• Journal of the Korean Society for Precision Engineering
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• v.16 no.10
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• pp.17-24
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• 1999

본 논문에서는 새로운 적응 퍼지 슬라이딩 모드제어 방법을 제시하였다. 제어기는 정확한 수확적인 모델이 없이도 점근적으로 시스템을 안정화시킬 수 있으며 적분항을 포함시킴으로서 정상상태에서의 오차를 좀 더 줄일 수가 있다. 직접구동모터는 감쇄기어가 없어서 부하나 외란 토크의 변화에도 모터 역학에 직접적으로 많은 영향을 줄 수가 있다. 제어기의 실제성능을 확인하기 위하여 불확실한 부하나 변소를 갖는 직접구동모터의 위치제어에 적용하였다.

• 한국신재생에너지학회:학술대회논문집
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• 2006.06a
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• pp.315-318
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• 2006

포항풍력에너지연구소에서는 에너지 관리공단의 지원으로 2004년부터 풍력터빈 KBP-2000M에 사용될 발전기를 개발해 오고 있다. KBP-2000M에 사용되는 발전기는 기어비가 24인 기어박스를 가진 가변속도형식의 발전기이다. 발전기의 직경은 1.87m 이고 축 방향의 길이는 1.288m 로 영구자석을 사용하여 여자하는 형식으로 설계되었다. 이러한 설계는 풍력발전기에서 요구하는 주요 요구조건인 고효율, 고 신뢰성을 만족시키기 위해서 매우 중요하다 이 보고에서는 발전기의 물리설계에서 얻어진 사양을 기준으로 하여 열 해석에서 얻어진 열 손실을 이용하여 냉각시스템 설계를 하였으며 펌프 및 라디에이터 선정에 관해서 논의한다.

• Proceedings of the KIEE Conference
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• 2015.07a
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• pp.746-747
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• 2015

전동기와 부하시스템은 직결, 혹은 커플링을 통하여 연결이 된다. 이때의 동력을 전달하는 커플링, 기어, 벨트 등의 특성에 따라 전달되는 토크의 특성이 달라진다. 본 논문에서는 동력 축과 부하 축을 기구적으로 분리가 가능한 영구자석 커플링을 적용한 구동 전동기-부하시스템에 축계 시스템 해석을 위하여 유한요소 해석을 통하여 비틀림 각도 변화에 따른 전달 토크를 얻고, 이를 활용하여 기구 해석 모델에 적용해 보고, 전동기-부하 시스템의 토크 변동 가능성에 대해 알아본다.

• Proceedings of the Korea Information Processing Society Conference
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• 2023.11a
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• pp.748-749
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• 2023

본 논문은 평탄한 지형뿐만이 아닌 턱과 계단 같은 비평탄 요소가 있는 지형에서도 주행이 가능한 바퀴 구동형 지능 로봇 설계를 목적으로 지형 극복 기능을 구현하기 위한 구동 방식을 크랭크의 원리를 이용한 기어 구조를 이용했고, 지능로봇의 지능적 요소를 구현하기 위해 구성된 임베디드 시스템에 대해 정리한 논문이다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.11
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• pp.5392-5395
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• 2013

Application of electric wheelchair, sort of wheelchair which is playing important role in transporting patients and old people, has been increasing. In this study, we designed the electric wheelchairs' driving system. Using the multi-step gear, the driving system can get great power, even though the small capacity of motors. First, we designed the multi-step gear, test its bending strength and contact strength, as well as verified its performance. We installed 'B-type electric brake(Multiple plate clutch, Anti-magnetization) in same axle of the driving system, so it is possible to stop under huge torque and small size. Using this driving system of the multi-step gear which we designed, it's possible to improve driving gear efficiency 30% up and create the high-competitive electric wheelchair. And, it is easy to repair and control.

