• Title/Summary/Keyword: 밸브 형상

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An experimental study on the characteristics of the swirl ratio distribution with an intake port geometry (흡기포트 형상에 따른 선회비 분포특성에 관한 실험적 연구)

  • Lee, Ji-Geun;Ju, Bong-Cheol;No, Byeong-Jun;Gang, Sin-Jae
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.21 no.6
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    • pp.725-734
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    • 1997
  • The effect of helical intake port geometry on in-cylinder swirl flow characteristics was studied. Two helical intake ports were selected to change swirl ratio, mean flow coefficient with the variation of valve lifts, valve eccentricity ratios and axial distance. The measurements were made by using an impulse swirl meter. The port B modified to increase the swirl ratio( $R_{s}$) had the tendency of the increased non-dimensional rig swirl ( $N_{r}$) distribution in comparison with that of the port A. And the $N_{r}$ distribution was remarkably improved at low valve lifts. The modification of the geometry to increase the swirl ratio ( $R_{s}$) in helical intake port resulted in the decrease of the mean flow coefficient ( $C_{f(mean)}$) regardless of valve eccentricity ratio ( $N_{y}$). And also non-dimensional rig swirl ( $N_{r}$) in the high valve lift affected the calculation of swirl ratio considerably.onsiderably.

An experimental study on the dynamic behavior in an aero-valved pulsating combustor (공기밸브형 맥동연소기의 동적 특성에 관한 실험적 연구)

  • 임광열;최병륜;오상헌
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.11 no.5
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    • pp.846-855
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    • 1987
  • The experimental study was carried out to investigate the performance characteristics of the aero-valved pulsating combustor designed to increase the practical applications of the system. The geometric effect on the stable condition and the dynamic behavior of the system is identified. The equivalence ratio, the inflammability limit, the operating frequency, and thrust were also measured when the system oscillated stably. It is found that while the operating condition is sensitive to the diameter of the inlet pipe and the length of the tailpipe, the maximum value of the turn down ratio was obtained up to 3.2. The measured air flow rate shows that the equivalence ratio increases monotonously with the increasing fuel flow rate and decreasing air inlet diameter and tailpipe length. The measured operating frequency can be approximated by the simple linear equation and the discrepancy is within five percent. The system produced the maximum total thrust of 14N and the minimum specific fuel consumption of 0.155 Nm$^{3}$/h.N when the total thrust was 13N.

A Study on the Steady Flow Characteristics by PDA and Tumble Control Valve in Combustion Chamber (스월 및 연소실 형상에 의한 정상유동특성에 관한 연구)

  • Kim Dae-Yeol;Han Young-Chool;Park Bong-Kyu
    • Transactions of the Korean Society of Machine Tool Engineers
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    • v.15 no.4
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    • pp.74-82
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    • 2006
  • This paper describes the steady flow characteristics due to PDA and tumble control valve in combustion chamber. We also investigated the flow inclination angle defined as the inverse tangent of non-dimensional rig tumble(NRT) devided by non-dimensional rig swirl(NRS) to find dominant flow direction. So we adapted two different types of PDA valve(port deactivation valve) to strengthen a swirl flow. The in-cylinder swirl flow different tendency between with/without PDA valve. It might be thought to be affected by swirl flow. We could find that tumble ratio and swirl ratio is different by PDA valve. The comparison are taked account of the swirl, the tumble ratio comparison in same mass flow rate. As a result, PDA valve is better than tumble control valve both in steady flow condition and swirl, tumble ratio. The data from present study are available for design of engine as the basic data.

Development of High Thrust $H_2O_2$ Monopropellant Thruster for Reaction Control System of Space Launch Vehicles (발사체 자세제어 적용을 위한 고추력 과산화수소 단일추진제 추력기 개발)

  • An, Sung-Yong;Kim, Jong-Hak;Yoon, Ho-Seung;Kwon, Se-Jin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.1
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    • pp.1-10
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    • 2010
  • Design and performance evaluation of $H_2O_2$ monopropellant thrusters to be used at reaction control of space launch vehicles were presented in this paper. Design thrust level was determined as 100, 250 Newton which is nominal thrust level for commercial space launch vehicles. Qualification thruster models including solenoid valves were developed after the reactor design were evaluated at engineering thruster models. Each thruster was evaluated by measurement of characteristic velocity, thrust, specific impulse, and pulse response times at sea level test condition.

