• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2000.06a
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• pp.1192-1197
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• 2000

Piping systems of the power generating stations have been generally protected by hydraulic and mechanical snubbers which can allow large displacements arising from temperature change while those can reduce or absorb stresses due to vibrations. However these snubbers require amounts of budget for maintenance or replacement because of the leakage, lubrication and finally short life cycle. Recently the snubbers consisted of wire rope have been proved to reduce vibrations of piping systems. While the wire rope snubbers are free of maintenance such as leakage and lubrication, imported price are so high. Now it is necessary to design, manufacture and certificate these wire rope snubbers.

• Proceedings of the Korean Vacuum Society Conference
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• 2014.02a
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• pp.145.2-145.2
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• 2014

최근 반도체 산업의 급속한 발전으로 반도체 생산 설비 시설 또한 꾸준히 증설되어가는 추세이다. 이에 따라 반도체 산업의 핵심기술로 부각되고 있는 진공 기술은 다양한 응용목적을 위한 진공시스템 설계와 운영을 필요로 한다. 진공시스템의 알맞은 설계는 시스템 구성에 따른 진공특성을 예측하는 것이 중요하며 목적에 부합한 진공펌프를 선택하고 운영하여 최소비용으로 시스템 활용효율성을 극대화할 수 있는 설계를 해야 한다. 또한 공정의 저전력, 대유량화 추세에 따라 고유량 영역의 드라이펌프 부하 내구성 대응 요구에 부응하는 객관적 내구성평가의 정립 및 표준 측정 시험평가 방법의 필요성이 점차 대두되고 있는 경향에 있다. 본 연구에서는 드라이펌프의 공정현장 적응능력 평가를 위하여 최소 1시간에서 3시간동안 압력별 가스부하에 따른 드라이펌프의 실시간 특성을 관찰하였다. 실험은 1 mbar에서 최대 300 mbar까지의 연속적인 부하 조건에서 유량, 진동, 소음, 소비전력과 Sudden Vent Test를 실시간으로 측정하였고 드라이펌프의 특성 분석은 각 용량별 압력에 따른 유량, DP BP 소비전력, 소음, 진동, DP Body Temperature 등의 데이터를 Type에 따라 비교 분석하였다. 이에 부응하는 평가 장치 구축 및 데이터분석은 한국표준과학연구원 진공펌프 평가실험실에서 수행되었다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.11 no.10
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• pp.3633-3640
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• 2010

For a development of non-contact magnet gear which is magnetized as a helical shape, a method of 3-dimensional FEM analysis is used. An elementary technique required for magnetic property analysis and parts design about magnet gear is ensured. In order to test a performance of clean conveyor and turning device which is composed with magnet gear, a clean class 10 environment booth is used for a trial test. It is verified that the magnet conveyor can be acceptable under a condition of clean class 10 by a result of trial test about transfer speed, maximum torque permission, cleanness, maximum transfer weight, existence of hunting and degree of noise.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.113-113
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• 2013

최근 반도체 산업의 급속한 발전과 더불어 핵심기술로 부각되고 있는 진공 기술은 다양한 응용목적을 위한 진공시스템 설계와 운영을 필요로 한다. 이는 진공에 대한 기초지식과 이해가 요구되며, 설계제작 및 운영은 많은 시간과 큰 비용이 요구된다. 따라서 응용 진공시스템 제작에는 구성에 따른 시스템 진공특성을 예측하는 것이 중요하며 목적에 부합한 진공펌프를 선택하고 운영하여 최소비용으로 시스템 활용효율성을 극대화할 수 있는 설계를 해야 한다. 현재 반도체 및 디스플레이 공정의 저전력, 대유량화 추세에 따라 최대 3,000 m3/h급의 드라이펌프가 여러 공정에서 적용되고 있는 추세이다. 이에 대응한 고유량 영역의 드라이펌프 부하 내구성 대응 요구에 부응하는 객관적 내구성평가의 정립 및 표준 측정 시험평가 방법의 필요성이 점차 대두되고 있는 경향에 있다. 이러한 현실적인 요구 조건에 필요한 기본적인 평가로 압력대별 드라이펌프의 적응능력을 실시간 측정하였다. 실험 조건으로는 각 드라이펌프 용량별 N2 가스를 1 시간에서 3 시간동안 1 mbar에서 최대 300 mbar까지 연속적인 부하 조건에서의 유량, 진동, 소음, 소비전력 등을 실시간으로 측정하였다. 이에 부응하는 평가장치 구축 및 시험분석은 한국표준과학연구원 진공펌프 평가실험실에서 수행되었다.

• Journal of Environmental Impact Assessment
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• v.20 no.6
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• pp.787-795
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• 2011

Noise barrier is generally used with welding of joint rail for railway noise reduction in our country. But the noise barrier for high speed railway has weak point in low frequencies about 315Hz band. In this study, For developing of Interference-type Noise Reduction Device(INRD), acoustic analysis were performed using commercial software. For verifying the improvement in the noise reduction, noise measurement before and after installing of INRD were performed in Anechoic Chamber. From these acoustic analysis and noise measurement, it was known that developed INRD has a good noise reduction performance and can be used efficiently with conventional noise barrier.

