Shear behaviors and failure mechanisms of 2D C/SiC pins prepared by chemical vapor infiltration
Source abstract
Abstract
Abstract Connecting and fastening large-scale all-C/SiC airfoils to the fuselage of hypersonic vehicle requires C/SiC fasteners of high-performances under the re-entry environment. In this paper, 2D C/SiC pins prepared by chemical vapor infiltration (CVI) were sheared off to demonstrate their strength sensitivity to the nonuniform microstructures, such as porosity and ply orientation. Results showed that their average shear strengths increase linearly from 85.8 to 134.8 MPa as their average total porosity decreases from 23.2% to 14.5%. The shear strengths of 2D C/SiC pins are almost the same as the in-plane shear strengths of 2D C/SiC composites, under the condition that both have identical total porosity. In contrast, the variances of the pin shear strength are much higher than the in-plane shear strength, which is mainly ascribe to the effects of the loading angle between the shear plane and the ply orientation. The porosity of the 2D C/SiC pin is the main microstructural factor influencing the pin shear strength. Matrix shear cracking, debonding between matrix and fibers, crack deflection along fibers and interlayer sliding are the main shear failure mechanisms. Due to the secondary bending deformation, the interlayer sliding and the corresponding fiber pull-out mechanisms dominate the final ductile fracture behavior.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Advanced ceramic materials synthesis · Aluminum Alloys Composites Properties · High-Velocity Impact and Material Behavior
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (20)
Show source-provided references
1. CMC thermal protection system for future reusable launch vehicles: generic shingle technological maturation and tests10.1016/j.actaastro.2009.01.035 ↗
2. Challenges in ceramic science: a report from the workshop on emerging research areas in ceramic science10.1111/jace.12033 ↗
3. Materials selection in design of structures and engines of supersonic aircrafts: a review10.1016/j.matdes.2012.10.001 ↗
4. The physics and mechanics of fibre-reinforced brittle matrix composites10.1007/BF00355946 ↗
5. Ceramic matrix composite (CMC) thermal protection systems (TPS) and hot structures for hypersonic vehicles
6. Narottam · 2014
7. Lange · 2006 · 41
8. Pichon · 2006 · 1
9. X-43A hypersonic vehicle Technology development10.1016/j.actaastro.2006.02.021 ↗
10. Mühlratzer · 2008 · 331
11. CMC key technologies - background, status, present and future applications
12. Secure tightening of a CMC fastener for the heat shield of Re-entry vehicles10.1016/j.compstruct.2009.07.002 ↗
13. Miller · 1998 · 2444
14. Preparation and properties of C/SiC bolts via precursor infiltration and pyrolysis process10.1007/s12598-011-0349-z ↗
15. Preparation and mechanical properties of C/SiC nuts and bolts10.1016/j.msea.2012.03.045 ↗
16. Effects of porosity on in-plane and interlaminar shear strengths of two-dimensional carbon fiber reinforced silicon carbide composites10.1016/j.matdes.2016.03.017 ↗
17. Effects of z-pin's porosity on shear properties of 2D C/SiC z-pinned joint10.1016/j.compstruct.2017.04.013 ↗
18. Effect of PyC interphase thickness on mechanical behaviors of SiBC matrix modified C/SiC composites fabricated by reactive melt infiltration10.1016/j.carbon.2014.05.092 ↗
19. Mechanical and electromagnetic shielding properties of carbon fiber reinforced silicon carbide matrix composites10.1016/j.carbon.2015.08.011 ↗
20. Mechanisms of deformation and failure in carbon-matrix composites subject to tensile and shear loading10.1111/j.1151-2916.1995.tb08897.x ↗