AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
Article Link
Collect
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Full Length Article | Open Access

Thermo-mechanical properties of RTM-made carbon fibre/polyimide composite attaching collar under transient heating

Shengda JIANGa,Chuyang LUOa( )Peng ZHANGbJianwen BAObPeipei CAIcXufeng XIAc
Shanghai High Performance Fibers and Composites Center (Province-Ministry Joint), Center for Civil Aviation Composites, Donghua University, Shanghai 201620, China
AVIC Composite Technology Center, Science and Technology on Advanced Composites Laboratory, Beijing 101300, China
Luoyang Optoelectro Technology Development Center, Luoyang 471009, China

Peer review under responsibility of Editorial Committee of CJA.

Show Author Information

Abstract

This study focuses on the thermo-mechanical properties of Carbon Fibre/Polyimide Composite (CFPC) attaching collars under transient heating. The CFPC attaching collars were fabricated by a high-temperature resin transfer moulding process, and their thermo-mechanical properties under the conditions of simultaneous transient heating and bending load were investigated. The results show that the attaching collar tends to fail at 118% of the limit load. The failure mode includes the fracture of the connecting screws, local extrusion damage of the hole edges, and slight ablation damage at the outer plies. And there is no observable residual deformation in the composite attaching collar. Furthermore, considering that the material properties vary with temperature, a progressive damage model based on the sequential thermo-mechanical coupling method was established to study the failure mechanism of the attaching collar. Finally, the damage factor of the CFPC was calculated to assess the safety status of the attaching collar. The results show that the primary damage modes of the composite attaching collar are intralaminar failure, which mainly occurs at the heat insulation layer and the hole edges, and these slightly affect the structural bearing capacity. A good correlation between the experiment and FEA is obtained. The test methods and analysis models proposed contribute to the safety assessment of composite structures under transient heating.

References

1

Xiong JJ, Shenoi RA. General aspects on structural integrity. Chin J Aeronaut 2019;32:114–32.

2

Luo CY, Xiong JJ. Static pull and push bending properties of RTM-made TWF composite Tee-joints. Chin J Aeronaut 2012;25:198–207.

3

Yang BF, Yue Z, Geng XL, et al. Effects of space environment temperature on the mechanical properties of carbon fiber/bismaleimide composites laminates. Proc Inst Mech Eng Part G J Aerosp Eng 2018;232:16–113.

4

Wolfrum J, Dinnebier H, Körwien T. Rapid high temperature loads on dry and moist carbon fibre epoxy composite materials. J Compos Mater 2014;48:3513–20.

5

Vieille B, Chabchoub M, Gautrelet C. Influence of matrix ductility and toughness on strain energy release rate and failure behavior of woven-ply reinforced thermoplastic structures at high temperature. Compos B Eng 2018;132:125–40.

6

Suvarna R, Arumugam V, Bull DJ, et al. Effect of temperature on low velocity impact damage and post-impact flexural strength of CFRP assessed using ultrasonic C-scan and micro-focus computed tomography. Compos B Eng 2014;66:58–64.

7

Dubary N, Taconet G, Bouvet C, et al. Influence of temperature on the impact behavior and damage tolerance of hybrid woven-ply thermoplastic laminates for aeronautical applications. Compos Struct 2017;168:663–74.

8

Wang Y, Zhang JP, Fang GD, et al. Influence of temperature on the impact behavior of woven-ply carbon fiber reinforced thermoplastic composites. Compos Struct 2018;185:435–45.

9

Wang SQ, Dong SL, Gao Y, et al. Thermal ageing effects on mechanical properties and barely visible impact damage behavior of a carbon fiber reinforced bismaleimide composite. Mater Des 2017;115:213–23.

10

Zrida H, Fernberg P, Ayadi Z, et al. Microcracking in thermally cycled and aged Carbon fibre/polyimide laminates. Int J Fatigue 2017;94:121–30.

11

Owens GA, Schofield SE. Thermal cycling and mechanical property assessment of carbon fibre fabric reinforced PMR-15 polyimide laminates. Compos Sci Technol 1988;33:177–90.

12

Lu C, Chen P, Yu Q, et al. Thermal residual stress distribution in carbon fiber/novel thermal plastic composite. Appl Compos Mater 2008;15:157–69.

13

Bek L, Kottner R, Laš V. Material model for simulation of progressive damage of composite materials using 3D Puck failure criterion. Compos Struct 2021;259:113435.

14

Zhu YT, Xiong JJ. High-temperature effect on the mechanical performance of screwed CFRPI–TC4 alloy joints repaired with metal inserts. J Compos Mater 2020;54:2245–60.

15

Zhu YT, Xiong JJ, Luo CY, et al. Progressive damage characteristics of screwed single-lap CFRPI-metal joint subjected to tensile loading at RT and 350℃. J Compos Mater 2021;55:2069–86.

16

Liu PF, Liao BB, Jia LY, et al. Finite element analysis of dynamic progressive failure of carbon fiber composite laminates under low velocity impact. Compos Struct 2016;149:408–22.

