Effect of different stacking sequences on hybrid carbon/glass/epoxy composites laminate: Thermal, dynamic mechanical and long-term behavior

被引:21
作者
da Silva Monte Vidal, Dielly Cavalcanti [1 ]
Ornaghi Jr, Heitor L. [1 ]
Ornaghi, Felipe Gustavo [1 ]
Monticeli, Francisco Maciel [1 ]
Cornelis Voorwald, Herman Jacobus [1 ]
Hilario Cioffi, Maria Odila [1 ]
机构
[1] Sao Paulo State Univ, Sch Engn, Dept Mat & Technol, Fatigue & Aeronaut Mat Res Grp, Sao Paulo, Brazil
基金
巴西圣保罗研究基金会;
关键词
Structural composites; stacking sequence; carbon fiber; long-term prediction; BANANA FIBER; PREDICTION; TEMPERATURE; POLYMER; IMPACT; CREEP; MODEL; SIMULATION; RESISTANCE; STRENGTH;
D O I
10.1177/0021998319868512
中图分类号
TB33 [复合材料];
学科分类号
摘要
In the present study, different stacking sequences on hybrid carbon/glass/epoxy composites laminate were examined in relation to thermal, dynamic mechanical and long-term behavior. A positive hybrid effect was found for both hybrid composites (interleaved-Hybrid 1 and in block-Hybrid 2) showing that in some cases hybrid composites can properly replace carbon or glass composites. The composite containing all glass fiber in the middle (Hybrid 2) presented similar thermal behavior when compared to glass fiber composite. All hybrid composites presented higher storage modulus when compared to glass composite. Dynamic mechanical analysis showed that both hybrids can satisfactorily perform the requirement in a wide temperature range. The long-term prediction was successfully applied for all composites, showing to be highly temperature-dependent. Hence, depending on the application requirement, both hybrids can be used, saving weight and cost.
引用
收藏
页码:731 / 743
页数:13
相关论文
共 54 条
[1]  
Al-Qureshi HA, 2011, J MATER PROCESS TECH, V118, P58
[2]   Creep and interfacial behavior of carbon fiber reinforced epoxy filament wound laminates [J].
Almeida, Jose Humberto S., Jr. ;
Ornaghi, Heitor L. ;
Lorandi, Natalia P. ;
Bregolin, Bernardo P. ;
Amico, Sandro C. .
POLYMER COMPOSITES, 2018, 39 :E2199-E2206
[3]   Model for prediction of simultaneous time-dependent damage evolution in multiple plies of multidirectional polymer composite laminates and its influence on creep [J].
Asadi, Amir ;
Raghavan, J. .
COMPOSITES PART B-ENGINEERING, 2015, 79 :359-373
[4]   Fiber-reinforced polymer composites for construction-state-of-the-art review [J].
Bakis, CE ;
Bank, LC ;
Brown, VL ;
Cosenza, E ;
Davalos, JF ;
Lesko, JJ ;
Machida, A ;
Rizkalla, SH ;
Triantafillou, TC .
JOURNAL OF COMPOSITES FOR CONSTRUCTION, 2002, 6 (02) :73-87
[5]   Effect of chemical vapor infiltration on erosion and thermal properties of porous carbon/carbon composite thermal insulation [J].
Baxter, RI ;
Rawlings, RD ;
Iwashita, N ;
Sawada, Y .
CARBON, 2000, 38 (03) :441-449
[6]   Experimental RTM Manufacturing Analysis of Carbon/Epoxy Composites for Aerospace Application: Non-crimp and Woven Fabric Differences [J].
Brocks, Thatiane ;
Shiino, Marcos Yutaka ;
Hilario Cioffi, Maria Odila ;
Cornelis Voorwald, Herman Jacobus ;
Caporalli Filho, Angelo .
MATERIALS RESEARCH-IBERO-AMERICAN JOURNAL OF MATERIALS, 2013, 16 (05) :1175-1182
[7]   Modeling the Viscosity Development of Epoxy Resins during Injection of the RTM Process [J].
Caba, Stefan ;
Koch, Michael .
PROCEEDINGS OF THE REGIONAL CONFERENCE GRAZ 2015 - POLYMER PROCESSING SOCIETY PPS: CONFERENCE PAPERS, 2016, 1779
[8]  
Cho K.S., 2016, Viscoelasticity of Polymers: Theory and Numerical Algorithms
[9]  
Das S., COST AUTOMOTIVE POLY, DOI DOI 10.2172/777656
[10]   Determination of CTEs of cured epoxy and polyester (PET) stitching threads [J].
Deng, Shiqiang ;
Hou, Meng ;
Liu, Xiaolin ;
Qi, Ben ;
Ye, Lin .
JOURNAL OF COMPOSITE MATERIALS, 2011, 45 (20) :2071-2081