Full Text:
<3166>
CLC number: TH/C3778
On-line Access:
Received: 2008-04-08
Revision Accepted: 2008-08-10
Crosschecked: 2008-12-29
Cited: 3
Clicked: 6348
Mechanical analysis and reasonable design for Ti-Al alloy liner wound with carbon fiber resin composite high pressure vessel
| |||||||||||||
Chuan-xiang ZHENG, Fan YANG, Ai-shi ZHU. Mechanical analysis and reasonable design for Ti-Al alloy liner wound with carbon fiber resin composite high pressure vessel[J]. Journal of Zhejiang University Science A, 2009, 10(3): 384-391.
@article{title="Mechanical analysis and reasonable design for Ti-Al alloy liner wound with carbon fiber resin composite high pressure vessel",
author="Chuan-xiang ZHENG, Fan YANG, Ai-shi ZHU",
journal="Journal of Zhejiang University Science A",
volume="10",
number="3",
pages="384-391",
year="2009",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A0820025"
}
%0 Journal Article
%T Mechanical analysis and reasonable design for Ti-Al alloy liner wound with carbon fiber resin composite high pressure vessel
%A Chuan-xiang ZHENG
%A Fan YANG
%A Ai-shi ZHU
%J Journal of Zhejiang University SCIENCE A
%V 10
%N 3
%P 384-391
%@ 1673-565X
%D 2009
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A0820025
TY - JOUR
T1 - Mechanical analysis and reasonable design for Ti-Al alloy liner wound with carbon fiber resin composite high pressure vessel
A1 - Chuan-xiang ZHENG
A1 - Fan YANG
A1 - Ai-shi ZHU
J0 - Journal of Zhejiang University Science A
VL - 10
IS - 3
SP - 384
EP - 391
%@ 1673-565X
Y1 - 2009
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A0820025
Abstract: To consider the internal pressure loaded by both the cylindrical Ti-Al alloy liner and the carbon fiber resin composite (CFRC) wound layers, two models are built. The first one is a cylinder loaded with the internal pressure in the hoop direction only. In this model, the total hoop direction load is distributed over all layers under the internal pressure. The second one is a cylinder loaded with the internal pressure in the axial direction only. In this model, the total axial load is distributed over all cylinders under the internal pressure. Taking the boundary conditions of the continuous displacement between layers into account, a group of equations are built. From these equations, we get the solutions of stresses in both hoop direction and axial direction loaded by every layer under internal pressures. After the stresses are obtained, a reasonable design can be done. An example is given in the final section of this study.
[1] Agarwal, B.D., Broutman, L.J., 1990. Analysis and Performance of Fiber Composites (2nd Ed.). John Wiley & Sons, Inc., New York.
[2] Bi, H.Z., 2006. Carbon fiber and their application in aeronautic field. Hi-Tech Fiber & Application, 3:43-45 (in Chinese).
[3] Braun, C.A., 1992. Manufacturing process controls for high reliability carbon filament-wound seamless aluminum lined composite pressure vessel. AIAA, 92:3609.
[4] Chen, H.H., Deng, H.J., Li, M., Lin, X.S., 1997. Modern Composite Materials. China Logistics Publishing House, Beijing, China (in Chinese).
[5] Messager, T., Pyrz, M., Gineste, B., Chauchot, P., 2002. Optimal laminations of thin underwater composite cylindrical vessels. Composite Structures, 58(4):529-537.
[6] Parnas, L., Nuran, K., 2002. Design of fiber-reinforced composite pressure vessels under various loading conditions. Composite Structure, 58:83-95.
[7] Paul, H.Z., Timothy, J.F., 2003. Fiber reinforced vessel design with a damage criterion approach. Composite Structure, 4:395-411.
[8] Perreux, D., Lazuardi, D., 2001. The effects of residual stress on the non-linear behaviour of composite laminates. Part II. Layer, laminate non-linear models and the effect of residual stress on the model parameters. Composite Science and Technology, 61(2):177-190.
[9] Smerdov, A., 2000. A computational study in optimum formulations of optimization problems on laminated cylindrical shells for buckling: I. Shells under axial compression. Composite Science and Technology, 60(11):2057-2066.
[10] Verijenko, V.E., Adali, S., Tabakov, P.Y., 2001. Stress distribution in continuously heterogeneous thick laminated pressure vessels. Composite Structures, 54(2-3):371-377.
[11] Wild, P.M., Vickers, G.W., 1997. Analysis of resin composite-wound cylindrical shells loaded by combined centrifugal, pressure and axial loading. Composites Part A Applied Science and Manufacturing, 28(1):47-55.
[12] Wu, Y.C., Hu, J., Li, P., 2003. Stress analysis of metal lined fiber reinforced composite material pressure vessel. Chemical Equipment Technology, 5:46-49.
[13] Xia, M., Takayanagi, H., Kemmochi, K., 2001. Analysis of multi-layered resin composite-wound composite pipes loaded by internal pressure. Composite Structures, 53(4):483-491.
[14] Zheng, C.X., Cao, K., 2005. Light Weight Resin Composite Aluminum Liner High Pressure Vessel. Chinese Patent No.03150968.1.
[15] Zheng, C.X., 2006a. Composite Material Pressure Vessel. Chemical Industry Press, Beijing, China (in Chinese).
[16] Zheng, C.X., 2006b. Research of reasonable winding angle of ribbons of flat steel ribbon wound pressure vessel. Journal of Zhejiang University SCIENCE A, 7(3):445-449.
[17] Zheng, J.Y., Liu, F.J., 2006. High-pressure Storage Vessels Used in Hydrogen Refueling Station. American Society of Mechanical Engineers, Pressure Vessels and Piping Division (Publication) PVP. Proceedings of 2006 ASME Pressure Vessels and Piping Division Conference Pressure Vessel Technologies for the Global Community, p.7-11.
[18] Zhou, L., Fan, F.Q., 2001. Mechanics of Composite Materials. Higher Education Press, Beijing, China (in Chinese).
Open peer comments: Debate/Discuss/Question/Opinion
<1>