|Table of Contents|

Comparative analysis on multi-type domes of filament-wound composite pressure vessels(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2020年06期
Page:
90-96
Research Field:
研究与设计
Publishing date:

Info

Title:
Comparative analysis on multi-type domes of filament-wound composite pressure vessels
Author(s):
CAI Qiang; ZHAO Xiaoning; LI Xintian; DAN Linpeng; PU Xiaohang; HUANG Huihui
(China Academy of Launch Vehicle Technology, Beijing 100076, China)
Keywords:
composite material;  pressure vessel;  dome;  grid theory;  geodesic theory
PACS:
V421.4
DOI:
-
Abstract:
Filament-wound Composite Pressure Vessels(FCPV)has been widely used in the aerospace field.The main purpose of this paper is to meet the requirements of rapid concept design of FCPV and compare the effects of winding pattern and meridian type of domes on the properties of FCPV.A simplified geometric parameter model of FCPV was established.Based on the mature and reliable grid theory and geodesic theory, four types of domes(helical winding, helical winding ellipsoid, polar winding, polar winding ellipsoid)were studied.The control equations of each type of dome were derived.According to each type of dome, case calculation was carried out to verify the correctness of the design method.The result analysis shows that the design results of meridian, winding angle, wall thickness, fiber stress and pV/W of the same winding pattern are similar.Ellipsoid dome is recommended to avoid the curvature inflection point of meridian, which is also conducive to processing and manufacturing.The research results can provide reference for the design and selection of FCPV.

References:

[1] 王婉君,张鹏,贺政豪,等.碳纤维复合材料压力容器的研究进展[J].现代化工,2020,40(1): 68-71.
[2] 冯雪,沈俊,田桂,等.复合材料压力容器在航天领域的应用研究[J].火箭推进,2014,40(4): 35-42. FENG X,SHEN J,TIAN G,et al.Research of composite over-wrapped pressure vessels for space application[J].Journal of Rocket Propulsion,2014,40(4): 35-42.
[3] 陈军军,田桂,沈俊,等.“柱形”铝内衬纤维缠绕复合材料气瓶自紧分析[J].火箭推进,2014,40(3): 57-62. CHEN J J,TIAN G,SHEN J,et al.Analysis on autofrettage of filament-wound composite cylinder[J].Journal of Rocket Propulsion,2014,40(3): 57-62.
[4] 晏飞.纤维缠绕/金属内衬复合材料气瓶应力分析[J].火箭推进,2011,37(1): 46-50. YAN F.Stress analysis of filament-wound composite gas cylinders with metal liner[J].Journal of Rocket Propulsion,2011,37(1): 46-50.
[5] ROSATO D V,GROVE C S.Filament winding: its development,manufacture,applications,and design [M].[S.l.]:Interscience Publishers,1964.
[6] SHIBLEY A M.Filament winding[M]//Handbook of composites.Boston,MA: Springer US,1982: 449-478.
[7] PETERS S T,HUMPHREY W D,FORAL R F.Filament winding composite structure fabrication [M].[S.l.]:SAMPE International Business Office,1991.
[8] ZU L,KOUSSIOS S,BEUKERS A.Design of filament-wound domes based on continuum theory and non-geodesic roving trajectories[J].Composites Part A: Applied Science and Manufacturing,2010,41(9): 1312-1320.
[9] FUKUNAGA H,UEMURA M.Optimum design of helically wound composite pressure vessels[J].Composite Structures,1983,1(1): 31-49.
[10] HOJJATI M,SAFAVI ARDEBILI V,HOA S V.Design of domes for polymeric composite pressure vessels[J].Composites Engineering,1995,5(1): 51-59.
[11] 李长鹏,谢淮北,刘力红.纤维缠绕超高压容器承载特性研究[J].兵器材料科学与工程,2019,42(2): 25-30.
[12] 何朋飞.碳纤维缠绕压力容器结构设计及其有限元分析[D].武汉: 武汉工程大学,2018.
[13] 周吉.纤维缠绕压力容器的强度分析和优化设计[D].武汉: 华中科技大学,2015.
[14] 矫维成,王荣国,刘文博,等.纤维缠绕复合材料压力容器封头厚度预测[J].复合材料学报,2010,27(5): 116-121.
[15] 祖磊,穆建桥,王继辉,等.基于非测地线纤维缠绕压力容器线型设计与优化[J].复合材料学报,2016,33(5): 1125-1131.
[16] DE CARVALHO J,LOSSIE M,VANDEPITTE D,et al.Optimization of filament-wound parts based on non-geodesic winding[J].Composites Manufacturing,1995,6(2): 79-84.
[17] KIM C U,KANG J H,HONG C S,et al.Optimal design of filament wound structures under internal pressure based on the semi-geodesic path algorithm[J].Composite Structures,2005,67(4): 443-452.
[18] LIANG C C,CHEN H W,WANG C H.Optimum design of dome contour for filament-wound composite pressure vessels based on a shape factor[J].Composite Structures,2002,58(4): 469-482.
[19] TEW B W.Preliminary design of tubular composite structures using netting theory and composite degradation factors[J].Journal of Pressure Vessel Technology,1995,117(4): 390-394.
[20] 陈汝训.固体火箭发动机设计与研究[M].北京: 宇航出版社,1992.
[21] 周敏,王志辉.纤维缠绕压力容器封头段的网络分析[J].机械制造,2010,48(8): 39-41.

Memo

Memo:
-
Last Update: 1900-01-01