复合材料褶皱夹芯结构研究进展

邓云飞; 曾宪智; 周翔; 李向前; 熊健

doi:10.13801/j.cnki.fhclxb.20200903.001

复合材料褶皱夹芯结构研究进展

doi: 10.13801/j.cnki.fhclxb.20200903.001

邓云飞¹,
曾宪智¹,
周翔³,
李向前⁴,
熊健^2, ,

1.
中国民航大学　航空工程学院，天津 300300
2.
哈尔滨工业大学　复合材料与结构研究所，哈尔滨 150080
3.
上海交通大学　航空航天学院，上海 200240
4.
中国航发商用航空发动机有限责任公司，上海 200000

基金项目: 国家自然科学基金 (11702317；11572100)；航空科学基金 (2018ZF67011)；中央高校基本科研业务费资(3122019076)

详细信息

通讯作者:
熊健，博士，教授，博士生导师，研究方向为复合材料结构设计与性能评价　E-mail：jx@hit.edu.cn

中图分类号: TG156；V214.8；TB33
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- 被引次数: 0
出版历程
- 收稿日期: 2020-04-20
- 录用日期: 2020-08-21
- 网络出版日期: 2020-09-03
- 刊出日期: 2020-12-15

Research progress for the composite sandwich structure with foldcore

1.
College of Aeronautical Engineering, Civil Aviation University of China, Tianjin 300300, China
2.
Institute for Composite Materials and Structures, Harbin Institute of Technology, Harbin 150080, China
3.
School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China
4.
AECC Commercial Aircraft Engine Co. Ltd., Shanghai 200000, China

摘要

摘要: 复合材料褶皱夹芯结构是通过二维材料折叠而成的三维周期性空间结构，作为一种新型的夹芯结构，具有轻质、高比强度、高比刚度、芯子空间贯通及多功能潜力等优势。本文结合飞行器结构轻量化和多功能化要求，对近年来复合材料褶皱夹芯结构的主要研究成果与特点进行了总结和分析。阐述了复合材料褶皱夹芯结构的构型优化方案及制备工艺，重点归纳了复合材料褶皱夹芯结构的力学性能及多功能的研究现状，包括结构的准静态力学性能、抗冲击性能及隔声、热防护、隐身性能等。基于国内外研究现状，对未来复合材料褶皱夹芯结构的重点研究方向进行了展望。
- 复合材料 /
- 褶皱芯子 /
- 力学性能 /
- 失效机制
Abstract: The composite sandwich structure with foldcore is a new type of structural material with light weight, high specific strength, high specific rigidity and multi-functional potential, which is connected with each other in core space. This kind of three dimensional structures can be formed by folding based on two dimensional materials. The main research achievements and characteristics of composite sandwich structure with foldcore in recent years are summarized and analyzed according to the lightweight and multi-functional requirements of aircraft structure in this paper. The configuration optimization scheme and fabrication process of the composite sandwich structure with foldcore are described. Moreover, the research status of mechanical properties and multi-function of the composite sandwich structure with foldcore are summarized, including the quasi-static mechanical properties, impact resistance, sound insulation, thermal protection, stealth performance of the structure, etc. Based on the research status, it provides suggestions for the research possible direction of the composite sandwich structure with foldcore in future.
- composite /
- foldcore /
- mechanical property /
- failure mechanisms

HTML全文

图 1 褶皱夹芯结构

Figure 1. Sandwich structure with foldcore

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图 2 通道结构^[5]

Figure 2. Channel structure^[5]

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图 3 褶皱芯子几何参数^[9]

Figure 3. Geometric parameters of foldcore^[9]

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图 4 褶皱芯子构型^[10-11]

Figure 4. Configurations of foldcores^[10-11]

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图 5 褶皱芯子折叠工艺^[12]

Figure 5. Folding technology of core^[12]

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图 6 V型褶皱芯子设计方法^[14]

Figure 6. Design method of V-type foldcore^[14]

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图 7 缩进式V型褶皱芯子^[14]

Figure 7. Indented V-type foldcore^[14]

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图 8 改进V型褶皱芯子^[17]

Figure 8. Improvement of V-type foldcore^[17]

