• 전기의세계
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• v.17 no.2
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• pp.35-37
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• 1968

증기 Turbine plant의 제어방식은 점점 더 복잡하게 고도화하고 있으며 원심 또는 유압조속기등 Lever와 유압기구의 조합으로 구성된 기계유압식 Governor 대신에 전자유압식 Governor(Electro-Hydraulic Governor, EHG 일반적으로 광의의 의미로는 전자유압식제어장치 Electro-Hydraulic Control System이라함)의 개발에 주력하고 있으며 본보고서는 이에 대한 시험결과를 기술한 것이다. 본보고서는 산업용(자가발전용) 증기 Turbine의 전자유압식 Governor에 관한 것으로서 기계유압식에서의 복잡한 Lever 기구, Relay 장치등 기계부분의 전자유압화와 고압제어유의 채용및 이에 따르는 각부분의 Module화, Solid State화 및 소형 Unit화에 의하여 취급및 보수가 용이한 고성능의 제어장치를 개발하게 되었다. 특히 미국의 GE사에서 이에 대한 개발이 앞서 있으며 현재 100MW까지 약 30대가 실용화되고 있다고 한다. (이글은 일본화력발전지 1968년 1월 제136호에서 발췌한 글이다.)

• Proceedings of the KTCVS Conference
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• 1995.10a
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• pp.44-44
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• 1995

• Aerospace Engineering and Technology
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• v.7 no.1
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• pp.151-160
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• 2008

In this paper, the analysis results of synthetic resonance characteristics are described for the electrohydraulic thrust vector control actuation system. The synthetic resonance is induced by integration of position servo actuation system on the flexible launch vehicle mounting structure. The new resonance mode is synthesized due to composition of hydraulic resonance for electrohydraulic position servo system with inertia load condition and structural resonance for flexible mounting structure. This synthetic resonance can make stability of control system worse by feedback and amplification of control system. The exact nonlinear analysis model of this phenomenon is developed to predict and design a control algorithm for improvement characteristics. The DPF (Dynamic Pressure Feedback) control algorithm has been designed and has excellent resonance suppression capability.

• Aerospace Engineering and Technology
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• v.6 no.2
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• pp.164-170
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• 2007

In this paper, the development results of electromechanical TVC actuation system is described in the aspect of design, analysis, manufacturing and test. The kinds of prime power for TVC actuation system is classified by the variety of propulsion system of launch vehicle. The electric power by battery is the sole candidate for prime power of TVC actuation system at the view point of feasible domestic infra technologies for the present. The characteristic analysis study is performed between electromechanical and electrohydraulic actuation system with respect to power efficiency, performance and weight efficiency. The electromechanical actuation system has superiority of power and weight efficiency according to less opportunity of power conversion process.

• Aerospace Engineering and Technology
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• v.4 no.1
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• pp.162-170
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• 2005

In KSLV-I, actuation system for thrust vector control of kick motor was configured as electro-hydraulic servo actuation system and consisted of actuators, hydraulic power supply system, hydraulic power distribution system and control system. In case of hydraulic power supply system, we use EMDP(Electric Motor Driven Pump) to supply hydraulic power. Generally, we use brushed DC motor for EMDP but it is not easy to operate EMDP using brushed DC motor at a high altitude. Hence, we are developing EMDP using brushless DC motor to use at a high altitude. In this study, we will explain control system for BLDC motor to drive hydraulic pump.

• 전기산업
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• v.3 no.3
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• pp.71-85
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• 1992

• Transactions of the Korean Society of Mechanical Engineers
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• v.8 no.2
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• pp.104-110
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• 1984

An electro-hydraulic copying system is developed and its performance is experimentally investigated. As compared with a mechanical hydraulic coping system, this system has a basic difference in that; (1) the stylus movement is converted into an electrical signal via a position transducer. (2)the actuator displacement is also measured by a position sensing element, which serves as a feedback signal. Since the system parameters affect the control performance, the response characteristics such as percentage overshoot, rise time, settling time and steady state error are experimentally obtained under variation of these variables. The system parameter include supply pressure, servo amplifier gain and feedback gain. The experimental result shows that the cutting tool follows a stylus input motion to a desirable accuracy. The implication of this result indicates that the developed system can enhance the copying accuracy of the conventionally used mechanical type of hydraulic copying system.

• Proceedings of the KIEE Conference
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• summer
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• pp.890-892
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• 2004

단락발전기를 이용하여 대전류 단락시험을 실시하는 시험 설비중 단락전류 투입시 정밀한 투입 위상각 제어와 주접점 접촉시 바운싱이 없는 투입개폐기 특성이 요구된다. 이러한 특성을 만족시키기 위하여 공압식, 모터식, 유압식등 여러 종류의 투입개폐기가 사용되고 있으며 Actuator와 주 접점 형상설계 및 조립기술에 의한 바운싱이 없는 제품 제작이 중요하다. 본 논문에서는 정격전압 24 kV 단락전류 47 kA, 통전시간 0.5 s의 투입용량과 연속 반복 투입시 $\pm0.1$ ms의 오차특성을 가진 정밀급 유압식 투입개폐기의 동작특성과 핵심부품 조사 및 바운싱 제거를 위한 대책실시와 반복시험을 통하여 투입개폐기 특성에 대한 연구를 목적으로 한다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.14 no.5
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• pp.2106-2112
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• 2013

In a traditional hydraulic elevator, elevator car is descended by down control valve, and the oil hydraulic energy must be lost during the descending stroke. In this paper, hybrid type energy saving unit for a hydraulic elevator is researched to save the hydraulic energy which is lost during the descending stroke. The energy is stored as converted electrical energy, and the saved energy is reused as the auxiliary power for the ascending stroke of elevator car or the main power of other parts. The results show that the output characteristics are stable and good and the research is successful and useful to reuse the saved energy during the descending stroke of elevator car.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.12
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• pp.82-89
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• 2006

This paper describes the development results of electrohydraulic actuation system which performs the attitude and trajectory control of pitch and yaw motion using thrust vector control for high altitude launching vehicle operated in high vacuum environment (altitude higher than 300 km). As compared with electrohydraulic actuation system for low altitude launch vehicle which operated under altitude of stratosphere, the intensified development requirements, newly adopted design and manufacturing technologies, newly developed test equipments and test results are summarized in this paper. The development test and evaluation of actuation system were successfully accomplished. The developed actuation system will be installed on KSLV-I after finishing verification of interface and integration compatibility with related other systems.