• Proceedings of the Korean Reliability Society Conference
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• 2006.05a
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• pp.362-370
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• 2006

차량의 충격과 진동을 완화하고 링크의 조정역할을 하는 Rubber Bushing제품의 내구성이 약하게 되면 Control arm에서의 이탈사고나 차량의 떨림, 소음으로 인한 고객 불만이 발생하게 된다. 따라서, 국내외 시장에서의 경쟁력 향상을 위해 Rubber Bushing에 대한 내구성, 정특성, 동특성의 개선을 위한 기술의 개발이 요구되고 있다. 본 연구의 목적은 Rubber Bushing을 개발하는데 있어서 종전의 재료설계, 형상설계 및 공정설계에 대한 분석을 행하고, 실험계획법(DOE)을 활용하여 가장 적은 샘플의 시험으로 최적의 설계요소를 찾아내는 방법을 연구하는데 있다. Bushing의 품질특성이 재료, 형상 및 공정에서 어떠한 조건을 가질 때 특성치가 가장 높은 바람직한 반응을 얻을 수 있는 가를 연구하여 최적반응 조건을 결정하고자 한다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.9
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• pp.493-501
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• 2016

In this study, core technologies of a traction system on a mountain tram operating on the track of mountain road full of sharp curves and steep gradients were developed. In domestic mountain resort areas, sometimes the transportation service is not provided in winter because of ice and heavy snow on roads, so a mountain railway service independent of the climate and geographic conditions is needed. A traction system was designed taking into account of the power of a traction motor to climb the gradient of 120 ‰, which is common in domestic mountainous areas. and power transmission system was designed to consider the installation space for the traction system. In addition, a reduction gear and a propeller shaft were developed. An elastic pinion was developed and applied to the rack & pinion bogie system for steep gradient so that noise and vibration generated by contact between the steel gears could be reduced. Impact comparison tests showed that the vibration level of the elastic pinion is one-third lower than that of previous steel pinion. Independent rotating wheels and axles were developed for the bogie system to operate on the sharp curve of a 10 meter radius. In addition, the band braking system was developed to enhance the braking force during running on the steep gradient. A test for the braking force showed it exerts the required braking force. The performance of the developed core components were verified by the tests and finally they were applied to the bogie system running on the track of steep gradient and sharp curve.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.2
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• pp.127-134
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• 2020

High supersonic aircraft are exposed to high temperature environments by aerodynamic heating during supersonic flight. Thermal protection system structures such as double-panel structures are used on the skin of the fuselage and wings to prevent the transfer of high heat into the interior of an aircraft. The thin-walled double-panel skin can be exposed to acoustic loads by supersonic aircraft's high power engine noise and jet flow noise, which can cause sonic fatigue damage. Therefore, it is necessary to examine the behavior of supersonic aircraft skin structure under thermal-acoustic load and to predict fatigue life. In this paper, we designed and fabricated thermal-acoustic test equipment to simulate thermal-acoustic load. Thermal-acoustic testing of the titanium specimen under thermal-acoustic load was performed. The analytical model was verified by comparing the thermal-acoustic test results with the finite element analysis results.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.3
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• pp.129-136
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• 2020

A Cut Out Switch (COS) is used for line protection and pole transformer protection in power systems. The COS used to protect the pole transformer is installed on the power side of the pole transformer to protect the electric equipment from fault currents. The COS is composed largely of a body and a fuse holder, and when the fault current is energized, the element of the fuse link in the fuse holder is melted to block the fault current. The arc generated when the COS fuse link is blown causes fire and noise, causing discomfort to residents in the surrounding area, and the arc flame can cause secondary damage to the peripheral device. In this study, a current-limiting COS fuse with improved overcurrent blocking performance rather than explosion type was developed to solve the arc and noise problems during COS operation. The overcurrent breaking performance of the current-limiting COS improves the reliability by developing a striker and COS fuse bracket. In addition, this study aimed to verify the performance of the developed current-limiting COS fuse through a test at an authorized institution.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.17 no.12
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• pp.1152-1160
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• 2007

In this paper we deal with a design of integral sliding mode controller to reject the disturbance force acting on the suspension system in the magnetically levitated system which is propelled by the linear induction motor. The control scheme comprises an integral controller which is designed for achieving zero steady-state error under step disturbances, and a sliding mode controller which is designed for enhancing robustness under plant uncertainties. A proper continuous design signal is introduced to overcome the chattering problem. The disturbance force produced by the linear motor is formularized by using a curve fitting of the experimental raw data. Computer simulations show the effectiveness of the designed integral sliding mode controller to reject the disturbance force.