A Study on the Noise Reduction and Performance Improvement of the Hot Water Distributing System (시스템분배기 소음방지 및 성능개선방안 연구)

  • Kim, Yong-Ki;Lee, Tae-Won;Han, Tae-Su;Yoo, Sun-Hak
    • Proceedings of the SAREK Conference
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    • 2009.06a
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    • pp.1055-1060
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    • 2009
  • Noise is one of the major environmental problems in human life. But hot water distributers with the flow rate control valve bring about often noise according to the heating control condition in residential buildings. The sound power level increased as the flow rate and pressure difference increased. And thus, experimental analyses for the flow rate control and the pressure difference control were carried out in this study to reduce the noise emitted from the flow rate control valve. As the results, the flow rate control method using a SMA(Shape Memory Alloy)-valve and the flow rate control system using a pressure difference sensor can be expected to control noise in the region of below 50 dB of sound power level.

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Computer Simulation and Shape Design Sensitivity Analysis of the Valve inside the Reciprocal Compressor using Finite Element Model (유한 요소 모델을 이용한 왕복동식 압축기 밸브의 거동 해석 및 형상 설계 민감도 해석)

  • 이제원;왕세명;주재만;박승일;이성태
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.05a
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    • pp.796-801
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    • 2002
  • The goal of this research is the shape design of the valve using a computer simulation. For an analysis a basic mathematical model describing compression cycle is considered as consisting of five sets of coupled equations. These are the volume equation (kinematics), valve dynamic equation (dynamics), ideal gas equation (thermodynamics), Bernoulli equation (fluid dynamics), and dynamic equation of fluid particle based on Helmholtz equation (acoustics). Valve motion is made by the superposition of free vibration modes obtained by the finite element method. That is, the eigenvalues and eigenvectors are the sufficient modeling factors fur the valve in the simulation program. Thus, to design a shape of the valve, shape design sensitivity through chain-ruled derivatives is considered from two sensitivity coefficients, one is the design sensitivity of the capability of compressor with respect to the eigenvalues of the valve, and the other is the design sensitivity of the eigenvalue with respect to the shape change of the valve. In this research, the continuum design sensitivity analysis concepts are used for the latter.

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Combustion chamber layout for modern otto-engine (Otto 엔진의 연소실 Layout)

  • Gruden, D.
    • Journal of the korean Society of Automotive Engineers
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    • v.8 no.2
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    • pp.13-21
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    • 1986
  • 점차 엄격해지는 요구조건을 만족시켜 주기 위해서는 승용차용 엔진의 실제특성과 운전특성을 지 배하는 설계변수의 조절은 불가피하며, 그중에서도 엔진의 핵심부인 연소질의 설계는 가장 중요 하다. 부분 부하에서의 SI기관의 연료경제성을 향상시키는 가장 좋은 방법이 압축비를 상승시 키는 것이므로, 앞으로의 여소실은 고압축비에서도 옥탄가가 높은 연료를 요구하는 성향을 낮 추는 특성을 갖고 있어야 한다. 새로운 엔진의 향상을 최적화하기 위하여는 quench area의 크 기와 위치 그리고 적절한 quench distance의 성질이 중요하며, 또한 연소실의 소형화, 스파크 플러크의 위치, 표면적/체적의 비 그리고 화염전파거리등도 고려에 넣어야 한다. 승용차용 엔진의 요구조건은 연소실을 피스톤 크라운에 위치시키는 용이한 방법을 통하여 해결될 수 있으며, 이 러한 형상의 연소실은 실린더 헤드에 장치한 연소실과 비교하여 다음과 같은 장점을 갖고 있다. - 스파크 플러그 주변에 연소실을 배치하기 쉽다. - 연소실 내에 quench area의 설정이 자유롭다. - 연소실 layout의 개조없이 압축비의 설정이 자유롭다. - 연소실의 조합이 간단하다. - 실린더벽으로의 열손실이 감소되어 열효율이 증대된다. - 공연비의 희박가능한계가 크다. - EGR성능이 향상되어 NOx 의 배출과 연료소비율이 감소된다. - 필요하다면 연소실실 또는 직접분사식 Diesel 기관으로서의 개조가 간단하다. 만약 생산단가가 크게 상승하지 않는다면, NOx의 배출과 연료소비율이 작으면서도, 비출력이 큰 4-밸브 연소실이 실용화 될 전망이다.

