• Journal of Aerospace System Engineering
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• v.18 no.3
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• pp.56-64
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• 2024

In this study, a drop impact tester was developed to comprehensively conduct basic testing and academic research on the drop impact characteristics of aerospace structures. A drop tester enables accurate assessment of the dynamic stresses and deformations that occur when an aircraft collides with the ground, thereby enabling the verification of important design factors, such as safety and mechanical strength. The drop tester consists of an electromagnet to attach and drop the test object, a crane to adjust the drop height of the test object, and a drop support structure for vertical drops. Numerical analysis of the drop test object for the test was performed, and basic tests were performed using the drop impact tester. Through the analysis and test results, the structural shape of the landing gear was analyzed, and the behavior of each part was evaluated.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05a
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• pp.258-263
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• 1998

원자력 발전소의 제어봉 낙하 시간 측정 시험은 원자로 비상 정지 명령에 따른 제어봉의 낙하 속응성이 지침서의 제한치 이내에 있는지를 주기적으로 확인함으로써 제어봉의 원자로 안전 운전 및 정지 기능을 확인하는 중요한 시험이다. 현재 고리2호기를 비롯한 WH형 발전소들은 제어봉이 디지틀 제어봉 위치 지시(DRPI) 코일속을 낙하할 때 유기되는 전압을 검출하여 제어봉 낙하 시간을 측정하는 방법을 사용하고 있다. 이 방법은 제어봉을 뱅크별로 인출한 후 하나씩 개별 낙하시키기 때문에, 제어봉 낙하 시간 측정 시험에 많은 시간과 다수의 인력이 소요되며, 측정시 격납용기내에 작업자가 장시간 체류해야 하는 단점이 있다. 이러한 DRPI 신호 이용 제어봉 낙하 시간 측정 방법의 단점을 보완하여 제어봉 구동 장치(CRDM)내 이동권선 신호를 이용하는 다중 낙하 방식의 새로운 측정 방법을 제안하고, 측정 장치를 개발하였다. 개발된 제어봉 낙하 시간 측정 장치를 이용하여, 고리2호기 제어봉 낙하 시간 측정 시험시 기존의 방법과 병행 측정 시험을 수행하고 그 결과를 비교 검토하여 충분히 정확하게 제어봉 낙하 시간을 측정할 수 있음을 보였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.11
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• pp.1121-1125
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• 2008

A development of landing gear drop test rig system for a small aircraft was studied and presented in this paper. Hydraulic actuators were considered in order to operate test system automatically and the wire winch system was applied to keep safety of test operators. This rig system was manufactured after checking the structural stability. Friction force measurement and drop velocity evaluation tests were done to confirm the confidence of test system. As a results of evaluation tests, it was confirmed that developed landing gear drop test system was adaptable.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2012.06a
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• pp.282-283
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• 2012

국제표준규격(ISO 12215-5) 및 국내 플레저보트 검사지침의 개정에 따라 길이 6미터 미만의 플레저보트의 낙하시험에 의한 강도시험기준을 적용 가능하게 되었다. 하지만 현재 낙하시험은 자유낙하 시 내력 및 외력에 의한 선체 내부의 찌그러짐, 크랙, 박리, 파손 등을 육안으로 검사하는 방법으로 시험결과의 정량적인 판단이 이루어지지 않고 있다. 따라서 본 연구에서는 레저선박의 낙하시험을 위한 시스템 및 운용프로그램을 개발하여 플레저보트의 구조안전성의 정량적 평가가 가능한 시스템을 개발하고 다단 롤포밍 기법을 적용한 5m급 알루미늄레저보트에 적용하여 시스템의 성능을 검증하였다.

• Journal of the Korean Society of Marine Environment & Safety
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• v.18 no.4
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• pp.365-370
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• 2012

International Organization for Standardization has recently published ISO 12215-5 which is the small craft-hull construction and scantling. According to ISO 12215-5 AnnexB, the scantling determination can be accomplished by drop test for craft with a length $L_H$ of 2.5m up to 6m and single-skin construction. The current method, however, of visual test has the issue where it is difficult to make an objective evaluation of ship body strength. In this study, in order to develop an evaluation system that can make a quantitative evaluation of the drop test of leisure boats, the domestic/foreign regulations on drop test of leisure boats are analyzed and the drop test evaluation system is designed, and the system applicability is reviewed through 5-meter level aluminum ship, and the issues incurred by the state of the ship and the posture while dropping were checked.

