Abstract

All-aluminium cylinders are used for on-board storage of compressed natural gas in vehicles. Besides being subjected to the maximum fill pressure, these cylinders are subjected to fluctuating pressures, due to refuelling operations. In order to establish a relevant test method to ensure leak before break failure performance, elasto-plastic finite element stress analysis of the design containing various defects was carried out to obtain a theoretical basis for the establishment of the test method. Axial semi-elliptical cracks in the central portion of the cylinder and circumferential cracks in the bottom of the cylinder are modelled using 20-node hexahedron elements. Not only the cylindrical body but also the neck and transition areas of the cylinder are considered in the modelling. Slender cracks with lengths approximately five times the wall thickness of the cylinder, which often appear in applied all-aluminium gas cylinders, are considered. Crack depths varied from 22.5% to 100% of the wall thickness. Through discussions about the calculated J-integral and crack mouth opening displacement (CMOD) of the axial and circumferential cracks, the effects of the different cracks on all-aluminium cylinders in the elasto-plastic deformation state are made clear. The analyses show that under the elasto-plastic deformation state, axial cracks in the centre of the cylinder are more dangerous for the cylinder than circumferential cracks in the bottom of the cylinder, if these are of the same size and under the same conditions. The axial external crack is found to be most severe among these different crack types. Finally, the CMOD of cylinders with an axial external crack have been measured by the experimental method and a good agreement between the calculated CMOD and the tested CMOD was reached.

Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call