• 유공압시스템학회:학술대회논문집
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• 2010.06a
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• pp.33-38
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• 2010

As for an oil hydraulic vane pump of vehicle hydraulic systems, the highest of planning technique required by the acquisition of optimum profile data which can be available to predict noises and vibrations. Pressure pulsation may result in considerable vibration and noise of pump component as well as cavitation in hydraulic system. The influences of the discharge pressure and rotating speed of the vane on the dynamic pressure in chamber surrounding a vane have been investigated. It is very important to predict pressure pulsation in vane pump. This paper presents analysis of technique of vane pump for automatic transmission. The predicted result using AMESim model were good agreement with the experimentally obtained results.

• Proceedings of the Korea Water Resources Association Conference
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• 2019.05a
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• pp.200-200
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• 2019

본 연구에서는 실제 가압장 및 가압장후단부의 상수도관망에 발생가능한 수충격해석을 수행하고 신뢰성해석을 수행하여 파괴확률을 정량적으로 산정하였다. 이를 위해 가압장의 펌프운영조건을 다르게 적용하였고 관말단부의 압력센서를 이용하여 토출압을 선택적으로 운영하면 수충격의 규모도 작아지고 파괴확률도 대폭 줄어드는 것을 확인할 수 있었다. 가압장의 토출압을 선택적으로 운영하기 위해서는 관말단부에 필수적으로 충분한 수압이 존재해야하며 이를 위해서 실시간 모니터링이 가능한 압력계를 설치하게 된다. 이 압력계로부터 수신되는 데이터를 통하여 펌프의 운영이 이루어지고 최소한의 에너지 사용을 통해 효율을 증대하고 피해율도 저감하게 된다. 본 연구에서 개발된 센서기반 펌프운영시스템이 적용된 실제 상수도관망은 현재 가압장의 운영조건으로 24시간 75m의 펌프 토출압을 유지하고 있으며 관말단부의 수용가에 충분한 수압이 전달되고 있다. 가압장의 고압유지는 관말단부에 충분한 수압을 전달하기 위한 것이지만 상수도관망에서 누수와 시설물에 대한 많은 피해를 유발할 수 있다. 따라서 본 연구에서는 가압장의 펌프토출압을 75m와 60m로 선택적 운영을 할 수 있도록 프로그램을 개발하였다. 기존 가압장의 운영조건과 선택적 운영조건을 사용하여 수충격해석을 수행하였고 신뢰성해석모형을 사용하여 파괴확률을 정량적으로 산정할 수 있었다. 가압장의 운영조건을 최적화하여 효율은 증대하고 피해율을 저감할 수 있는 방법을 찾을 수 있었다. 이를 위해서 가압장의 인버터 설치는 물론이고 펌프의 최적운영을 위해 개발된 펌프운영 프로그램을 가압장 배전반에 장착하여 경제적인 운영이 될 수 있을 뿐만 아니라 실제 상수관망에서 과도한 수압으로 인해 발생할 수 있는 여러 가지 피해를 최소화할 수 있을 것으로 판단된다. 또한, 본 연구에서는 기존의 펌프장 토출압으로 운영되었을 때와 비교하여 에너지 절감율을 정량적으로 산정하여 비교분석하였다. 가압장 후단의 작은 마을을 대상으로 하여 절감된 전기요금은 적은 양이라 할 수 있겠으나 개발된 시스템을 전국에 적용한다면 에너지 절감으로 인한 경제적 파급효과는 크다고 할 수 있다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.103-106
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• 2008

In this work it was studied that the effect on sub-component of engine considering change of engine inlet pressure caused by variable acceleration during flight of launcher. Also the transitional performance was predicted according to variable acceleration. Engine inlet pressure was defined as summation of propellant head in tank, ullage pressure and pressure difference of line, etc. Therefore consumption of propellant and acceleration of launcher led to change of engine inlet pressure, which affected on discharge pressure of pumps. This effect changed mass flow rate of gas generator and main combustor hence it was observed that engine performance was changed definitely.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2005.11a
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• pp.220-223
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• 2005

System design parameters of gas generator cycle liquid rocket engines were investigated and compared in the present study. Characteristic velocity of combustor, pressure drop of combustor injector, exit pressure of pump, pump efficiency and specific power of turbine were considered as a system design parameter. The result shows the characteristic velocity is in the range of 1700-1770 m/s, pressure drop of combustor injector, 4-10 bar, pump exit pressure ratio to combustion pressure, 120-230%, pump efficiency, 60-80%, specific power of turbine, $0.28-0.58MW{\cdot}s/kg$.

• Journal of Drive and Control
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• v.6 no.2
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• pp.17-25
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• 2009

• Journal of Drive and Control
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• v.9 no.4
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• pp.105-118
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• 2012

• Journal of the Korean Society of Propulsion Engineers
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• v.13 no.1
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• pp.43-50
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• 2009

The characteristics at the intermediate operation point of the turbopump-gas generator(TP-GG) coupled test were investigated by analytical method. The pump outlet pressure, gas generator mixture ratio, gas generator pressure, and temperature were examined considering risk minimization of test. The engine system shows different behavior from the TP-GG coupled test at the intermediate operation point since the combustion pressure feeds back to the flow rate in the lines. The advanced valve changes in the combustor line helps less risky mode transition.

• Aerospace Engineering and Technology
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• v.10 no.1
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• pp.63-69
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• 2011

In this study, we developed a dispersion analysis program of the gas-generator cycle liquid propellant rocket engine by expanding the mode analysis software(GEMAT). The performance dispersions of an engine that are arisen from the internal dispersion factors of engine's sub-components were formulated and solved to find the effects of each dispersion factor. We were also able to present the calculation method to find the required pressure margin for the compensation of those dispersion to satisfy the required performances of engine. Using this method, we could propose a novel procedure of compensating during the ground firing test which would induce the performance improvement by lessening the pumps discharge pressures or augmenting the combustion chamber pressure.

• Journal of Drive and Control
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• v.11 no.2
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• pp.1-8
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• 2014

In this study, the authors carried out experiments and numerical simulations in order to clarify the pressure pulsation characteristics in multiple-delivery rotating-cam and stationary-cylinder type radial piston pumps. Also, a tee filter was applied to the pump in order to mitigate the pressure pulsation. Through the experiments and simulations, it was known that pressure pulsation with a magnitude higher than 40% of the mean load pressure could occur in the pump used in the experiments. Moreover, it was confirmed that a tee filter designed in this study could effectively mitigate the pressure pulsation.

• Proceedings of the SAREK Conference
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• 2006.06a
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• pp.572-577
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• 2006

Numerical simulation has been made on the performance of an oil free air compressor for automotive electronic air suspension system. Calculation results on the flow rate at various air supply pressures were reasonably well compared to the experimental data. With the aid of the computer simulation program, parametric study on the compressor design parameters has also been carried out for the compressor performance improvement: Increase in the discharge port diameter or discharge valve stiffness was found to be effective to increase the flow rate per unit compressor input for the present compressor model.