A predictive modeling tool for damage analysis and design of hydrogen storage composite pressure vessels

Author(s):  
Ba Nghiep Nguyen ◽  
Hee Seok Roh ◽  
Daniel R. Merkel ◽  
Kevin L. Simmons
2010 ◽  
Author(s):  
William C. Fort, III ◽  
Richard A. Kallman ◽  
Miguel Maes ◽  
Edward G. Skolnik ◽  
Steven C. Weiner

2021 ◽  
Vol 255 ◽  
pp. 113046
Author(s):  
Song Lin ◽  
Liuqing Yang ◽  
Hui Xu ◽  
Xiaolong Jia ◽  
Xiaoping Yang ◽  
...  

Author(s):  
Elias Ledesma ◽  
Salvador M. Aceves ◽  
Francisco Espinoza-Loza ◽  
Bahram Ravani

This work presents the development of a toolkit for the analysis and design of composite pressure vessels. The toolkit is developed in APDL (ANSYS parametric design language) to work inside ANSYS. In addition to the macros in APDL, a graphical user interface is developed in Tk/Tcl to access the toolkit. The toolkit includes a tool for composite material analysis with the method of cells, developed and implemented to get laminae properties from fiber and matrix properties. A shell elements tool and a hexahedral elements tool were implemented to generate 3D type 3 (metal lined) or type 4 (plastic lined) fiber reinforced pressure vessel models. A mixed Tsai-Wu and maximum stress tool was also implemented in the toolkit to predict composite failure. In addition to these tools, there are two scripts to model honeycomb as well as an algorithm to perform a netting analysis.


2017 ◽  
Vol 42 (31) ◽  
pp. 20056-20070 ◽  
Author(s):  
Damien Halm ◽  
Fabien Fouillen ◽  
Eric Lainé ◽  
Mikaël Gueguen ◽  
Denis Bertheau ◽  
...  

2003 ◽  
Author(s):  
E Udd ◽  
M. Kunzler ◽  
S. Calvert ◽  
S. Kreger

2021 ◽  
pp. 002199832110335
Author(s):  
Osman Kartav ◽  
Serkan Kangal ◽  
Kutay Yücetürk ◽  
Metin Tanoğlu ◽  
Engin Aktaş ◽  
...  

In this study, composite overwrapped pressure vessels (COPVs) for high-pressure hydrogen storage were designed, modeled by finite element (FE) method, manufactured by filament winding technique and tested for burst pressure. Aluminum 6061-T6 was selected as a metallic liner material. Epoxy impregnated carbon filaments were overwrapped over the liner with a winding angle of ±14° to obtain fully overwrapped composite reinforced vessels with non-identical front and back dome layers. The COPVs were loaded with increasing internal pressure up to the burst pressure level. During loading, deformation of the vessels was measured locally with strain gauges. The mechanical performances of COPVs designed with various number of helical, hoop and doily layers were investigated by both experimental and numerical methods. In numerical method, FE analysis containing a simple progressive damage model available in ANSYS software package for the composite section was performed. The results revealed that the FE model provides a good correlation as compared to experimental strain results for the developed COPVs. The burst pressure test results showed that integration of doily layers to the filament winding process resulted with an improvement of the COPVs performance.


2018 ◽  
Vol 185 ◽  
pp. 573-583 ◽  
Author(s):  
Roham Rafiee ◽  
Mohammad Ali Torabi

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