• 제목/요약/키워드: Free Drop Test

검색결과 86건 처리시간 0.043초

저중력 환경 모사를 위한 낙하 시험 방법 연구 (Investigation of Drop Test Method for Simulation of Low Gravity Environment)

  • 백승환;유이상;신재현;박광근;정영석;조기주;오승협
    • 한국추진공학회지
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    • 제25권4호
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    • pp.78-87
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    • 2021
  • KSLV 상단의 임무 다각화를 위해서는 저중력 환경에서 액체 추진제의 거동을 정확히 파악하고 있어야 한다. 지상에서 저중력 환경을 모사하는 방법은 자유낙하 방법이 있지만, 공기저항이 항상 동반된다. 공기 저항을 제거하기 위하여 공기 저항 차단캡슐을 이용한 낙하 시험을 진행하였다. 공기 저항 차단캡슐 내부에 시험체를 위치하고 7 m 높이에서 1.2초 동안 낙하하여 시험체의 저중력 환경을 조성하였다. 낙하하는 동안 0.01 g 이하의 중력가속도를 측정하였으며 지표면에 도달하기 전 최소 가속도는 약 0.005 g였다. 추후 낙하 높이 및 낙하 시간이 증가한다면 개선될 수 여지가 있다.

드럼 세탁기 포장재 낙하해석 및 완충 특성 (Drop Analysis of a Package and Cushion Performance of Drum Washing Machine)

  • 김창섭;배봉국;성도영
    • 대한기계학회논문집A
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    • 제34권11호
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    • pp.1733-1740
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    • 2010
  • 대형 드럼세탁기의 낙하 충격에 대한 포장재의 동적 거동 분석을 수행하였다. 해석에는 충격 해석에 널리 쓰이고 있는 LS-DYNA를 사용하였으며, 자유 낙하 시의 충격 가속도와 유효 응력, 그리고 고속 카메라를 통한 포장재 압축 변형 비교를 통해 해석 결과의 신뢰성을 검증하였다. 완충 특성 및 포장재 구조 에 대한 파라미터 분석을 통해 기존 포장 구조에 대한 설계 개선안을 도출하였으며, 유통 시험을 통해 유효성을 검증하였다. 본 연구에서 사용한 해석 기법 및 분석 방법 등을 통해, 향후 드럼 세탁기의 완충 성능 및 재료비 개선에 효과적으로 기여할 수 있을 것으로 기대된다.

OSP.ENIG 표면 처리된 기판과 Sn-3.0Ag-0.5Cu 솔더 접합부의 낙하충격 신뢰성 평가 (Drop reliability evaluation of Sn-3.0Ag-0.5Cu solder joint with OSP and ENIG surface finishes)

  • 하상옥;하상수;이종범;윤정원;박재현;추용철;이준희;김성진;정승부
    • 마이크로전자및패키징학회지
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    • 제16권1호
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    • pp.33-38
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    • 2009
  • 전자 기기 제품들이 소형화 및 휴대화 되면서 낙하충격 신뢰성에 대한 관심이 높아지고 있다. 본 연구에서는 대표적인 무연솔더인 Sn-3.0Ag-0.5Cu 솔더를 이용하여 ENIG (Electroless Nickel Iimmersion Gold), OSP (Organic Solderability Preservative) 표면 처리와 등온 시효 시험 (High Temperature Storage test)에 따른 보드 레벨 패키지 (board level package)의 낙하충격 신뢰성 (drop reliability) 시험을 수행하였다. 또한 충격 조건을 변화시켜 시편에 가해지는 가속도 (G:acceleration)와 충격 지속 시간 (pulse duration)에 따른 신뢰성을 평가하였다. 기판의 strain측정 결과 중앙 부위가 가장 응력이 컸으며, 충격가속도에 비례하여 응력이 증가하였다. 시효 처리 전에는 OSP처리된 기판이 다소 우수한 신뢰성을 보였지만, 시효 처리후에는 ENIG기판에서 신뢰성이 우수하였고, 반대로 OSP는 감소하는 경향을 보였다. OSP의 경우 과도한 금속간화합물 (intermetallic compound)의 성장으로 인해 접합 계면에서 취성파괴 (brittle fracture)가 일어난 것을 관찰할 수 있었다.

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자동차 전장용 무연 솔더 기술 (Lead-free Solder Technology and Reliability for Automotive Electronics)

  • 이순재;정재필
    • 마이크로전자및패키징학회지
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    • 제22권3호
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    • pp.1-7
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    • 2015
  • In this study, properties of Pb-free solders for automotive electronics parts were discussed. Lead-free solders for electronics became important after RoHS (Restriction of the use of certain Hazardous Substances) to avoid environmental pollution. Also the growing electronic rate in automotive parts and ELV (End-of Life Vehicles) make Pb-free solder for automotive electronics to be inevitable trend. Definitely, Pb-free solder for automotive electronics should have good wettability, basic strength, but need more reliability than other solders, since it has harsh condition like high temperature, humidity and engine vibration. Thus, shear strength test, thermal shock, drop test and many others are needed to ensure the high reliability. This study describes the properties and requirements of Pb-free solders for automotive electronics.

