• Title/Summary/Keyword: 유압동력 발생장치

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A Study of the Variation in Intensifier Performance Characteristics Varying with Pressure and Temperature (압력·온도 변화에 따른 초고압 발생기 성능특성 연구)

  • Kim, Hyoung-Eui;Lee, Gi-Chun;Kim, Jae-Hoon
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.34 no.9
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    • pp.1249-1255
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    • 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.

An experimental study on the improving noise characteristic of hydraulic power unit (유압동력 발생장치의 소음특성 개선을 위한 실험적 연구)

  • Lee, Gi Chun;Lee, Yong Bum
    • Journal of Advanced Marine Engineering and Technology
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    • v.37 no.6
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    • pp.638-643
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    • 2013
  • Nowadays, the hydraulic power unit (HPU) has been increased its working pressure and enlarged its capacity in order to improve the performance of the hydraulic system, but it produces noise leveled around 110dB(A) during operation. Recently, due to the reinforcement of industrial safety regulations and the requirement of improving work environment, a separated HPU room is installed at outside or underground of the building as to reduce the noise from HPU, but there are also problems of power loss owing its fluid friction of pipe system and of deficient accessibility during its failure accident. In this study, experiment is performed to improve the noise characteristics with installing a soundproof chamber to minimize the power loss and exclude effectively the high leveled noise, which is generated during the power conversion of HPU.

A Reliability Study of Direct Flow Control Type Hydraulic Pump by the Electric Motor (전기모터에 의한 직접유량 제어방식 유압펌프의 신뢰성 연구)

  • Sung, Baek-Ju;Kim, Doh-Sik
    • Proceedings of the KIEE Conference
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    • 2011.07a
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    • pp.1033-1034
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    • 2011
  • 공작기계에 유압동력을 공급하는 유압동력발생장치의 신뢰성은 공작기계 전체의 신뢰성과 밀접한 관계를 가진다. 전기모터에 의해 유량을 직접제어하는 유압펌프의 시제품에 대한 신뢰성을 평가하기 위해서 성능시험, 내환경시험, 그리고 수명내구시험을 실시할 필요가 있다. 본 연구에서는 2단계 품질기능 전개를 통해 전기모터에 의한 직접유량 제어방식 유압펌프의 신뢰성평가 시험항목을 결정하였다. 시험항목에는 전기모터에 대한 항목, 유압펌프에 대한 항목, 하우징 및 냉각시스템에 대한 항목이 포함되어 있다. 신뢰성평가 시험 항목 중, 가장 큰 비중을 차지하는 수명내구시험에 대해 무고장수명시험을 산출하고, 시험소요시간 단축을 위한 가속모델을 제안하고, 실제 구동 조건을 적용하여 가속수명시험시간을 산출하였다.

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KSR- III 추력벡터제어를 위한 유압-서보 김발엔진 구동시스템에 관한 연구

  • Lee, Hee-Joong
    • Aerospace Engineering and Technology
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    • v.1 no.1
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    • pp.141-146
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    • 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.

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유압베인펌프의 마찰특성

  • 정재연;이종순;김장현;이봉구
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1989.06a
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    • pp.22-28
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    • 1989
  • 유압베인펌프는 토출유량이 많고 소형으로 동력밀도는 높으나 토출압력면에스는 피스톤식 펌프에 뒤지기 때문에 발생압력의 고압화에 대한 연구가 계속되어 왔다. 유압장치의 경제적인 압력으로서 $300kgf/cm^2$가 제시되어 있는 가운데, 유압베인펌프의 고압화의 연구가 진행중에 있는 점, 또한 최근들어 에너지 절약의 일환으로 펌프의 수명연장 문제가 거론되어 지고 있는 점, 물에 타기 어려운 난연성유압 작동유를 사용할 경우 마찰증대 및 마모성능이 저하하는 점 등의 이유에서 유압베인 펌프의 마찰, 윤활문제가 중요시 되어지고 있다. 특히 펌프의 체적효율을 높이는 것과 마찰, 마모를 저하시키는 것과는 서로 상반된 관계에 놓여있기 때문에 문제의 해결에 어려움을 갖고 있다. 이와같은 모순을 해결하기 위해서는 베인과 캠링사이의 슬라이딩부분의 윤활상태를 파악하지 않으면 안된다. 그러나 베인의 선단부에는 10-20ms의 짧은 시간동안에 수백기압의 압력이 변화하기 때문에 지금까지 확실한 작용력의 파악이 어려워 이 분야의 윤활상태 파악에 관한 연구는 거의 이루어지지 않고 있다. 베인과 캠링간의 윤활상태를 윤활공학적 관점에서 보면 변동하중 상태에서의 슬라이딩 탄성유체윤활상태 또는 혼합윤활상태에 있는 것으로 판단되어지는데, 이와같은 여러가지 어려운 조건 때문에 윤활상태를 파악하는데, 어려운점이 뒤따르게 된다. 위와 같은 배경에 착안하여 본 연구에서는 유압베인펌프를 모델화하여 변동하중상태에서 실험이 가능한 장치를 제작, 사용하여 베인 선단 슬라이딩부분의 윤활상태를 파악하였다.

