4.7 Article

Following the effect of braid architecture on performance and damage of carbon fibre/epoxy composite tubes during torsional straining

Journal

COMPOSITES SCIENCE AND TECHNOLOGY
Volume 200, Issue -, Pages -

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compscitech.2020.108451

Keywords

Textile composites; Kinking; Damage mechanics; X-ray computed tomography; Braiding

Funding

  1. Engineering and Physical Science Research Council (EPSRC) [EP/F007906/1, EP/F001452/1, EP/I02249X, EP/M010619/1, EP/F028431/1, EP/M022498/1, EP/R00661X]
  2. EPSRC Future Composites Manufacturing Hub [EP/P006701/1]
  3. European Research Council [695638]
  4. EPSRC [EP/F007906/1, EP/M010619/1, EP/P006701/1, EP/F001452/1, EP/M022498/1, EP/I02249X/1, EP/F028431/1] Funding Source: UKRI

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The torsional performance of bi-axially braided carbon fibre reinforced polymer (CFRP) tubes as a function of braid architecture is investigated. It is found that for a given braid pattern, the 45 degrees braided CFRP tubes have higher shear moduli and lower shear strength than the 35 degrees braids. In general, 2/2 (regular) braided CFRP tubes exhibit both higher shear strength and higher shear modulus than 1/1 (diamond) braids. However, beyond the peak load, the shear strength of 2/2 braided CFRPs exhibits sudden and steep drops, resulting in a lower remnant shear strength than 1/1 structures after the shear strain exceeds 4.5%. Moreover, the damage evolution is monitored in-situ by synchrotron X-ray computed tomography during torsional straining. It shows that for a 2/2 structure, inter-tow debonded regions are vertically interconnected allowing rapid crack propagation and strength drops, whereas for the 1/1 braid they are distributed in a chequer board pattern causing a more gradual loss of strength. The fibre/matrix interfacial strength and tow cross-over density play key roles in the torsional failure of 1/1 and 2/2 braided CFRP tubes, as the former controls damage initiation and the latter controls damage propagation.

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