항공기 내부무장 분리특성 분석을 위한 풍동시험연구 (An Experimental Study on Aircraft Internal Store Separation Characteristics)

  • 안은혜;조동현;김종범;장영일;정경진;김상진;이호근;류태규;정형석
    • 한국군사과학기술학회지
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    • 제20권1호
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    • pp.81-89
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    • 2017
  • This study investigates store separation characteristics of an unmanned aerial vehicle having generic stealth configuration over unsteady flow of an internal bay. Free-drop wind tunnel tests are conducted to simulate bomb releases from an internal weapons bay while high-speed camera images are taken. The images are analyzed to examine the effects of flow velocity, angle of attack, flap deflection and the ejector force application on the store separation trajectories. For the free-drop wind tunnel tests, Froude Scaling is applied to match the dynamic similarity for the bomb model, and the ejector force is simulated by using small pneumatic cylinders. The results indicate that the test bomb model safely separates from the internal bay at the given test conditions and configurations. It is also observed that the effects of the flow velocity and ejector force application have greater impacts on the separation trajectories than those of angle of attack and flap deflection.

항공기 탑재체의 분리 후 공력 특성 변화 효과 (Changing Effect in Aerodynamic Characteristics of a Captive Body Separated from Aircraft)

  • 조환기;이상현;강치행
    • 한국군사과학기술학회지
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    • 제14권3호
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    • pp.397-404
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    • 2011
  • The aerodynamic characteristics of a separated captive body in flow field around aircraft are studied to observe aerodynamic stability for safe separation from aircraft. Since the captive body separated from aircraft is initially exposed to unsteady flow pattern, the change of aerodynamic forces and moments should be measured to analyze how the flow pattern affects on the captive body at the vicinity of aircraft. Aerodynamic forces and moments of the separated captive body are measured at selected positions along predictable dropping trajectories. The measuring trajectories, generated by the free drop test of the dropping model in the wind tunnel, are consisted of 9 possible lines by free dropped trajectories. Experimental results show that the aerodynamic forces and moments are significantly varied with the distance between the captive body and aircraft. In conclusion, the change of aerodynamic characteristics within flow field around aircraft should be considered to simulate trajectories of the separated captive body from aircraft.

사용후 핵연료 수송용기의 수평낙하충격에 관한 연구 (A Study on the Side Drop Impact of a Nuclear Spent Fuel Shipping Cask)

  • 정성환;이영신
    • 대한기계학회논문집A
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    • 제21권3호
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    • pp.457-469
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    • 1997
  • A nuclear spent fuel shipping cask is required by IAEA and domestic regulations to withstand a 9m free drop condition. In this paper, the structural analysis under the 9m side drop condition was performed to understand the dynamic impact behavior and to evaluate the safety of the cask for 7 PWR nuclear spent fuel assemblies. The analysis result was compared with the measured value of the 9m side drop test for the 1/3 scaled-down model and the accuracy of the 3D analysis was confirmed. Analysis in accordance with the diameter of impact limiters for the proto-type cask were performed. Through the analysis, the impact behaviors due to the side drop and the effects dependent on the diameter of impact limiters were grasped. Maximum stress intensities on each part of the cask were respectively calculated by using the stress evaluation program and the structural safety of the cask was finally evaluated in accordance with the regulations.

무연솔더 내 마이그레이션 플럭스개발에 관한 연구 (A Study on Development of Flux to Restrict Occurrence of ion Migration in Lead-Free Solder)

  • 유동수;임재훈;우성우
    • 한국신뢰성학회:학술대회논문집
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    • 한국신뢰성학회 2005년도 학술발표대회 논문집
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    • pp.385-392
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    • 2005
  • The restriction of the use of hazardous substances in electrical and electronic equipment legislation mandates the substitution of lead and other hazardous substances in electronics products by July 2006. Due to this legislative pressure, the electronics industry is moving to adoption of lead free solders. In this paper, we investigated a flux to restrict generating electrochemical migration in lead-free solder. The lead-free solders used in this study were Sn-0.7Cu-0.01P and Sn-3.0Ag-0.5Cu. To measure the resistance of electrochemical migration, the dew-cycle test and water drop test were adopted. As the result, now flux having high durable of electrochemical migration was developed.

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A study on accumulated damage of steel wedges with dead-rise 10° due to slamming loads

  • Seo, Byoungcheon;Truong, Dac Dung;Cho, Sangrai;Kim, Dongju;Park, Sookeun;Shin, Hyunkyoung
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제10권4호
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    • pp.520-528
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    • 2018
  • This paper presents the results of experimental investigation on the elastic-plastic response of steel unstiffened wedges with dead-rise $10^{\circ}$ subjected to repeated impulsive pressure loadings. Repeated drop tests were performed with both wedge thickness and drop height varied. The pressure and histories were recorded during the tests and the permanent deflections were measured after every drop. Using the recorded test result, the effects of flexibility of wedges and repetition have been investigated. From the pressure history obtained from the tests the characteristics of the impulses were identified. Numerical simulations of the tests were made using the measured pressure history and the permanent deflection predictions were compared with those of the experiments.