• Title/Summary/Keyword: Woven composite

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Development of composite filter with high performance meltblown non-woven (고성능 멜트블로운 부직포 복합필터 개발)

  • Lee Jae-Dal;Hong Young-Ki;Bae Kie-Seo
    • Textile Coloration and Finishing
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    • v.17 no.2 s.81
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    • pp.40-45
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    • 2005
  • Electret filter is good enough to protect health and environment from air pollution. The reason why is gathering particles not only by mechanical mechanism but also by electrostatic attraction. Especially this filter is shown lower pressure drop than general mechanical filters as glass fiber. For making electret filter media using polypropylene meltblown(M/B) nonwoven, the nonwoven is charged with corona which was supplied high voltage DC, AC, and pulse with DC power. The electret filter media is tested with $0.3{\mu}m$ sodium chloride and dioctyl phthalate(DOP) aerosol. Results revealed that filtration performance of electret filter media increased as corona was applied with higher voltage and with AC power rather than DC, and fiber diameter was fine and uniform.

A Probabilistic Analysis for Fatigue Cumulative Damage and Fatigue Life in CFRP Composites Containing a Circular Hole (원공을 가진 CFRP 복합재료의 피로누적손상 및 피로수명에 대한 확률적 해석)

  • 김정규;김도식
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.8
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    • pp.1915-1926
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    • 1995
  • The Fatigue characteristics of 8-harness satin woven CFRP composites with a circular hole are experimentally investigated under constant amplitude tension-tension loading. It is found in this study that the fatigue damage accumulation behavior is very random and history-independent, and the fatigue cumulative damage is linearly related with the mean number of cycles to a specified damage state. From these results, it is known that the fatigue characteristics of CFRP composites satisfy the basic assumptions of Markov chain theory and the parameter of Markov chain model can be determined only by mean and variance of fatigue lives. The predicted distribution of the fatigue cumulative damage using Markov chain model shows a good agreement with the test results. For the fatigue life distribution, Markov chain model makes similar accuracy to 2-parameter Weibull distribution function.

Drilling Characteristics of Glass Fiber Reinforced Polyester (유리섬유 강화 폴리에스터의 드릴가공 특성)

  • 김성일
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.9 no.3
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    • pp.90-95
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    • 2000
  • Today fiber composite materials are routinely used in such wide applications as ships automobiles aircraft space vehi-cles containers sporting goods and appliances. The current knowledge of machining glass fiber reinforced polyester com-posites unfortunately is inadequate for its optimum utilization in many applications. Therefore This paper deals with drilling characteristic of glass fiber reinforced polyester composites. In the drilling of glass fiber reinforced polyester the quality of the cut surfaces is strongly dependent on the drilling parameters. drilling tests were carried out on glass fiber reinforced polyester using standard HSS tools. The material containing random chopped strand fibers and woven roving was fabricated by hand lay-up The entrance and exit surface of the holes was examined. The cutting force was also mea-sured to analyze the drilling characteristics,.

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차수재(HDPE) 보호재로서 지오신세틱스의 천공에 대한 효과

  • 이광열;정진교;안용수;구태곤
    • Proceedings of the Korean Society of Soil and Groundwater Environment Conference
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    • 2003.09a
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    • pp.64-68
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    • 2003
  • The purpose of the study is to compare the efficiency of protection as a liner protective material for geosynthetics. A series of tests were conducted in this study to analyze the effects of geosynthetics against puncture loads. Various types of geosynthetics are used as a protective material. Non-woven, Geo-composite, NaBento GCL, GCL are used to create puncture failure that caused by vertically applied loads. The results indicated that combination of geosynthetics and a protective material can be subjected to bigger loads than geosynthetics and a protective material separated each other do.

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Radial flow advancement in multi-layered preform for resin transfer molding

  • Shin, K.S.;Song, Y.S.;Youn, J.R.
    • Korea-Australia Rheology Journal
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    • v.18 no.4
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    • pp.217-224
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    • 2006
  • Rapid flow advancement without void formation is essential in the liquid composite molding (LCM) such as resin transfer molding (RTM) and vacuum assisted resin transfer molding (VARTM). A highly permeable layer in multi-layered preform has an important role in improvement of the flow advancement. In this study, a multi-layered preform which consists of three layers is employed. Radial flow experiment is carried out for the multi-layered preform. A new analytic model for advancement of flow front is proposed and effective permeability is defined. The effective permeability for the multi-layered preform is obtained analytically and compared with experimental results. Compaction test is performed to determine the exact fiber volume traction of each layer in the multi-layered preform. Transverse permeability employed in modeling is measured experimentally unlike the previous studies. Accurate prediction of flow advancement is of great use for saving the processing time and enhancing product properties of the final part.

