• Composites Research
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• 제20권3호
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• pp.17-24
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• 2007

본 연구는 순수 Kevlar 직물과 실리카 입자를 포함하는 전단농화유체가 함유된 Kevlar 액체방탄재(STF-Kevlar)에 대한 방탄충격에 의한 파단모드 연구이다. Cal.22 파편탄과 9mm FMJ 볼탄에 의한 방탄시험에 의하여 이 두 재료는 거시적 측면에서 다른 파단모드를 보여주었다. 순수 Kevlar 직물에서는 얀의 뽑힘(Pull-out)이, 그리고 STF-Kevlar 액체방탄재에서는 얀의 파단이 충격에너지를 흡수하는 주 기구로 나타났다. 전자주사현미경에 의한 미시적 관찰에서 Kevlar 섬유 표면의 벗겨짐, 섬유가 여러 가닥으로 갈라지는 스프리트, 그리고 섬유의 절단, 이 세가지 파단 모드가 손상 정도의 차이는 있지만 공통적으로 두 재료에서 관찰되었다. STF-Kevlar에서, 얀 섬유의 파단은 첫째는 실리카 입자로 덮여있는 얀-얀, 직물-직물 사이의 마찰력과, 둘째는 충격시 전단농화 현상의 발생으로 얀의 이동이 강력하게 억제되기 때문인 것으로 보인다.

• Elastomers and Composites
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• 제54권2호
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• pp.91-96
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• 2019

The purpose of this study was to examine the effect of different yarn twisting methods on physical properties. Plain single jersey structured fabrics were knitted from Kevlar yarn, and from Kevlar/HPPE, and from Kevlar/Basalt fiber, and from Kevlar/Glass fiber and Kevlar/Stainless steel fiber blended and core-spun yarns. and then, The fabrics were coated NBR Latex. The physical properties, including tear strength, modulus, degree of penetration, heat resistance, and cut resistance of the knitted fabrics were investigated and compared. Kevlar/HPPE blended yarn fabrics recorded the highest heat resistance (13 Sec.). and Kevlar/HPPE blended yarn fabrics had good cut resistance (Cut Level 4).

• 한국염색가공학회지
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• 제7권1호
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• pp.43-50
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• 1995

The grafting of methacrylonitrile(MAN) onto Kevlar 49 filament surface was carried out by anionic polymerization using sodium methylsulfinylcarbanion formed from sodium hydride and dimethyl sulfoxide(DMSO). The effects of reaction conditions on the grafting percentage(GP) and on the tensile strength of the fiber were investgated. GP marktedly increased with increasing metalation time, and NaH concentration, polymerization temperature and time. The tensile strength of fiber decrased with increasing metalation time, and NaH concentration, polymerization temperature and time. The optimum conditions to increase over 40% of GP with below 10% reduction rate of tensile strength of fiber : NaH concentration ; 30.6 mmol/l/0.5g Kevlar, metalation time : 10min, polymerization tempera- ture : 5$0^{\circ}C$, polymerization time: 20 sec, monomer concentration : 1.12mol/l/0.5g Kevlar.

• Composites Research
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• 제16권4호
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• pp.74-79
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• 2003

Micromechanical 시험법과 음향방출을 이용하여 산소 플라즈마 처리된 PBO와 Kevlar 섬유강화 에폭시 복합재료의 계면물성과 미세파괴메카니즘을 고찰하여 상호 비교하였다. 산소 플라즈마 처리된 PBO와 Kevlar 섬유강화 에폭시 복합재료의 계면전단강도와 접착일은 극성 작용기의 도입으로 향상 시킬 수 있었다. 임계표면장력과 총 표면자유에너지 중 극성 표면자유에너지는 플라즈마 처리된 Kevlar 섬유에서 가장 컸으며. 미처리된 PBO의 섬유의 경우에서 가장 작았다. Microfibril 파단 형상은 산소 플라즈마 처리된 Keviar 섬유의 경우에서는 명확하게 관찰 되었으며. 미처리와 비교차여 microfibril 파단이 대각선 방향으로 연속적해서 일어나 가장 많은 섬유 파단 신호가 감지되었다 비파괴 음향방출법을 이용하여 얻은 섬유파단 감지 결과는 microdroplet과 두 섬유강화 복합재료 시험법에서 광학현미경을 이용하여 관찰한 미세파단 형상과 상호 일치하였다.

