journal article·2020-09

Assessment of contact-induced damage mechanisms in thick-walled composite cylinders

Ruben AJ Weerts, Olivier Cousigné, Klaas Kunze, Marc GD Geers, Joris JC Remmers

Publisher page

Abstract

In order to unravel the damage mechanisms occurring in composite-overwrapped pressure vessels (COPVs) subjected to crash conditions, a combined experimental-numerical study has been performed. For the purpose of generality and simplicity, quasi-static contacts on filament-wound cylinders are considered in this paper, as a precursor for geometrically complex impacts on COPVs. Rings with different wall thicknesses are tested to assess how failure mechanisms change when transitioning from thin-wall to thick-wall cylinders. The experimental results are used to identify, which mechanisms occur, and the numerical model is subsequently exploited to analyze the corresponding mechanisms. Based on the understanding of the mechanisms, a method to improve the damage tolerance of thick cylinders is presented. The rings are locally pre-delaminated during manufacturing to promote the growth of these pre-delaminations instead of the initiation of fiber failure.
Source: crossref · Quality: baseline

Research context

OpenAlex topics: Mechanical Behavior of Composites · Mechanical stress and fatigue analysis · Structural Analysis of Composite Materials

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

Affiliations

Department of Mechanical Engineering, Mechanics of Materials, Eindhoven University of Technology, Eindhoven, The Netherlands

Department of HydrogenSupply, BMW AG, Munich, Germany

References (28)

Show source-provided references
1. 10.1039/C8EE01157E10.1039/C8EE01157E ↗
2. Blanc-Vannet P, Bardoux O, Alexandre N, et al. Residual performance of composite pressure vessels submitted to mechanical impacts. In proceedings of the 7th international Conference on Hydrogen Safety (CHS2017) , Hamburg, Germany, September 2017.
3. Szoucsek K and Steinhauser M. Hochdruckgasbehälter für ein Kraftfahrzeug sowie Kraftfahrzeug mit mindestens einem Hochdruckgasbehälter. Patent application DE 10 2015 212 979 A1, Germany, 2016.
4. Szoucsek K Kryogen betankbarer Hochdruckgasbehälter. Patent application DE 10 2015 212 979 A1, Germany, 2016.
5. 10.1016/j.compositesb.2014.10.03010.1016/j.compositesb.2014.10.030 ↗
6. Matheis R, Murnisya H and Johansson T. Modelling of thick UD composites for type IV pressure vessels. In proceedings of the 10th European LS-Dyna Conference , Würzburg, Germany, June 2015.
7. Ribeiro ML · Int J Vehicle Struct Syst · 2012 · 4 · 118
8. 10.1016/j.compositesb.2015.01.00410.1016/j.compositesb.2015.01.004 ↗
9. 10.1016/j.compositesa.2011.10.00410.1016/j.compositesa.2011.10.004 ↗
10. 10.1016/j.camss.2017.09.00110.1016/j.camss.2017.09.001 ↗
11. 10.1177/002199830504873310.1177/0021998305048733 ↗
12. Kreculj D · Tech Gazette · 2013 · 20 · 485
13. 10.1016/S1359-835X(01)00073-210.1016/S1359-835X(01)00073-2 ↗
14. 10.1016/j.compstruct.2016.12.03010.1016/j.compstruct.2016.12.030 ↗
15. 10.1016/j.compositesb.2015.01.01010.1016/j.compositesb.2015.01.010 ↗
16. 10.1016/j.ijimpeng.2016.07.00110.1016/j.ijimpeng.2016.07.001 ↗
17. 10.1016/j.proeng.2017.09.74510.1016/j.proeng.2017.09.745 ↗
18. Lasn K · IOP Conf Ser Mater Sci Eng · 2016 · 139
19. 10.1016/j.compstruct.2015.04.01310.1016/j.compstruct.2015.04.013 ↗
20. Kim EH, Lee I and Hwang TK. Impact response and damage analysis of composite overwrapped pressure vessels. In: 52nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference , Denver, Colorado, 2011. USA: American Institute of Aeronautics and Astronautics.10.2514/6.2011-1863 ↗
21. 10.1016/j.compstruct.2015.03.02710.1016/j.compstruct.2015.03.027 ↗
22. 10.1016/j.compstruct.2016.03.06010.1016/j.compstruct.2016.03.060 ↗
23. Schweizerhof K, Walz M, Rust W, et al. Quasi-static structural analysis with LS-DYNA – merits and limits. In proceedings of the 2nd European LS-Dyna Conference , Gothenburg, Sweden, July 1999. Linköping, Sweden: Engineering Research AB.
24. Im JM, Shin KB and Hwang TK. Evaluation of mode I, II interlaminar fracture toughness for a filament wound carbon/epoxy composite under low and high temperature. In: 16th European Conference on Composite Materials , Seville, Spain, January 2014.
25. 10.1016/j.proeng.2015.12.17110.1016/j.proeng.2015.12.171 ↗
26. 10.1016/j.ijsolstr.2014.03.03810.1016/j.ijsolstr.2014.03.038 ↗
27. ASTM D5528. Standard test method for mode I interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites. West Conshohocken, PA: ASTM International, 2013.
28. ASTM D7905. Standard test method for determination of the mode II interlaminar fracture toughness of unidirectional fiber-reinforced polymer matrix composites. West Conshohocken, PA: ASTM International, 2014.