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Analysis of Dynamic Characteristics for High speed Plunger-type Solenoid (고속 플런저형 솔레노이드의 동특성 해석)

  • 백동기;성세진
    • The Transactions of the Korean Institute of Power Electronics
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    • v.2 no.1
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    • pp.26-32
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    • 1997
  • In this paper, numerical analysis of dynamic characteristics for the plunger-type solenoid was used for a high speed solenoid valve with fast switching is discussed. The theoretic analysis of the electromagnetic field including eddy currents in the solenoid is studied by using permeance. The optimum value of design parameters which are a mass and an area of the plunger, a source voltage, a elastic modulus of the spring, a stroke, a number of turns, are obtained by the results of the investigation on effect of a parameter on others. And dynamic characteristics of acting solenoid that is the variation of magnetic force, displacement, solenoid current are investigated.

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Analysis of Flow Performance According to Actuator Geometry of Receptacle for Hydrogen Charging System with Filter Applied (필터가 장착된 수소충전시스템용 리셉터클의 작동부 형상에 따른 유동 성능 분석)

  • JU HWAN CHOI; GU HO KIM;JAE KWANG KIM;YONG KI KIM;HYUN KYU SUH
    • Transactions of the Korean hydrogen and new energy society
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    • v.34 no.1
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    • pp.17-25
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    • 2023
  • The purpose of this study was to propose a design that shows optimal performance by changing the geometry of the internal flow path of the receptacle in order to prevent the decrease in flow rate and differential pressure performance due to the application of the receptacle in the hydrogen charging system. To achieve this, 3D computational fluid dynamics simulation was performed for the receptacle, according to the geometry of the flow path inside the receptacle. The pressure results at the inlet and outlet were measured the same as both of N and H2 in the experiment, and the flow rate of H2 was 3.75 times higher than that of N2. In addition, since the flow performance of the receptacle improved under conditions where the flow path was widened, it was confirmed that reducing the diameter of the poppet and the width of the guide are advantageous for improving performance.

Water droplet generation technique for 3D water drop sculptures (3차원 물방울 조각 생성장치의 구현을 위한 물방울 생성기법)

  • Lin, Long-Chun;Park, Yeon-yong;Jung, Moon Ryul
    • Journal of the Korea Computer Graphics Society
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    • v.25 no.3
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    • pp.143-152
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    • 2019
  • This paper presents two new techniques for solving the two problems of the water curtain: 'shape distortion' caused by gravity and 'resolution degradation' caused by fine satellite droplets around the shape. In the first method, when the user converts a three-dimensional model to a vertical sequence of slices, the slices are evenly spaced. The method is to adjust the time points at which the equi-distance slices are created by the nozzle array. In this method, even if the velocity of a water drop increases with time by gravity, the water drop slices maintain the equal interval at the moment of forming the whole shape, thereby preventing distortion. The second method is called the minimum time interval technique. The minimum time interval is the time between the open command of a nozzle and the next open command of the nozzle, so that consecutive water drops are clearly created without satellite drops. When the user converts a three-dimensional model to a sequence of slices, the slices are defined as close as possible, not evenly spaced, considering the minimum time interval of consecutive drops. The slices are arranged in short intervals in the top area of the shape, and the slices are arranged in long intervals in the bottom area of the shape. The minimum time interval is pre-determined by an experiment, and consists of the time from the open command of the nozzle to the time at which the nozzle is fully open, and the time in which the fully open state is maintained, and the time from the close command to the time at which the nozzle is fully closed. The second method produces water drop sculptures with higher resolution than does the first method.