• Title/Summary/Keyword: 충격흡수기

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The Impact fracture Behaviors of Low Density LD Carbon/Carbon Composites by Drop Weight Impact Test (낙하 충격 시험에 의한 저밀도 2-D탄소/탄소 복합재의 충격파괴거동)

  • 주혁종;손종석
    • Polymer(Korea)
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    • v.26 no.2
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    • pp.270-278
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    • 2002
  • In this study, the fracture behavior by low velocity impact damage and the tendencies of impact energy absorption were investigated. Low velocity impact tests were performed using a mini tower drop weight impact tester, and graphite powder, carbon black and milled carton fiber were chosen as additives. Addition of graphite powder increased the maximum load and maintained the stress long until the total penetration happened. At the content of 9 vol%, they showed the maximum of 42% improvement in impact strength compared composites containing no additives. At the test with low impact energy of 0.4 J, impact energy was consumed by delamination in the composite containing no additives, however, as graphite contents increased, the tendency of failure changed to the penetration of the specimen.

Manufacture and characteristics of arrester module using braided composite (직조형 복합재료를 이용한 피뢰기 모듈의 제조 및 특성)

  • Han, Dong-Hee;Cho, Han-Goo;Han, Se-Won;Hur, Chang-Su
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2004.05b
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    • pp.15-18
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    • 2004
  • 피뢰기에 뇌 또는 이상전압과 같은 정격이상의 고장전류가 유입되어 발생하게 되는 순간적인 열 충격과 내부압력 상승은 폭탄이 내부에서 터지는 것과 같은 엄청난 양의 충격에너지이다. 본 연구에 있어서 폴리머 피뢰기의 제조에 사용된 모듈용 브레이드 복합재료는 압력해소 및 폭발 비산하지 않도록 하는 기능을 수행하도록 설계되어있다. 기존의 폴리머 피뢰기에 적용된 복합재료보다 충격에너지를 흡수하는 구조물에 유리한 브레이드 복합재료를 피뢰기 모듈의 제조에 도입한 것은 매우 의미 있는 일이라 판단된다. 따라서 본 연구에서는 열경화성 브레이드 복합재료를 제조하기 위하여 프리폼을 먼저 제작한 다음 금형에 삽입한 후 진공상태에서 수지를 주입하여 경화시키는 RTM공법을 이용하였다. 본 연구의 목적은 브레이드 패턴 및 방압개소 설계 등의 기초적인 자료조사 및 실험을 통하여 폴리머 피뢰기의 폭발 비산을 방지할 수 있는 압력해소 성능을 위한 기초 자료를 확보하고자 하는 것이다. 브레이드 복합재료의 기본적인 경화거동을 등온 및 동적 DSC를 이용하여 고찰하였고, 기본적인 전기적 특성을 평가하였으며, 방압개소를 가진 폴리머 피뢰기 모듈의 고장전류시험시 예상되는 열 충격에 대한 성능을 검증하기 위하여 열팽창계수를 측정하였다.

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A Experimental Study to Understand of a Characteristics of a Piezo-Generator using Impact Energy (충격에너지를 활용한 압전 발전기의 특성을 이해하기 위한 실험 연구)

  • Lee, Jaejun;Moon, Hakyong;Kwon, Sooahn;Ryu, Seungki
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.31 no.5D
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    • pp.689-695
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    • 2011
  • In this paper, available power generation on the road from renewable energy technologies on how to use the piezoelectric effect has been studied. A lot of vehicles on road that can generate electricity using renewable energy technology as part of the external shock to convert the load into electrical energy using piezoelectric effect piezoelectric generator can be applied to road space. Piezoelectric power harvesting using piezoelectric ceramics for the development of impact load characteristics were tested as function of various experimental design such as generator design and array of piezo-ceramic. To design the piezoelectric generator, the characteristics of piezoelectric ceremic were compared depending on the type of impact load as function of impact load, shock-absorbing.

Dynamic Behaviors and Optimal Design of an Aircraft Nose Landing Gear using ADAMS (ADAMS를 이용한 항공기 전륜착륙장치의 동적거동해석 및 최적설계)

  • Kim, Sun-Goo;Kim, Cheol;Kim, Young-Man
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.7
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    • pp.612-618
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    • 2007
  • The dynamic behaviors of a KT-1 family aircraft nose landing gear have been analyzed and the optimal design of an aircraft shock absorber has been conducted to improve efficiency of shock energy absorption. The nose landing gear is modeled as a 2 DOF system using ADAMS and various operational and environmental landing conditions were considered. The results of dynamic simulation for various landing conditions agree well with experiments. Also the effect of parameters of a shock strut on the dynamic behaviors and on shock energy absorption of the nose landing gear has been evaluated for optimal design to define design variables. It has been found that the parameters of a shock strut such as oil-density and orifice area have more effects on dynamic behaviors than those of operation conditions. Optimal design is performed to maximize the efficiency of shock energy absorption using Feasible Direction Method. As a result the design values of the shock strut for maximum efficiency of shock energy absorption are derived and it turns out that efficiency and dynamic behaviors of the nose landing gear were improved by the optimal design.

