• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.6
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• pp.56-63
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• 2004

In this study, dynamic aeroelastic analyses of the canard with oscillating flap are conducted considering the effect of aerodynamic compressibility. The canard model considered herein is an all-movable type with a pitching axis on a canard-rotor-wing aircraft which was considered as one of the major UAV candidates under developing in Korea. The equivalent structural model is constructed based on the initial design data by the Korea smart UAV development center. Both the frequency and the time-domain aeroelastic analyses have been applied to practically conduct parametric studies on the effects of equivalent torsional stiffness. In the case of all-movable control surface with oscillating flap, the equivalent rotational stiffness of the pitch axes are important design parameters. The parametric results for the aeroelastic instability are practically presented.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.1
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• pp.238-244
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• 2017

A spindle with a built-in motor can be used to simplify the structure of a machine tool system, but the rotor inevitably has unbalanced mass. This paper presents an analysis of the dynamic behavior. The spindle was used in a CNC lathe and investigated using the finite element method and transfer matrices. The high-speed spindle can be very sensitive to the rotation of an unbalanced mass, which has a harmful effect on many machine tools. Thus, a balancing procedure was performed with a spindle-bearing system for the CNC lathe by numerical analysis. The balancing was performed through the influence coefficient method, and the whirl orbit radii before and after balancing were compared to evaluate the effects. The results show that the rotational speed of the spindle seriously affects the whirl responses of the spindle. The whirl responses were also affected by other factors, such as the unbalanced mass and bearing stiffness. The balancing of the assembled spindle model significantly reduced the whirl orbit magnitude.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.38 no.4
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• pp.289-309
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• 2014

A rotor blade is an important device that converts kinetic energy of wind into mechanical energy. Rotor blades affect the power performance, energy conversion efficiency, and loading and dynamic stability of wind turbines. Therefore, considering the characteristics of a wind turbine system is important for achieving optimal blade design. This study examined the general blade design procedure for a wind turbine system and aero-structure design results for a 2-MW class wind turbine blade (KR40.1b). As suggested above, a rotor blade cannot be designed independently, because its ultimate and fatigue loads are highly dependent on system operating conditions. Thus, a reference 2-MW wind turbine system was also developed for the system integrated load calculations. All calculations were performed in accordance with IEC 61400-1 and the KR guidelines for wind turbines.

• Proceedings of the Korean Society of Soil and Groundwater Environment Conference
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• 2006.04a
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• pp.266-269
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• 2006

지하수, 해수 혹은 지표수의 희토류원소의 분포도에 있어서 Eu과 Ce은 산화수의 변화에 따라 다른 희토류원소로터 벗어나게 되고, 이로이해 Eu과 Ce의 이상이 발생된다. 지표수와 지하수의 연계성을 밝혀내기 위해 희토류원소를 이용하여 전주-완주지역에서의 지표수와 지하수시료를 2002년부터 2004년까지 6차례에 걸쳐 채취하였다. 이중 2003년 8월까지의 시료는 2개기관에서 각각 희토류원소 함량을 측정하였다. 또한 대수층 구성암석과의 상관성을 밝혀내기 위해 동일한 지역에서 코어시료를 채취하였다. PAAS(Post Archean Australian Shale)로 규격화한 희토류 원소분포도에 의하면, 갈수기인 2002년 4월과 2003년 11월의 지표수와 지하수는 대체적으로 중희토류가 부화되었고, 아울러 강한 Eu의 정(+)의 이상과 Ce의 부(-)의 이상을 보여주었다. 그러나 갈수기가 끝난 2003년 6월과 장마가 끝난 직후인 2003년 8월의 시료에서는 대부분의 지표수와 지하수 시료가 Eu의 강한 부(-)의 이상을 보여주었다. 그리고 일부 시료에서는 Ce의 부(-)의 이상도 관찰되었다. 이와 같은 Ce과 Eu의 변화는 산화-환원작용의 영향을 받은 산화수(즉 Ce3+와 Ce4+, Eu2+와 Eu3+)의 변화에 의한 것으로 해석할 수가 있다. 뿐만 아니라, 본 연구결과에 의하면, 전주-완주 지역에서의 지표수와 지하수는 매우 밀접한 연관성을 갖고 있으며, 그 순환속도 또한 비교적 빠른 편으로 나타났다. 그리고 본 연구결과, 희토류원소는 지표수와 지하수의 연계성을 밝혀내는 데 있으며 매우 유용한 지시자임을 확인하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.12 no.4
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• pp.48-55
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• 2008

In this paper, numerical analysis of the surface gas temperature on turbine blades has been performed to investigate the temperature profiles characteristics of a partial admission supersonic turbine driven by high temperature and pressure gas of pyro-starter with two different types of turbine blade edge shape. In order to examine the surface gas temperature on turbine blades at initial starting, computations tlave been carried out at several turbine rotational speeds in the range of $0{\sim}10,000$ rpm for each type of turbine edge shape. "Sharp" edge and "Round" edge types were taken as the turbine edge shape factor. As turbine rotational speed increased, the average temperature of turbine blades was further decreased. It was also found that the surface temperature of turbine blades with a sharp edge was lower than round-type edge turbine blades.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2009.05a
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• pp.535-538
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• 2009