Synthesis and mechanical properties of flax fabric reinforced geopolymer composites

  • Assaedi, Hasan S.;Alomayri, Thamer S.;Shaikh, Faiz U.A.;Low, It-Meng
    • Advances in materials Research
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    • v.3 no.3
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    • pp.151-161
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    • 2014
  • Geopolymer composites reinforced with different layers of woven flax fabric are fabricated using lay- up technique. Mechanical properties, such as flexural strength, flexural modulus and fracture toughness of geopolymer composites reinforced with 2.4, 3 and 4.1 wt% flax fibres are studied. The fracture surfaces of the composites are also examined using scanning electron microscopy. The results show that all the mechanical properties of the composites are improved by increasing the flax fibre contents. It is also found that the mechanical properties of flax fabric reinforced geopolymer composites are superior to pure geopolymer matrix. Micro-structural analysis of fracture surface of the composites indicated evidence of various toughening mechanisms by flax fabrics in the composites.

Spin Test of 3D C/SiC Composite Blisk Rotor Model

  • Hashimoto. Ryosaku;Ogawa, Akinori;Sofue, Yahushi;Hojo, Masahiro
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2004.03a
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    • pp.398-400
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    • 2004
  • The three-dimensional woven fabric C/SiC composites blisk turbine rotor model was evaluated. The spin tests of the blisk model were performed to measure strain distributions at the room temperature. The rotational strength of the blisk model could be improved by the fiber addition. But, there are still more researches to be done.

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Numerical Simulation of Preform Molding Using Carbon Fabric (카본 패브릭을 이용한 프리폼 성형에 대한 수치모사)

  • Park, Eun-Min;Lee, Soon-Young;Choi, Kyung-Hwan;Kim, Sun Kyoung
    • Composites Research
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    • v.33 no.2
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    • pp.61-67
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    • 2020
  • Preforming is crucial in resin transfer molding process using woven fabric. When shear deformation exceeds the locking angle, wrinkles are generated in the preform, which causes defects in the RTM process. Therefore, in this study, the allowable shear deformation limit of carbon fiber woven fabrics is quantified and the molding characteristics are verified using the actual fabric forming. As a result, the characteristics of creases according to the layer setups have been examined and the results have been discussed. Numerical analyses have been also performed using measured shear properties. These results have been compared with the experimental results.

Study on Out-of-plane Properties and Failure Behavior of Aircraft Wing Unit Structures (항공기 날개 부분 단위구조체의 면 외 방향 물성 및 파손거동에 관한 연구)

  • Yoon, Chang-Mo;Lee, Dong-Woo;Byun, Joon-Hyung;Tran, Thanh Mai Nguyen;Song, Jung-il
    • Composites Research
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    • v.35 no.2
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    • pp.106-114
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    • 2022
  • Carbon fiber-reinforced plastic, well known high specific strength and high specific stiffness, have been widely used in the aircraft industry. Mostly the CFRP structure is fabricated by lamination of carbon fiber or carbon prepreg, which has major disadvantage called delamination. Delamination is usually produced due to absence of the through-thickness direction fiber. In this study, three-dimensional carbon preform woven in three directions is used for fabrication of aircraft wing unit structure, a part of repeated structure in aircraft wing. The unit structure include skin, stringer and rib were prepared by resin transfer molding method. After, the 3D structure was compared with laminate structure through compression test. The results show that 3D structure is not only effective to prevent delamination but improved the mechanical strength. Therefore, the 3d preform structure is expected to be used in various fields requiring delamination prevention, especially in the aircraft industry.

A Study on the Failure Modes of Neat Kevlar Fabric and Kevlar Liquid Armor Impregnated with Shear Thickening Fluid (케블라 직물과 전단농화유체로 함침된 케블라 액체 방탄재의 파단모드 연구)

  • Yoon, Byung-Il;Song, Heung-Sub;Paik, Jong-Gyu
    • Composites Research
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    • v.20 no.3
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    • pp.17-24
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    • 2007
  • In this study, the failure modes by ballistic impacts were studied both for a neat Kevlar woven fabric and a Kevlar liquid armor impregnated with shear thickening fluid (STF) containing silica particles. These two materials showed quite different failure modes macroscopically in ballistic impacts tests used by Cal.22 FSP and 9mm FMJ bullet. Yarn pull-out for the neat Kevlar woven fabric and yarn fracture occurred partially through all plies from 1st ply to last one for the STF-Kevlar are an important energy absorption mechanisms. The results observed by S.E.M showed commonly fiber damage which are torn skin in the longitudinal fiber direction, fiber split axially and fiber fracture for two materials. The reasons why STF-kevlar liquid armor material exhibits excellent ballistic performance are as follow: firstly the increased friction forces between yarn-yarn and fabric-fabric covered with silica particles and secondary the evolution of shear thickening phenomenmon resulting in suppression of yarn mobility.