphase adherence), well its (e.g., number nearest neighbors) only if itself surpassed a threshold 200 nm. Finally thinner interphases, limited value added high there no from any environment.

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Matrix cracking of fiber-reinforced ceramic composites in shear

The mechanics of cracking in fiber-reinforced ceramic matrix composites (CMCs) under general loadings remains incomplete. The present paper addresses one outstanding aspect of this problem: the development of matrix cracks in unidirectional plies under shear loading. To this end, we develop a model based on potential energy differences upstream and downstream of a fully bridged steady-state mat...

متن کامل

Criteria for Progressive Interfacial Debonding with Friction in Fiber-reinforced Ceramic Composites

Criteria for progressive debonding at the fiber/mattix interface with friction along the debonded interface are considered for fiber-reinfoxed ceramic composites. The energy-based criterion is adopted to analyze the debond length, the crack-opening displacement, and the displacement of the composite due to interfacial debonding. The analytical solutions are identical to those obtained from the ...

متن کامل

Interfaces and interfacial mechanics : influence on the mechanical behavior of ceramic matrix composites (CMC)

The influence of fiberlmatrix interactions on the mechanical behavior of ceramic matrix composites is examined on glass matrix composites and mainly on composites made by chemical vapor infiltration (CVI) of a fiber preform by a SiC matrix. Then the relationships between interfaces and features of the stress-strain behavior are highlighted on microcomposite specimens using experimental data and...

متن کامل

Ultrasonic Characterization of the Fiber-Matrix Interfacial Bond in Aerospace Composites

The properties of advanced composites rely on the quality of the fiber-matrix bonding. Service-induced damage results in deterioration of bonding quality, seriously compromising the load-bearing capacity of the structure. While traditional methods to assess bonding are destructive, herein a nondestructive methodology based on shear wave reflection is numerically investigated. Reflection relies ...

متن کامل

Anomaly Detection and Microstructure Characterization in Fiber Reinforced Ceramic Matrix Composites

ANOMALY DETECTION AND MICROSTRUCTURE CHARACTERIZATION IN FIBER REINFORCED CERAMIC MATRIX COMPOSITES Name: Bricker, Stephen E. University of Dayton Advisor: Dr. Russell Hardie Ceramic matrix composites (CMCs) have the potential to replace current superalloys being used in hot components of jet engines. CMCs with continuous fiber reinforcement exhibit significant strength retention beyond tempera...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Journal of the American Ceramic Society

سال: 2021

ISSN: ['0002-7820', '1551-2916']

DOI: https://doi.org/10.1111/jace.17673