17

Liao BB, Liu PF. Finite element analysis of dynamic progressive failure of plastic composite laminates under low velocity impact. Compos Struct 2017;159:567–78.

18

Iarve E, Hoos K, Braginsky M, et al. Progressive failure simulation in laminated composites under fatigue loading by using discrete damage modeling. J Compos Mater 2016;51:2143–61.

19

Wan L, Yaser I, Sheng Y, et al. Progressive failure analysis of CFRP composite laminates under uniaxial tension using a discrete element method. J Compos Mater 2021;55:1091–108.

20

Wang YC, Huang ZM. Bridging tensor with an imperfect interface. Eur J Mech A/Solids 2016;56:73–91.

21

Chen Q, Tu WQ, Liu RN, et al. Parametric multiphysics finite-volume theory for periodic composites with thermo-electro-elastic phases. J Intel Mat Syst Str 2017;29:530–52.

22

Rozylo P, Debski H, Kubiak T. A model of low-velocity impact damage of composite plates subjected to compression-after-impact (CAI) testing. Compos Struct 2017;181:158–70.

23

Shaterzadeh AR, Abolghasemi S, Rezaei R. Finite element analysis of thermal buckling of rectangular laminated composite plates with circular cut-out. J Therm Stress 2014;37:604–23.

24

Liu Q, Ma JB, Xu XY, et al. Load bearing and failure characteristics of perforated square CFRP tubes under axial crushing. Compos Struct 2017;160:23–35.

25

Gorfain JE, Key CT. Damage prediction of rib-stiffened composite structures subjected to ballistic impact. Int J Impact Eng 2013;57:159–72.

26

Wagner W, Balzani C. Simulation of delamination in stringer stiffened fiber-reinforced composite shells. Comput Struct 2008;86:930–9.

27

Zhou DW, Louca LA, Saunders M. Numerical simulation of sandwich T-joints under dynamic loading. Compos B Eng 2008;39:973–85.

28

Xiong JJ, Zhu YT, Luo CY, et al. Fatigue-driven failure criterion for progressive damage modelling and fatigue life prediction of composite structures. Int J Fatigue 2021;145:106110.

29

Liu G, Luo CY, Zhang DJ, et al. Mechanical performance and failure mechanism of thick-walled composite connecting rods fabricated by resin transfer molding technique. Appl Compos Mater 2015;22:423–36.

30

Wu DF, Wang YW, Pan B, et al. Experimental research on the ultimate strength of hard aluminium alloy 2017 subjected to short-time radioactive heating. Mater Des 2012;40:502–9.

31

Wu DF, Song H, Li YT, et al. A study on mechanical properties of 5A06 Al-Mg alloy at transient heating. J Exper Mech 2006;21:591–5 [Chinese].

32

Wu DF, Song H, Gao ZT, et al. Mechanical properties of 2A12 Al alloy at transient heating. J Beijing Univ Aeron Astron 2007;33:531–4 [Chinese].

33

Jiang KH, Zhou SZ, Wu DF. Bending experiment of composite beams at transient high temperature. J Beijing Univ Aeron Astron 1996;22:145–8 [Chinese].

34

Zhang YW, Hao ZP, Wu DF, et al. Tensile properties of Al-Mg-Li alloy by fast heating. Miss & Spac Vehicl 2010;6:50–2 [Chinese].

35

Wu DF, Pan B, Wang YW, et al. Mechanical properties of super-high strength Al 7A04 at transient heating. Acta Metall Sin 2011;47:755–60 [Chinese].

36

Connell J, Smith JG, Hergenrother P, et al. High temperature transfer molding resins: Laminate properties of PETI-298 and PETI-330. High Perform Polym 2003;15:375–94.

37
ABAQUS version 2016 user’s manual. Mason: Dassault Systemes Simulia Corp; 2016.
38

Bai JB, Dong CH, Xiong JJ, et al. Progressive damage behaviour of RTM-made composite T-joint under tensile loading. Compos B Eng 2019;160:488–97.

39

Christiansen E, Andersen KD. Computation of collapse states with von Mises type yield condition. Int J Numer Meth Engng 1999;46:1185–202.

40

Wang CK, Huang CG, Sun YL, et al. Influence of heating rate and strain rate on tensile strength of 30CrMnSi. Acta Metall Sin 1995;31:A475–8 [Chinese].

Chinese Journal of Aeronautics
Pages 393-405
Cite this article:
JIANG S, LUO C, ZHANG P, et al. Thermo-mechanical properties of RTM-made carbon fibre/polyimide composite attaching collar under transient heating. Chinese Journal of Aeronautics, 2023, 36(3): 393-405. https://doi.org/10.1016/j.cja.2022.11.009

33

Views

2

Crossref

2

Web of Science

2

Scopus

Altmetrics

Received: 09 November 2021
Revised: 21 November 2021
Accepted: 31 December 2021
Published: 17 November 2022
© 2022 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

Return