• Title/Summary/Keyword: Mechanical impact

검색결과 2,819건 처리시간 0.029초

복합판재의 파단 변형률 불확실성을 고려한 탄 관통 잔류속도에 대한 시험 및 수치해석 (Test and Numerical Analysis for Penetration Residual Velocity of Bullet Considering Failure Strain Uncertainty of Composite Plates)

  • 차명석;이민형
    • 대한기계학회논문집A
    • /
    • 제40권3호
    • /
    • pp.281-288
    • /
    • 2016
  • 복합재는 재료 불균질성에 의해 고속 충돌 시 방호성능 자료가 산포한다. 본 연구에서는 다수의 충돌시험으로 복합판재 잔류속도 산포를 확보하고 수치해석으로 예측하는 방법을 정립하였다. 먼저 10개의 동일 시편으로 인장시험을 수행하여 파단변형률 산포를 얻었다. 같은 재료로 제작된 4ply([0/90]s)와 8ply([0/90/0/90]s) GFRP(Glass Fiber Reinforced Plastic) 복합판재에 FSP(Fragment Simulating Projectile) 고속 충돌시험을 동일 조건에서 다수 수행하여 잔류속도 산포를 얻었다. 인장시험에서 얻어진 파단 변형률 분포를 이용하여 수치해석을 수행하였다. 충돌속도는 4ply와 8ply 각각 411.7m/s와 592.5m/s이다. 시험 결과와 비교하여 적절한 잔류속도의 산포를 예측할 수 있었다. 추가적으로 복합판재의 경우 Solid요소 대비 Layered Solid요소로 모델링하면 계산시간이 감소되었다.

구간 조합 복합재료 판의 충격 특성에 미치는 겹침부 설계에 관한 연구 (Effect of Overlap Design on the Impact Characteristics of Piecewise Integrated Composite Plates)

  • 황희윤
    • Composites Research
    • /
    • 제36권1호
    • /
    • pp.25-31
    • /
    • 2023
  • 복합재료 구조는 필요한 기계적 성능을 충족하기 위해 서로 다른 적층 각도로 적층하여 설계되었다. 외부 하중을 받는 복합재료 구조물에 대한 발생하는 응력은 위치에 따라 다르지만, 최대 응력을 바탕으로 적층 순서를 결정하는데, 이는 효율적이지 않으며 일반적으로 최적의 설계가 아니다. 최근 이러한 비효율성을 해결하기 위해 구간 조합 복합재료(PIC)가 제안되었다. PIC는 인접한 조각들 사이의 완벽한 결합을 가정하지만, 이것은 매우 이상적이고 달성하기 어렵다. 따라서 경계에서의 중첩은 서로 분리되지 않도록 하기 위해 필수적이다. 본 연구에서는 중첩 설계가 PIC 플레이트의 충격 파손 모드에 미치는 영향을 조사하였다. 속경화 탄소섬유 프리프레그를 이용하여 서로 다른 겹침부 형상 및 절개선 간격을 가지는 시험편을 제작하였으며, ASTM D 7136에 따라 충격시험을 수행하였다. 복합재료 적층판의 충격 파손 형태는 겹침부 설계에 따라 서로 다른 양상을 가졌으며, 이로 인해 충격흡수에너지 및 충격하중곡선의 경향에도 영향을 주었음을 알 수 있었다.

同一한 衝擊에너지 條件下의 CFRP 斜交積層板의 衝擊損傷과 配向角의 關係 (Relations Between Impact Damage and Ply Angle Under Same Impact Energy Condition)

  • 배태성;;양동율
    • 대한기계학회논문집
    • /
    • 제16권10호
    • /
    • pp.1824-1832
    • /
    • 1992
  • 본 연구에서는 충돌입자의 크기의 영향을 평가하기 위하여 동일한 운동에너지 를 갖는 직경 5mm 및 10mm의 강구를 시편에 충돌시킨 후 배항각 변화에 따른 손물역의 크기 변화를 초음파현미경(SAM)과 주사전자현미경(SEM)으로 관찰하였고, 충돌에 따른 압축강성의 변화를 고찰하기 위하여 충격전후의 압축탄성계수를 측정하였다.

센서 동역학을 고려한 충격응답해석 (Analysis of Impact Responses Considering Sensor Dynamics)

  • B. J. Ryu;K. Y. Ahn;B. H. Kwon;I. S. Oh;Lee, G. S.
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2002년도 추계학술대회논문초록집
    • /
    • pp.373.1-373
    • /
    • 2002
  • Impact is the most common type of dynamic loading conditions that give rise to impulsive forces and affects the vibrational characteristics of mechanical systems. Since the impact force and response are measured indirectly through the sensors, it is difficult to predict the impact force and acceleration. In this study, contact force model based on the Hertz law is proposed in order to predict the impact force correctly. (omitted)

  • PDF

고속충격을 받는 CFRP 복합재료의 잔류강도 예측 (Prediction of Residual Strength of CFRP Subjected to High Velocity Impact)

  • 박근철;김문생
    • 대한기계학회논문집
    • /
    • 제18권3호
    • /
    • pp.600-611
    • /
    • 1994
  • The purpose of this research is to propose a model for the prediction of residual strength. For this purpose, two-paremeter model based on Caprino's is developed and formulated by the ratio of indentation due to impact and normalized residual strength. The damage zone is considered only as an indentation. Impact tests are carried out on laminated composites by steel balls. Test material is carbon/epoxy laminate. The specimens are composed of $[{\pm}45^{\circ}/0^{\circ}/90^{\circ}]_2$ and $[\pm}45^{\circ}]_4$ stacking sequence and have $0.75^T{\times}0.26^W{\times}100^L(mm) dimension. A proposed model shows a good correlation with the experimental results And failure mechanism due to high impact velocity is discussed on CFRP laminates to examine the initiation and development of damage by fractography and ultrasonic image ststem. The effect of the unidirectional ply position on the residual strength is considered here.

