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

• Journal of the korean Society of Automotive Engineers
• /
• v.17 no.5
• /
• pp.28-35
• /
• 1995

본 해설에서는 클러치 제어용 유압계 특성에 대하여 간략히 서술하고 각 장치즐의 장단점을 비교 검토함과 동시에, 본 저자들이 개발한 클러치 조작용 유압계에 쓰이는 압력조절장치에 대하여 설명한다. 1. 변속장치내 클러치 조작용 유압계 특성. 1.1 클러치 조작용 유압계 제어의 필요성. 1.2 변속시 충격 토크의 저감법. 1.3 클러치 조작용 유압계의 제어방식.

• 전기의세계
• /
• v.17 no.2
• /
• pp.35-37
• /
• 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.)

• Journal of the korean Society of Automotive Engineers
• /
• v.13 no.6
• /
• pp.30-38
• /
• 1991

자동차의 제동장치, 조향장치, 자동 변속장치 등에 요구되는 큰 힘을 얻기 위하여 유압식 구동장치가 중량당 출력비가 높고 응답특성이 좋으며 과부하에 대한 방지기능이 간단하게 이루어 진다는 장점이 있기 때문이다. 본 고에서는 우리나라에서도 전자제어식 제동장치, 조향장치, 자동변속장치, 현가장치 등의 개발을 시도하고 있는 현 시점에서 기술축적이 가장 취약한 분야라고 볼 수 있는 자동차용 전기유압밸브의 기본적인 메카니즘에 대하여 종합적으로 소개하고자 한다.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.34 no.9
• /
• pp.1249-1255
• /
• 2010

An ultra high- pressure system generally consists of a hydraulic power unit, an oil supply unit, an electrical power supply device, and an electrical control device. The hydraulic power unit supplies the hydraulic power to the intensifier to create generate ultra high pressure. The intensifier amplifies increases the pressure using the oil supplied from by the hydraulic power unit. The electrical supply devices and control devices maintain are provided for the electric motors, valves, and sensors. In this study, instead of a flow-control device, a pressure-control type device was mounted on a manifold block in the hydraulic power unit instead of the flow-control type. A servo valve was fitted in the intensifier, and the performance characteristics of the intensifier varied according to the variations of in the pressure cycle and with the temperature of the operating oil in the hydraulic power unit.

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

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

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.13 no.9
• /
• pp.3869-3875
• /
• 2012

In this study, mathematical modeling and experimental analysis were executed in order to evaluate the valve dynamic characteristics when the hydraulic pressure applied. High pressure on the master cylinder effects on the valve dynamic characteristics have been analyzed. The pulsation pressure generated in hydraulic systems causes noise, vibration and odd effect to the system. To reduce the pulsation pressure, high frequency PWM control of 20KHz was attempted. Also, an analytic method is proposed for the resultant forces of electromagnetism and hydraulic pressure generated in the real vehicle electro stability program. Consequently, results of solenoid valve dynamic characteristics analysis derived in the study can be confirmed criteria for the optimal control of electronic stability program system.

• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 1993.04b
• /
• pp.181-184
• /
• 1993

일반적으로유압 장치를 사용하여 힘, 속도, 그리고 위치 등을 제어하는 경우 그 제어계의 설계, 제어방식의 선택에있어서는 최종 목표치의 정도, 응답성 등의 제어 성능을 고려함과 동시에 공업적으로는 가격, 동력효율 등이 중요한 설계인자로서 고려 되어 져야한다. 제어 방식응 벨브 제어와 펌프 제어 방식으로 크게 나뉘어 질 수 있으나, 벨브 제어방식에 있어서는 유압 서보벨브를 사용하여 출력 기구를 고정도로 직접 구도하는 것이 많으나 동력손실이 큰 편이며, 효율을 개선하기 위하여 압력 보상형 비례 전자 제어 벨브를 이용하는 것도 있으나, 소출력용으로서만 이용가능할 뿐이다. 이에 비하여 가변 용량형 펌프를 이용한 제어방식은 정도, 응답성은 다소 뒤떨어 지지만 효율이 양호하고 대출력 기구에 적용 가능하다는 점에서최근 주목의 대상으로되고 있다. 본 연구에서는 에너지의 효율적인사용이 가능한 전기. 유압 펌프 시스템을 설계하기위하여 먼저 각 신호전달 요소에 대한 동특성 및 정특성 실험을 행하여 시스템의 근사적인 모델링을 행하고 사판의 경사각을 제어함으로써 유압모터의 속도를 제어하는 시스템을 설계하여그 성능을 고찰하고자 한다.

• Aerospace Engineering and Technology
• /
• v.1 no.1
• /
• pp.141-146
• /
• 2002

During dynamic flight by propulsion of rocket engine, in the atmosphere, the attitude control of flight vehicle can be accomplished by the aerodynamic fin actuator. But, in the outer space, the method of TVC(Thrust Vector Control) is only depend on for it. There are many systems which were developed for TVC. In our research, among them we adopted gimbal engine actuation system which could control the vector of thrust by swivelling rocket engine connected by gimbal. There are electro-hydraulic, electro-mechanical and pneumatic system which can be used as gimbal engine actuation system, but the electro-hydraulic system that has high ratio of output power to mass is preferred for the high power system. In this note, we made a mathematical model of the electro-hydraulic gimbal engine actuation system for the TVC of KSR-III in detail and on the base of this model we performed a simulation study. And then, we verified the model by making a comparison between the simulation and the experiments on the real system.