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A Study on the Air Vent Valve of the Hydraulic Servo Actuator for Steam Control of Power Plants (발전소의 스팀제어용 유압서보 액추에이터의 공기배출 밸브에 관한 연구)

  • Lee, Yong Bum;Lee, Jong Jik
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.6
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    • pp.397-402
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    • 2016
  • To produce adequate electricity in nuclear and thermal power plants, an optimal amount of steam should be supplied to a generator connected to high- and low-pressure steam turbines. A turbine output control device, which is a special steam valve employed to supply or interrupt the steam to the turbine, is operated using a hydraulic servo actuator. In power plants, the performance of servo actuators is degraded by the air generated from the hydraulic system, or causes frequent failures owing to an increase in the wear of the seal. This is due to the seal being burnt as generated heat using the produced compressed air. Some power plants have exhausted air using a fixed orifice, and thus they encounter power loss due to mass flow exhaust. Failures are generated in hydraulic pumps, electric motors, and valves, which are frequently operated. In this study, we perform modeling and analysis of the load-sensing air-exhaust valves, which can be passed through very fine flow under normal use conditions, and exhaust mass flow air at the beginning stage as with existing fixed orifices. Then, we propose a method to prevent failures due to the compressed air, and to ensure the control accuracy of hydraulic servo actuators.

A Study on the Lateral Vibration Reduction of the High-speed Electric Multiple Unit (동력분산형 고속열차의 횡방향 진동저감에 관한 연구)

  • Jeon, Chang-Sung;Park, Joon-Hyuk;Kim, Sang-Soo;Kim, Seog-Won
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.12
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    • pp.797-803
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    • 2019
  • This study was carried out to reduce the lateral vibration of high-speed electric multiple units. In the study, the high-speed electric multiple unit prototype (HEMU-430X) has a high lateral vibration at low equivalent conicity regardless of the wheel profiles (XP55, GV40, S1002). As wheel wear progresses and the equivalent conicity increases, the lateral vibration tends to decrease. The reason is that a combination of the suspension characteristics causes the body and bogie to resonate at a frequency of 1.4 Hz when the equivalent conicity is low, resulting in body hunting. An investigation of the lateral vibration of overseas high-speed trains showed that a decrease in the hydraulic stiffness of the yaw damper could improve the vibration. The series stiffness of the yaw damper is a combination of the hydraulic stiffness and elastic joint. In this study, an attempt was made to improve the lateral vibration by lowering the stiffness of the elastic joint. The series stiffness of the adjusted yaw damper was approximately 60% compared to the original one. The on track test results showed improvement in the lateral vibration for both running directions. The vibration reduction method of this study can be used for EMU-250 and EMU-320 in future commercial operations.

Study of the high pressure hose assemblies by accelerated life test (고압호스 조립체의 가속수명시험에 관한 연구)

  • Lee, Gi Chun;Lee, Yong Bum
    • Journal of Advanced Marine Engineering and Technology
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    • v.37 no.8
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    • pp.886-892
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    • 2013
  • Hydraulic hose assemblies are used as piping components for construction machinery, automobile, aircraft, industrial machinery, machine tools, and machinery for ships. Then the reliability of hose assemblies is important because total hydraulic system, which used to deliver the fluid power ($P^*Q$) needed to flexibility in the piping system, is not operated if the hose assembly failed in the system. The data of the accelerated life test estimated through the shape parameter(${\beta}$) resulting of the Weibull distribution analysis. This study has tried to reduce the test time resulting from varying impulse pressure range and the flexing diameter. Accelerated life test model for the test results was adopted the GLL(generalized log linear) and the accelerated indexes are identified as 6.64 for the pressure and 4.46 for flexing radius. Also, it found that shape parameter is 6.19, scale parameter(${\eta}$) is $1.035{\times}108$, which were adopted the pressure 35 MPa and the flexing diameter R100 mm in the used condition.

Flight Safety Improvement on Surion through Circuit Design and Software Reformation of Data Acquisition Unit (수리온 데이터획득/처리장치 동작회로 및 소프트웨어 개선을 통한 비행안전성 향상)

  • Jun, Byung-kyu;Jeong, Sang-gyu;Kim, Young-mok;Chang, In-ki
    • Journal of Advanced Navigation Technology
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    • v.19 no.5
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    • pp.370-378
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    • 2015
  • The data acquisition unit, signal acquiring and processing equipment, processes and provides major data of an aircraft such as engine system, power train system, hydraulic system, etc. However, it had lots of failure related to the system during production test flight, and it is necessary to fix them perfectly as soon as possible because of the significance of the equipment. In this paper, it contains failure classification and analysis for each defect element to improve whole software as well as electrical circuit. Particularly, utilizing Fault Injection Method based interworking test, more efficient improvement activity was performed for not only equipment level but also aircraft level, and as a result, it is achieved that considerable betterment of Surion quality and flight safety.