• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.12
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• pp.758-764
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• 2019

The chassis of the Korean light tactical vehicle adopts a frame-on-body structure that uses lightweight design technology in terms of equipment operating characteristics. Military vehicles are operated in much harsher conditions compared to civilian vehicles, including mountainous terrain, especially steep slopes. Due to this characteristic, frame-welded cracks were found on some military vehicles. Therefore, in this paper, road damage analysis was conducted by identifying various roads including the military unit's road. The result confirmed that the operating environment of some military units' tactical road was much harsher than the endurance road test condition. A solution was derived through defect analysis, design review, and actual vehicle driving test. This study can be used as a reference by suggesting the development direction for the durability test of a new vehicle.

• Proceedings of the Korean Society of Food and Cookery Science Conference
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• 1993.11a
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• pp.377-377
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• 1993

• 한국무역상무학회:학술대회논문집
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• 2006.12a
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• pp.27-53
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• 2006

• Proceedings of the Korean Institute of Communication Sciences Conference
• /
• 1996.10a
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• pp.300-303
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• 1996

• Fire Protection Technology
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• s.39
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• pp.74-76
• /
• 2005

• Journal of Korea Fair Competition Federation
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• no.129
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• pp.34-43
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• 2006

• Proceedings of the Korean Institute of Communication Sciences Conference
• /
• 1996.10a
• /
• pp.293-296
• /
• 1996

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.21 no.6
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• pp.448-454
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• 2020

This study aims to determine the cause of structural defects occurring during aircraft operations and to verify the structural integrity of the improved features. The fracture plane was analyzed to verify the characteristics of the cracks and the fatigue failure leading to the final fracture was determined by the progress of the cracks by the repeated load. During aircraft operations, the comparative analysis of the load measurement data at the cracks with the aircraft design load determined that the measured load was not at the level of 30% of the design to be capable of being damaged. A gap analysis resulted in a significant stress of approximately 32 ksi at the crack site. Pre-Load testing also confirmed that the M.S. was reduced by more than 50% from +0.71 to +0.43, resulting in a sharp increase in aircraft load and the possibility of cracking when combined. Thus, structural reinforcement and the removal of the gap for aircraft cracking sites improved the defect. Based on the structural strength analysis of the improvement features, the bulkhead has a margin of about +0.88 and the fitting feature is about +0.48 versus allowable stress. In addition, the life analysis results revealed an improvement of approximately 84000 hours.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.11
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• pp.386-393
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• 2019

In this study, we investigated the cause of a voltage controller failure that occurred in the operation of a combat vehicle and attempted to establish a solution for the failure. The failure in the voltage controller was found to be related to thermal resistance, which could be identified by disassembly analysis and a high temperature operation test. Especially, in the disassembly analysis, there was damage caused by high temperature such as soot on the molding material and cracking of the resisters. In addition, in the high temperature operation test, the test results show that the internal temperature of the voltage controller was relatively higher than the external temperature. This means that the voltage controller failure could be attributed to the excessive heat and insufficient thermal resistance. In order to improve the thermal resistance of the voltage controller, several designs with changing circuits and structures were devised. Improvement of thermal resistance was verified by measuring reduction of internal temperatures in the high temperature comparison test.

• Information and Communications Magazine
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• v.32 no.5
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• pp.31-35
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• 2015

IoT 서비스 사업자, IoT 기기 공급업체 또는 산업분야별로 구축한 IoT 서비스가 파편화돼 가는 상황에서 IoT 플랫폼간 상호운용성(Interoperability) 관련 기술 개발의 필요성이 증대되고 있다. 본 논문에서는 IoT 서비스 플랫폼간의 상호운용성 및 IoT 디바이스간의 상호운용성을 개선하기 위한 플랫폼간 연동(Interworking) 기술 및 개방형 표준 플랫폼 기술 적용 방안을 제시하였으며 사용 편의를 위한 상황인식(Context-Awareness) 기술 구현안을 제시하였다. 본 논문에서는 모다정보통신이 개발한 oneM2M 국제표준 기반의 지능형 IoT 플랫폼인 OMNIPASS와 다양한 IoT 플랫폼 간의 상호연동성을 지원하는 IoT Gateway장치로서 Smart Brain을 소개하고 이를 통해 IoT 서비스의 발굴과 다양한 산업 응용 분야의 확산을 도모하고자 한다.