Auto Pilot is the system which move automatically the vessel through locating operation mode to automatic after entering operating course using a electronic chart or plotter. And water jet is the a propulsion system that make a power to push the vessel through spouting the accelerated water which is absolbed by the hole in the bottom of vessel. The water jet receive the effect of the depth of water lowly, it's acceletion efficiency is higher under high speed and have an advantage on vibrating and floating sound, so it's demand is increasing as new propulsion system. However, the signal systems of auto Pilot and water jet are defferant, we need the system to communicate between each system. We propose the interface system which communicate between Auto pilot and water jet efficiently in this journal.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.50 no.9
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• pp.599-608
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• 2022

Urban air mobility (UAM) equipped with rotor system is subject to ground effect at vertiport during takeoff and landing. The aerodynamic performance of the aircraft in ground effect should be analyzed for the safe operation. In this study, The ground effects on the aerodynamic performance and wake structure of the quadcopter electric vertical takeoff and landing (eVTOL) configuration equipped with coaxial counter-rotating propellers were investigated by using the lattice Boltzmann method (LBM). The influence of the ground effect was observed differently in the upper and lower propellers of the coaxial counter-rotating propeller system. There was no significant change in the aerodynamic performance of the upper propeller even if the propeller height above the ground was changed, whereas the averaged thrust and torque of the lower propeller increased significantly as propeller height decreased. In addition, the amplitude of the thrust fluctuation tended to increase as the propeller height decreased. The propeller wake was not sufficiently propagated downstream and was diffused along the ground due to the outwash flow developed by the ground effect. The impingement of the rotor wakes on the ground and a fountain vortex structure were observed.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.9
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• pp.92-100
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• 2017

The Helicopter MRA Control Rod System has the important function of controlling the speed, height, and direction of helicoptersby adjusting the main rotor disc. However, the ingress of water into the inner control rod can cause ice damage in the rod during winter operation and also corrosion;these defects need to be rectified. The water flowed into the control rod through the upper side space, and the rod was cracked during icing expansion occurring at low temperature. The corrosion occurred due to the lack of coating process during the manufacturing process. To resolve these problems, the upper rod was sealed to prevent water inflow and a coating process was added to prevent corrosion. These solutions were verified by awaterproof test and a salt fog test. The phenomena, causes and measures were reviewed and the methods of improvement were established and proven. This proposed technology to prevent water infiltration and corrosion will contribute to the safety of rotary wing aircraft.

• Journal of the Earthquake Engineering Society of Korea
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• v.13 no.2
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• pp.37-46
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• 2009

In this study, the seismic performance of the Buckling Restrained Knee Bracing (BRKB) system was evaluated through a pin-connected 1-bay 1-story frame. The BRKB system using a bolted channel section developed was composed of a steel plate as a load-resisting core member and two channel sections as a restrainment of the local and global buckling of the core plate. The main purpose of the BRKB system is to be used as an effective tool to re-strengthen/rehabilitate old low- and mid-rise RC frame buildings, which do not have enough seismic resistance to earthquake loadings. The main variables for the test specimens were the size of the core plates, stiffeners and the use of guide plates. The test results showed that the size of the core plate, which was the main element for the load-resisting member, was the most important parameter to achieve ductile behavior under tension as well as compression, until the maximum displacement exceed twice the design drift limit given by the AISC Seismic Provisions.

• Proceedings of the KWS Conference
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• 2010.05a
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• pp.66-66
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• 2010

국내 화력발전의 $CO_2$배출량을 크게 줄이고, 친환경, 그린 화력발전시스템을 위한 가장 효과적인 수단은 발전효율을 획기적으로 증대시키는 것이기 때문에 이를 목표로 한 기술개발은 경제적으로나 산업적으로 파급효과가 매우 크다. 발전효율 증대를 위한 핵심기술은 증기터빈의 성능향상이다. 현재 일본, 미국, EU 등 각국이 가장 관심을 가지고 기술개발에 심혈을 쏟고 있는 초내열, 내식 합금소재는 $700^{\circ}C$이상에서 기계적 성능을 보장할 수 있는 Ni기 합금개발이고, 현재까지 상당한 기술수준에 이르고 있는 것으로 파악되고 있다. 국내의 경우는 관련기술개발을 위해 연구가 진행되고 있으나, 기술적으로 아직 미흡한 수준이다. Ni기 초내열, 내식합금을 개발해서 그것을 화력발전용 증기터빈 부품, 특히 초내열합금 용접형 터빈로터 소재로 이용하기 위해서는 체계적이고 실용적인 연구를 통하여 용접형로타의 내구성과 신뢰성이 보장되는 최적 수준의 접합기술 개발이 선행되어야 한다. 따라서 본 연구는 선행연구로 $700^{\circ}C$이상 초내열/내식 Ni기 합금소재의 용접기술 개발을 위한 후보 소재 Alloy 617의 동종재료 용접 기술 개발을 목표로 한다. 본 연구는 Alloy617 12.6t 맞대기 이음으로 U그루브 내로갭 TIG용접을 하였다. 1pass 1layer 방식으로 총 8pass 8layer로 용접하였다. 전류 및 용접속도는 동일하게 두고 실드가스를 Ar 또는 Ar-$H_2$ 가스로 변경하여 시험하였다. Ar가스 TIG용접은 비드표면에 산화스케일이 생기고, 비드면이 거칠며 전체적으로 산화되었다. 반면에 Ar-$H_2$가스 TIG용접은 비드표면에 산화스케일이 없으며 표면이 미려하고 산화되지 않았다. 실드가스에 수소가스 첨가시 환원성가스로 역할을 하게 되고 이에 따라 용융지 표면에 산화피막을 제거하여 용접비드를 청정하게 하는 효과를 가진다.