• Composites Research
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• 제20권3호
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• pp.1-7
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• 2007

본 연구는 전단농화유체(STF)가 함침된 Kevlar 복합재료(STF-Kevlar composite)의 제조 및 방탄성능 평가에 관한 내용이다. 전단농화유체는 fumed silica와 구형 silica를 에틸렌글리콜에 혼합하여 제조하였고 이 유체를 Kevlar직물에 함침시켜 액체방탄재료를 제작하였다. 전단농화거동을 조사한 결과 사용된 STF는 모두 전단농화거동이 발현됨을 확인하였다. 그리고 방탄시험 결과 구형silica STF-Kevlar 복합재료가 보다 우수한 방탄특성을 나타내었다. 한편 방탄시험 시 neat Kevlar 시험편에서는 탄자가 섬유를 pull-out하면서 관통하는 현상이 발생하였으나 LBA시험편에서는 섬유의 pull-out 대신 원주방향으로 섬유가 변형되면서 방탄재료가 변형되는 거동을 보여 서로 다른 변형거동을 각각 나타내는 것으로 관찰되었다.

• Fibers and Polymers
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• 제1권1호
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• pp.45-54
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• 2000

Impact behaviors of the large deformable composites of Kevlar fiber reinforced composites of different preform structures have been investigated. An analytic tool was developed to characterize the impact behavior of the Kevlar composites. The image analysis technique, and deply technique were employed to develop energy balance equation under impact loading. An energy method was employed to establish the impact energy absorption mechanism of Kevlar multiaxial warp knitted composites. The total impact energy was classified into four categories including delamination energy, membrane energy, bending energy and rebounding energy under low velocity impact. Membrane and bending energy were calculated from the image analysis of the deformed shape of impacted specimen and delamination energy was calculated using the deplying technique. Also, the impact behavior of Kevlar composites under high velocity impact of full penetration of the composite specimen was studied. The energy absorption mechanisms under high velocity impact were modelled and the absorbed energy was classified into global deformation energy, shear-out energy, deformation energy and fiber breakage energy. The total energy obtained from the model corresponded reasonably well with the experimental results.

• Restorative Dentistry and Endodontics
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• 제25권3호
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• pp.371-380
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• 2000

The effect of fiber reinforcing materials on the fracture strength of composite resin was evaluated. Each ten composite resin bars reinforced by glassfiber[Fiber-Splint ML$^{(R)}$(Polydentia SA, Switzerland)], polyethylene fiber [Ribbond$^{(R)}$(Ribbond Inc., U.S.A.)] and polyaramid fiber[Kevlar$^{(R)}$(DuPont, U.S.A.)] were loaded under the 3-point compression technique. Another ten pure composite resin bars without reinforcement were used as a control group. Then mean fracture strength and standard deviation were calculated and a ANOVA and Scheffe test were used in statistics. The results were as follows: 1. Kevlar group showed the highest fracture strength as 175.5MPa (p<0.05). Fiber-Splint ML group showed the lowest fracture strength as 112.7MPa. 2. The mean value of fracture strength in Ribbond group was 136.4MPa, and that of unterated control group was 143.6MPa. No difference was found between the two groups. 3. Ribbond and Kevlar reinforcement groups showed a catastrophic failure, where complete separation of pieces occurs to a unseparated fracture pattern. The use of Kevlar reinforcement fibers with composite resin showed significant increase in the average load failure and the presence of the fibers did prevent the catastrophic crack propagation present in the unreinforced samples. The use of Ribbond reinforcement fibers with composite resin showed no significant increase in the average load failure. However, the presence of the fibers did prevent the catastrophic crack propagation. Because high strength of glassfiber are rapidly degraded on exposure to moisture and humidity. The use of Fiber-Splint ML reinforcement fibers with composite resin showed significant decrease in the average load failure and displayed catastrophic fractures.

• 한국안전학회지
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• 제23권6호
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• pp.34-37
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• 2008

The composite materials are widely used in the many applications of industry as well as aerospace field because of their high specific stiffness and strength which benefits the material and provides potential energy savings. However, composite materials also have a low property about external applied impact. In this paper, impact tests were conducted on different sample types(glass, carbon and kevlar composite) to obtain information such as absorbed energy and composite deformation using an instrumented impact test machine (DYNATUP 8250). 3 type samples were compared to experimental results. The data from impact test provided valuable information between the different type samples by wet lay up. This paper shows results of that kevlar composite has larger absorption energy and deformation than others.

• 한국응용과학기술학회지
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• 제24권1호
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• pp.23-30
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• 2007

Kevlar was chemically surface modified with resorcinol-formaldehyde(RF) prepolymer and VP rubber latex for application to high strength tirecords. RF prepolymer was easily obtained by polymerization at room temperature in the presence of a base catalyst. The mechanical and thermal properties of Kevlar were not significantly changed during surface treated under various conditions. The change of adhesion with rubber were investigated through H-test method. Maximum increase of adhesion force between rubber and Kevlar was obtained up to 40% than that of untreated one when the fiber was soaked in RFL dipping solution and thermally treated at $170^{\circ}C$ for 3 - 5min.

• 한국섬유공학회:학술대회논문집
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• 한국섬유공학회 1995년도 춘계학술발표회 프로그램 및 초록
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• pp.18-18
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• 1995