PBT/ABS 블렌드의 물성에 관한 연구 (A Study on the Mechanical Properties of PBT/ABS blends)

  • 이중희;윤기호;박민정
    • 한국복합재료학회:학술대회논문집
    • /
    • 한국복합재료학회 2001년도 추계학술발표대회 논문집
    • /
    • pp.149-152
    • /
    • 2001
  • Poly-butylene-terephalate(PBT) can be impact modified by blending with ABS material. The effects of the type of compatibilizer and ABS content on the mechanical properties of PBT/ABS blend were examined in this study. EVA-g-GMA and three type of polycarbonates were used as the compatibilizer. As the GMA content in EVA-g-GMA was increased, the tensile strength of PBT/ABS blend increased and the impact strength of it decreased. With increasing the EVA-g-GMA content in PBT/ABS blend, the tensile strength and impact strength decreased. With PC compatibilizer, the tensile strength of PBT/ABS blend decreased as the ABS content increased. However, the maximum impact strength was observed in 20~30% ABS content range.

  • PDF

복합조직의 파괴거동과 파괴혁성에 관한 연구 I

  • 송삼홍;김규생
    • 대한기계학회논문집
    • /
    • 제5권2호
    • /
    • pp.110-121
    • /
    • 1981
  • In order to study on the fracture behavior and the fracture thoughness of combined structure, the specimens, structural steel (SM28C) and 6:4 brass are annealed for ductility and investigated for the befavior of fracture and the absorbed energy at the variation of the impact velocity. The results obtained by this study are as follows: (1)The maximum load increases with the impact velocity, but in the condition of constant impact velocity it decreases as the ductility increases. (2)The absorbed energy increases with the impact velocity, but in the condition of constant impact velocity it is constant as the ductility increases. (3)In the case of the combined structure of peralite and ferrite, the microcracks initiates and propagates mainly in the ferrite structure intergranular in accompany with the slip, and the slip concentration phenomena occur in the boundary of pearlite structure However, in case of the combined structure of .alpha. and ..betha. phase, the microcracks initiates and propagares mainly in the .alpha. phase intergranularly, and slip concentration phenomena not ocur in the boundary of .betha. phase.

낙하 충격을 받는 다점 구속 장치를 착용한 헬기 승무원의 상해도 평가에 관한 연구 (A Study on the Injury Assessment of Helicopter's Crew with Multi Point Restraint System under Drop Impact)

  • 이중현;이영신
    • 대한기계학회논문집A
    • /
    • 제33권6호
    • /
    • pp.590-599
    • /
    • 2009
  • In this paper, a method of modeling seat belts on crew seat during dynamic seat testing was studied. The body segments of the occupant were modeled with joints. The joints consisted with various stiffnesses, dampings, and frictions. Three types of seat belt restraint systems were investigated. The analysis for on the injury assessment of helicopter's crew under drop impact was conducted. The effectiveness of the seat belt system for crashworthiness and safety was evaluated. As the results of impact analysis, head, neck and spine of the crew can be easily damaged in the vertical direction more than the longitudinal direction. Based on the verified model, behavior of human body was studied with three-point restraint systems. The displacement and injury level of the 12-point restraint system was the smallest.

사격시험 및 인체구조해석 (Filing Experiments and Structural Analysis of Human Body)

  • 이세훈;최영진;최의중;체재욱;이영신
    • 대한기계학회논문집A
    • /
    • 제31권7호
    • /
    • pp.764-776
    • /
    • 2007
  • On the human-rifle system, the human body is affected by the firing impact. The firing impact will reduce the firing accuracy and change the initial shooting posture. Therefore the study of biomechanical characteristics using human-rifle modeling and numerical investigation is needed. The musculoskeletal model is developed by finite element method using beam and spar elements. In this study structural analysis has been performed in order to investigate the human body impact by firing of 5.56mm small caliber machine gun. The firing experiments with the standing shooting postures were performed to verify analytical results. The result if this study shows analytical displacements of the human-rifle system and experimental displacements of the real firing. As the results, the analytical displacement and stress of human body are presented.

부착력과 마찰력이 개재된 마이크로 입자 충돌 운동 (Microparticle Impact Motion with Adhesion and Frictional Forces)

  • 한인환
    • 대한기계학회논문집A
    • /
    • 제26권8호
    • /
    • pp.1698-1708
    • /
    • 2002
  • The main topic covered in this paper is that of the impact process, that is, where two bodies come into contact and rebound or stick together. This paper presents how to determine the rebound velocities of a microparticle that approaches a surface with arbitrary initial velocities and relate the impact process to the physical properties of the materials and to the adhesion force. Actual adhesion forces demonstrate a significant amount of energy dissipation in the form of hysteresis, and act generally in a normal to the contact surfaces. Microparticles must also contend with forces tangent to the contact surfaces, namely Coulomb dry friction. The developed model has an algebraic form based on the principle of impulse and momentum and hypothesis of energy dissipation. Finally, several analyses are carried out in order to estimate impact parameters and the developed analytical model is validated using experimental results.