本研究的目的是建立一种用来预测纤维缠绕复合材料压力容器封头厚度的方法.针对固化成型的复合材料压力容器封头型面,基于封头段所有缠绕纱带总体积保持不变条件,提出了一种采用三次样条函数来预测复合材料压力容器封头厚度的方法.采用该方法对具有不同几何尺寸、不同缠绕工艺参数的复合材料压力容器进行了封头厚度预测,并与传统预测方法及实际厚度测量值作了对比分析.算例结果表明,该方法能够比传统方法更准确地预测纤维缠绕复合材料压力容器的封头厚度,从而为有限元建模分析提供精确的厚度参数.
参考文献
[1] | 沈军,谢怀勤,侯涤洋.纤维缠绕聚合物基复合材料压力容器的可靠性设计[J].复合材料学报,2006,23(4):124-128.Shen Jun,Xie Huaiqin,Hou Diyang.Reliability design of fiber wound reinforced plastics pressure vessel[J].Acta Materiae Compositae Sinica,2006,23(4):124-128. |
[2] | 边文凤,贾宝贤,杜善义.伪弹性合金内衬复合材料压力容器的强度分析[J].复合材料学报,2009,26(1):146-149.Bian Wenfeng,Jia Baoxian,Du Shanyi.Analysis on the strength of composite pressure vessels with pseudo-elastic inner alloy lining[J].Acta Materiae Compositae Sinica,2009,26(1):146-149. |
[3] | Harold D B,Dennis D D,William L R.Composite overwrapped pressure vessels,NASA/TP 2002-210769[R].Washington:NASA,2002:1-270. |
[4] | Aziz Onder,Onur Sayman,Tolga Dogan,Necmettin Tarakcioglu.Burst failure load of composite pressure vessels[J].Composite Structures,2009,89(1):159-166. |
[5] | Craig Clauss.Design,qualification,and thermal testing of a specialized composite overwrap pressure vessel(COPV),AIAA 2007-5558[R].Cincinnati:AIAA,2007:1-10. |
[6] | Eric M C.Design and test of a lightweight pressure vessel,AIAA 2007-2622[R].Williamsburg:AIAA,2007:1-9. |
[7] | James B C.Development of COPV-related standards,AIAA2007-2146[R].Honolulu:AIAA,2007:1-17. |
[8] | Pappu L N,Murthy S L.Designing of a fleet-leader program for carbon composite overwrapped pressure vessels,AIAA2009-2517[R].California:AIAA,2009:1-14. |
[9] | David L G,Daniel J M.Finite element analysis of a composite overwrapped pressure vessel,AIAA 2004-3506[R].Florida:AIAA,2004:1-15. |
[10] | Park J S,Hong C S,Kim C G.Analysis of filament wound composite structures considering the change of winding angles through the thickness direction[J].Composite Structures,2002,55(1):63-71. |
[11] | Hartung R F.Planar-wound filamentary pressure vessel[J].AIAA Journal,1963,12(1):2842-2844. |
[12] | Knoell A C.Structural design and stress analysis program for advanced composite filament wound axisymmetric pressure vessel(CLMTRANK),JPL Technical Report 32-1521[R].California:NASA,1971:1-32. |
[13] | 眉山(译).纤维缠绕压力容器的圆顶厚度[J].导弹与航天运载技术,1991(3):66-75.Mei Shan(Translate).Dome thickness of filament winding composite pressure vessels[J].Missiles and Space Vehicles,1991(3):66-75. |
[14] | Gramll K C,Namiki F,Onoda J.Dome thickness of filament wound pressure vessels[J].Trans Japan Soc Aerospace Sci,1990,100(33):66-79. |
[15] | Alexei A K.Refined thickness of filament wound shells[J].Science and Engineering of Composite Materials,2002,10(4):241-248. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%