• Journal of KSNVE
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• v.9 no.3
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• pp.593-599
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• 1999

A rotordynamic analysis is performed with a motor-bull gear rotor system supported on two partial bearings, which is intended to drive a high-speed turbo-chiller compressor impeller shaft through its built-in pinion gear. The motor-bull gear rotor system has a rated speed of 3,600 rpm, and is modeled utilizing the finite element method for analysis. As loadings on the bearings due to the gear action are significant in the system considered, each resultant bearing load is calculated statically by considering the generalized forces of the gear action as well as the rotor itself. The two support partial bearings are designed to take their varying loads along with their varying load angles, and they are also analyzed to give their rotordynamic coefficients. Then, a complex rotordynamic analysis of the motor-bull gear rotor-bearing system is carried out to evaluate its whirl natural frequencies and mode shapes and unbalance responses under various loading conditions. Results show that the bearings and entire rotor system are well designed regradless of operating conditions, i.e., loads and operating speeds.

• Journal of Aerospace System Engineering
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• v.13 no.4
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• pp.66-73
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• 2019

The objective of this study was to evaluate the structural safety of the basic design for the linear actuator for the flap control of aircrafts. The kinetic behavior of the linear actuator was determined using the multi-body dynamics (MBD) analysis, and the contact force was calculated to be used as input data for the structural analysis based on the finite element analysis. In the structural analysis, the thermal and static behaviors of the linear actuator satisfying the designed velocity were examined, and the structural safety of the linear actuator evaluated. Moreover, the dynamic behaviors of the key components of the linear actuator were investigated by the modal analysis. The actuation rod linearly moved with about 5 mm/s when the motor operated at 225 rpm and the maximum contact force of 32.83 N occurred between two driving gears. Meanwhile, the structural analysis revealed that the maximum thermal and static stresses were 1.57% and 78% of the yield strength of steel, respectively, and they were in a safe range of the structure. In addition, the linear actuator for the basic design is stable to the resonance by avoiding the natural frequencies of the components.

• Journal of Drive and Control
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• v.16 no.2
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• pp.15-21
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• 2019

In this study, the maximum system efficiency of the electro-hydrostatic actuators was experimentally investigated, where small size external gear pumps with volumetric displacement under 1.3 cc/rev were combined with a 400W servomotor as the prime mover. Since the efficiency data of the servomotor, gear pumps and hydraulic cylinder were not provided by the suppliers, experimental apparatuses for their efficiency measurement were extra built up. When a gear pump with a volumetric displacement of 1.27cc/rev was used on an electro-hydrostatic actuator system, the maximum system efficiency was not higher than 70%. This was because the most effective operation ranges of the motor and pump did not coincide each other. In order to match their operation ranges as one of the most crucial design factors, a speed reduction mechanism can be used, such as a timing belt. It was shown in the study that the maximum system efficiency could be increased from 70% to 76% in that way.

• Proceedings of the KIPE Conference
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• 1997.07a
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• pp.449-453
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• 1997

이 논문은 초음파모터를 이용한 직접구동방식의 전완로봇 개발에 관해서 논하였다. 기어 감속 없이 느린 동작하에서 큰 힘을 제공하기 위해 진행파형 초음파모터를 액츄에이터로 사용하였다. 이 시스템에서는 환경과의 상호작용력에 의한 힘 피드백 제어는 사용하지 않고, 위치 정보만을 사용하였다. 크랭크 회전같은 접촉작업과 핑거의 협력작업에 대한 실험을 고찰하였다.

• Aerospace Engineering and Technology
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• v.7 no.1
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• pp.49-60
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• 2008

In this technical paper, summarization of developmental results for the tilt-rotor SUAV Drive System being developed in the Smart UAV Development Center is carried out in view of design and analysis for the major components. The Drive System driving for the Rotor System of the SUAV is composed of very precise and advanced equipments, and also the applied technologies for development of the system had not ever experienced in the Korea. Therefore the collaboration study with an advanced company (EATI) in the USA performed in order to develop the SUAV Drive System.