• Transactions of the Korean Society of Mechanical Engineers A
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• v.34 no.1
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• pp.111-116
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• 2010

To improve occupants' safety in an emergency, crashworthy design is necessary to rotorcraft design and development. Especially, landing gear has the important role for crashworthy design because landing gear absorbs relatively large energy for the crash landing. In addition, military specifications require failure of landing gear shall not increase danger to any occupants by penetration of the airframe. To meet the specification requirements, crashworthiness device like failure mechanism should be prepared so that landing gear is collapsed safely and doesn't penetrate the airframe. In this study, design and design development test of the failure mechanism which is necessary for the rotorcraft landing gear was performed. First, collapse scenario was determined for the landing gear not to penetrate the airframe. Then, the failure pin which is the most important part of the failure mechanism was designed with 2 strength range in order to meet design criteria. Finally, design of the failure mechanism was verified successfully by design development test.

• Proceedings of the KSME Conference
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• 2008.11a
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• pp.497-501
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• 2008

To improve occupants' safety in an emergency, crashworthy design is necessary to rotorcraft design and development. To improve crashworthiness capability, most of the crash energy should be absorbed by rotorcraft and the energy transmitted to the occupants should be minimized. To absorb the crash energy efficiently, the individual energy attenuation provided by landing gear, structure, fuel tank and seats should be considered totally. Especially, landing gear has the important role for crashworthy design because landing gear absorbs relatively large energy for the crash landing. In addition, military specifications require failure of landing gear shall not increase danger to any occupants by penetration of the airframe. To meet the specification requirements, failure mechanism should be prepared so that landing gear is collapsed safely and doesn't penetrate the airframe. In this study, design of failure mechanism which is necessary for the rotorcraft landing gear was performed and the results were presented.

• Proceedings of the Korean Information Science Society Conference
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• 2002.04b
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• pp.115-117
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• 2002

메모리 기술의 발전은 주기억장치 데이터베이스가 널리 사용될 수 있는 토대를 마련하였다. 주기억장치 데이터베이스에서는 주기억장치의 휘발성으로 인해 시스템이 파손될 경우 모든 데이터들을 잃어버리게 되므로 데이터베이스를 일관된 상태로 복구시켜주는 회복기법이 매우 중요하다. 본 논문에서는 비휘발성 메모리이면서도 RAM과 같이 빠른 접근속도를 가지는 FRAM과 같은 고성능 비휘발성 메모리를 이용하여 그림자 갱신과 로그 기반 백업을 실시함으로써 시스템 파손 후, 마른 복구를 제공하면서도 기존의 로그 기반 백업이 가지는 문제점을 해결하는 회복기법을 제안한다.

• Journal of the Korea Institute of Building Construction
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• v.10 no.1
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• pp.65-72
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• 2010

The failure of expansion joints for bridges generally occurs in non-shrinkage mortar another problem is the release of anchors in expansion joints due to the impact and vibration that occurs when cars are driving over a bridge. In this study, to overcome the failure of expansion joints that is related to the failure of non-shrinkage mortar, an elastomeric mortar has been developed. The elastomeric mortar has a highly developed pull-out capacity compared with that of non-shrinkage mortar. Moreover, an anchor system that can be changed easily and prevent the fracture of expansion joints has been developed.

• Proceedings of the Korea Concrete Institute Conference
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• 2008.11a
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• pp.793-796
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• 2008

The failure of expansion joint for bridge is generally occurred on the non-shrinkage mortar and other problem is the release of anchors in expansion joint due to the impact and vibration during the driven car on the bridge. In this study, to overcome the failure of expansion joint by the failure of non-shrinkage, the elastomeric mortar is developed. The pull-out capacity developed elastomeric mortar compared with that of non-shrinkage mortar. Moreover the anchor system which can be change easily and prevent a fracture of expansion joint is developed.

• Journal of Aerospace System Engineering
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• v.12 no.2
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• pp.59-65
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• 2018

The landing gear (L/G) handle of an aircraft is an essential piece of equipment for aircraft take-off and landing. The bracket in the landing gear handle was fractured during a vibration test when developing the landing gear handle. This paper summarizes the vibration test procedures performed during landing gear handle development. A cause analysis, design improvements, and verification results of the fault in the vibration test are also provided.

• Proceedings of the Korea Concrete Institute Conference
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• 2008.11a
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• pp.645-648
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• 2008

The expansion joint is an important part of the bridge, but the failure is occurred on the non-shrinkage concrete which is connected to the slab of the bridge and the expansion joint, and the other problem is the release of anchors in expansion joint due to the impact and vibration during the driven car on the bridge, especially an overloaded car. In this study, to overcome the failure of non-shrinkage of concrete, high impact resisting mortar is developed. The high impact resisting mortar shall be a polyurethane material compounded with an aggregate system to develop excellent flexibility characteristics, high load bearing capacity.

• The Journal of the Korea institute of electronic communication sciences
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• v.8 no.6
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• pp.815-822
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• 2013

In this paper, the research is to develop a system that can detect the breakage of the rubber belt conveyor system in the transport of the raw materials required for the operation of logistics. We are to develop a system that can detect the breakage of the belt due to the electronic system of belt breakage occurs by placing the material on the inside of the belt, electric induction to minimize the damage of the belt. The belt repair costs, or reorder the steps of the logistics transit time can be reduced. Induced in the coil, and belt embedded in the transmitted signal as a way to detect the breakage of the belt was to detect the damage of the belt by detecting the electrical phenomena induced in the coil at the receiving end.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.63-63
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• 2004

구동 및 동력 전달용으로 많이 쓰이는 기어장치는 최근 고속도비에서 사용이 증가함에 따라 다단기어장치의 설계에 대한 관심이 높아지고 있다. 하지만 다단 기어장치의 설계는 장치의 파손확률을 고려하지 않고 정적인 하중과 균일한 강도를 유지하는 차원에서 접촉해석과 강도설계 등이 주류를 이루었으며 대부분 설계자의 경험과 감각에 의해 시행착오적이고 반복적인 방식으로 이루어지고 있다. 또한 임의의 시간에서 다단 기어장치가 설계자의 의도대로 작동할 확률인 신뢰성에 대한 연구가 미흡하였다.(중략)

• International Journal of Highway Engineering
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• v.11 no.2
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• pp.167-174
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• 2009

The simulation of dynamic load was conducted based on surface profile on asphalt concrete pavement, vehicle speeds, and suspension types using a truck simulation program. The results of the simulated dynamic load based on different surface profile, vehicle speeds, and suspension types are analyzed. As pavement roughness and vehicle speed are increased, the dynamic load was increased. Walking beam suspension produces greater dynamic load than air spring suspension. Pavement damage index is calculated based on covariance of dynamic load and Paris-Erdogan fracture parameter, n which is based on creep compliance tests of asphalt mixtures used in Korea. The higher covariance of dynamic load, confidence level, and fracture parameter are used, the greater pavement damage index is obtained. Specification of pavement roughness can be developed in various vehicle speeds and asphalt mixtures, and pay factor can be determined after constructing asphalt concrete pavement using pavement damage concepts.