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图 9 碳纤维橄榄型芯子^{[10, 18]}

Figure 9. Carbon fiber reinforced olive type foldcore^{[10, 18]}

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图 10 S型褶皱夹芯结构^[22]

Figure 10. Sandwich structure with S-type foldcore^[22]

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图 11 S型褶皱芯子与V型褶皱芯子屈曲破坏应力对比^[23]

Figure 11. Comparisons on buckling failure stress between S-type and V-type foldcores^[23]

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图 12 多种型面的褶皱芯子^{[9, 25]}

Figure 12. Foldcores of various configurations^[9,25]

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图 13 分割型模具操作流程^[23]

Figure 13. Operation process of split mold^[23]

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图 14 连续折叠与弯曲技术^{[10, 27]}

Figure 14. Continuous creasing and bending technique^{[10, 27]}

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图 15 褶皱夹芯圆筒结构的成型^[28]

Figure 15. Fabrication of sandwich cylinder structure with foldcore^[28]

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图 16 缠绕-铺贴工艺^[30]

Figure 16. Filament-winding and lay-up placing techniques^[30]

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图 17 褶皱结构的整体坐标系^[32]

Figure 17. Illustration of foldcore sandwich structures^[32]

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图 18 V型褶皱结构与蜂窝结构性能对比

Figure 18. Comparisons of performance between sandwich structures with V-type foldcore and honeycomb core

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图 19 V型褶皱夹芯结构与其它夹芯结构的抗冲击性能对比

Figure 19. Comparisons of impact resistance between sandwich structure with V-type foldcore and other sandwich structures

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图 20 芯子Z向平压等效过程^[9]

Figure 20. Equivalent process of Z-direction flat pressing of core^[9]

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图 21 V型褶皱芯子模量的理论值与数值模拟值^[10]

Figure 21. Theoretical and simulated modulus of V-type foldcore^[10]

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图 22 S型碳纤维褶皱夹芯结构(黑点部分)与其它夹芯结构性能对比^[23]

Figure 22. Comparison of properties between carbon fiber sandwich structures with S-type foldcore (black spot) and other sandwich structures^[23]

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图 23 V型褶皱芯子对信号的反射^[81]

Figure 23. Reflection of signal by V-type foledcore^[81]

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表 1 不同构型V型和S型褶皱芯子的参数

Table 1. Geometric parameters of different models for V-type and S-type foldcores

V-type foldcore			S-type foldcore			h/mm	l/mm	θ/(°)	β/(°)
Model	Relative density/%	Strength/MPa	Model	Relative density/%	Strength/MPa	h/mm	l/mm	θ/(°)	β/(°)
CU1	3.69	2.50	CH1	3.56	1.51	14	20	60	60
CU2	2.79	1.81	CH2	2.69	1.13	19	20	60	60
CU3	2.25	1.33	CH3	2.17	0.90	24	20	60	60
CU4	2.79	2.13	CH4	2.69	1.41	19	15	60	60
CU5	2.79	1.55	CH5	2.69	0.94	19	25	60	60
CU6	2.56	2.78	CH6	2.38	1.29	19	20	50	60
CU7	2.07	1.24	CH7	2.04	1.02	19	20	70	60
CU8	1.76	1.02	CH8	1.71	0.72	19	20	60	50
CU9	3.14	3.06	CH9	3.01	1.61	19	20	60	70

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表 2 V型褶皱夹芯结构模量预测

Table 2. Modulus prediction of sandwich structure with V-type folecore

Configuration	Flat compression modulus E_Z/MPa			Shear modulus G_ZX/MPa			Shear modulus G_ZY/MPa
Configuration	Theoretical	Numerical simulation	Difference/%	Theoretical	Numerical simulation	Difference/%	Theoretical	Numerical simulation	Difference/%
1	1309	1281	2.19	1309	1151	12.12	566	465	17.93
2	616	581	5.79	616	540	12.37	266	247	7.25
3	698	662	5.22	698	612	12.35	302	272	9.95
4	1164	1130	2.86	1164	1022	12.20	503	418	16.94
5	873	836	4.23	873	766	12.27	377	326	13.69

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