A Basic Study on the Alternative Development of Piston for Shock Absorber (충격 흡수기 피스톤의 대체 개발에 관한 기초적 연구)

  • 김영호;배원명;임동주
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1995.10a
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    • pp.121-124
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    • 1995
  • This study is aimed at cutting down the cost, weight and improving process by replacing the traditional sintered piston of the shock absorber with engineering plastic piston by means of injection molding. To obtain the high mechanical properties, glass fiber material was selected adequately and forming analysis considering fiber orientation was made to remove the forming deficit fators and to construct the optimal runner system. In addition, structural analysis using commercial software MOLDFLOW was performed under near conditions in actual driving of automotive. The results from the internal pressure process test, oilproof test based on forming, structural and strength analysis shows that hydraulic close performance and damping force considering the out of roundness of shock absorber are relatively good.

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An analysis on the ground impact load and dynamic behavior of the landing gear system using ADAMS (ADAMS를 이용한 항공기 착륙장치 지상 충격하중 및 동적거동 해석)

  • Choi, Sup;Lee, Jong-Hoon;Cho, Ki-Dae;Jung, Chang-Rae
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.4
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    • pp.114-122
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    • 2002
  • The integration of the landing gear system is a complex relationship between the many conflicting parameters of shock absorption, minimum stow area, complexity, weight and cost. Especially ground impact load and dynamic behaviors greatly influence design load of landing gear components as well as load carrying structural attachment. This study investigates ground impact load and dynamic behaviors of the T-50 landing gear system using ADAMS. Taking into account for various operational/environmental conditions, an analysis of shock absorbing characteristics at ground impact is performed with experience derived from a wide range of proprietary designs. Analytical results are presented for discussing the effects of aircraft horizontal and vertical speed, landing attitudes, shock absorbing efficiency. This analysis leads us to the conclusion that the proposed program is shown to be a better quantitative one that apply to a new development and troubleshooting of the landing gear system.

Material Tests for Module Type Crash Cushion (모듈타입 충격흡수장치를 위한 재료실험)

  • Ko, Man-Gi;Kim, Kee-Dong;Sung, Jung-Gon;Kim, Jin-Man
    • International Journal of Highway Engineering
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    • v.10 no.1
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    • pp.87-95
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    • 2008
  • One way to shield an atypical structure to secure the occupant safety of an impact vehicle is to stack energy absorbing material modules around the structure. To be applicable to a cushion module, material must have enough energy absorbing capabilities while satisfying the safety requirements of the vehicle occupant. Static compression test of the potential materials gives a good indication which material is good for a slacking module. This paper presents the mechanical properties that a cushion material must have to satisfy the safety requirements. Static tests are performed for Quard-Guard system module, sand bag, recycled tires, Geo-Container, Geo-Cell and Expanded Polystyren (EPS) Blocks. Static test results are discussed and EPS block of $30kg/m^{3}$ density showed good potential for a cushion module. To check the dynamic effect of EPS block, drop tests have been made up to 35.6km/h impact speed. Drop test results are compared with static test results and no appreciable difference was found. To improve the EPS module property, making holes to the block is suggested and drop test are performed for the modified blocks. From the drop test results, design values are suggested.

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A Study on the Water Hammer Arrester Considering the Way of First Assessment Test (최초의 평가시험 방법을 고려한 수격흡수기의 장치에 관한 연구)

  • Yeum, Moon-Cheon;Han, Yong-Taek
    • Fire Science and Engineering
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    • v.29 no.1
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    • pp.53-59
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    • 2015
  • Water hammering created by an unsteady flow in pipeline systems can cause excessive change in pressure, vibration, and noise. So, water hammer analysis is very important for limiting the damage caused to pipeline, pump and valve systems by operation conditions. On the other hand, water hammer arrester has been manufactured and used in order to minimize the damage caused by water hammering phenomenon in domestic, and it has been produced and installed as the low cost-oriented because of being no separate standard in the meanwhile. Therefore, our research team investigated about the standardization of water hammer arrester performance through the various methods, such as test methods for verification of one pipe, assuming the occurrence of water hammer in a water-based fire extinguishing system, separated for opening impact pressure and shut off impact pressure and for a branch pipe in order to make guideline for water hammer arrester performance. And finally, verified the performance of the water hammer pressure as the simple mechanical way using the U-shaped pipe and a test weight, so KFI standards for the water hammer arrester could be established.

Evaluation of the Dynamic Characteristics of Rubber Structure under Impact Force (충격하중을 받는 고무구조물의 동특성 평가)

  • Kim, Wan-Doo;Kim, Dong-Jin;Lee, Young-Shin
    • Elastomers and Composites
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    • v.41 no.1
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    • pp.40-48
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    • 2006
  • Mechanical systems with rubber parts have been used widely in industry fields. The evaluation of the physical characteristics of rubber is important in rubber application. Rubber material is useful to machine component for excellent shock absorbing characteristics. The impact characteristics of rubber were examined by experimental and finite element method. The impact test was conducted with a free-drop type impact tester. The ABAQUS/Explicit was used for finite element analysis. In the finite element analysis, elastic modulus of rubber using impact force was used as dynamic modulus, which are measured and predicted with dynamic property test and WLF model. The analysis result was coincided with the experimental results.