• Proceedings of the Korean Radioactive Waste Society Conference
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• 2005.11a
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• pp.339-347
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• 2005

A type IP-2 transport package should prevent a loss or dispersal of the radioactive contents and a more than $20\%$ increase in the maximum radiation level at any external surface of the package when it were subjected to the drop test under the normal conditions of transport. If a shielding thickness of IP-2 transport package is thick, a bolted lid type may prevent a loss or dispersal of the radioactive contents than the door type of ISO containers which are generally used as a type IP-2 transport package. In this paper, to evaluate the effect of drop directions on the bolt tension and the coherence of a bolt, the drop tests of preliminary small model are tested and evaluated for seven directions before the drop test of a type IP-2 transport package with a bolted lid type under the normal conditions of transport. Seven drop directions which are a bottom-vertical drop, a lid-vortical drop. a horizontal drop and four corner drops have been carried out. Using a force sensor, the bolt tension during the drop impact is measured. The coherence of bolt is evaluated by the difference between the fastening torque of bolt before a drop test and the unfastening torque of bolt after a drop impact.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.8
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• pp.681-688
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• 2021

This paper considers the trajectory and impact point dispersion analysis of the test launch vehicle (TLV). The analysis, which performed before and after its flight test on November 28, 2018, is described and verified by comparing with the flight test results. The six degree-offreedom (DOF) simulation is used to compute the dispersion of the trajectory, attitude, and impact point, where the launch vehicle performance variations and wind effects during the atmospheric phase are included. The impact area to guarantee the flight safety is determined using the results of the dispersion analysis. The flight test results confirm that the safe flight of TLV is performed within the predicted dispersion boundary.

• Proceedings of the KIEE Conference
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• 2009.07a
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• pp.2079_2080
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• 2009

MEMS 기술을 이용한 다양한 센서의 개발과정에서 신뢰성 확보는 매우 중요한 문제이며, 여러 가지 신뢰성 항목 가운데 낙하시험은 가장 기본이 되는 항목이다. 단시간 내에 낙하에 대한 내충격성을 확보하는 MEMS 센서를 개발하기 위해 본 논문에서는 FEA와 high-level 모델을 결합한 낙하시험 모의진단법을 제안하였다. 제안된 모의진단법을 통해 MEMS 소자에서의 최대응력과 응력분포, 최대변위, 그리고 낙하시의 과도응답과 오신호 등의 결과를 확보할 수 있으며 이들을 토대로 MEMS 소자에서의 취약부위를 파악하고 이를 보완할 수 있으며 낙하시의 오동작을 제거하도록 신호처리 회로 등을 보완할 수도 있을 것이며 이를 통해 단시간 내에 최소의 비용으로 내충격성을 확보한 MEMS 센서를 개발하는 것이 가능해질 것이다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.5
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• pp.24-29
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• 2004

In this paper, we summarize the results of free drop wind tunnel test, separation analysis and flight test in order to verify the safety during the separations of an external fuel tank and the LAU-131 rocket launcher from XKO-l. The wind tunnel test was conducted to show the safety in free drop of the stores and to gather the trajectory data for fine tune of MSAP(Multi-body Separation Analysis Program). The enhanced MSAP was then used to predict the trajectories of the stores with and without the ejector forces. A correlation of MSAP results for free drop case was also made to show the safety of jettison with the free drop type bomb rack. Moreover, the flight test was conducted. and its results were compared to analysis results. Finally, the safe jettison boundary was determined from the flight test.

• Proceedings of the KAIS Fall Conference
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• 2011.12b
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• pp.631-634
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• 2011

항공기용 착륙장치의 완충기 충격흡수 성능은 해석 과정을 거쳐 예측한 값과 낙하시험을 수행하여 그 성능을 입증하여야 한다. 이는 미 연방 항공 규정에서 요구하고 있는 사항이다. 본 논문에서는 착륙장치 낙하시험을 위한 설비, 시험절차 및 시험방법과 낙하시험 수행 결과를 제시한다.