• Title/Summary/Keyword: Gas control valve

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The Characteristic Study on Mixture Ratio Stabilizer for Gas Generator of LRE(Liquid Rocket Engine) (액체로켓엔진 가스발생기 혼합비 안정기의 특성 연구)

  • Jung, Tae-Kyu;Lee, Joong-Yeop;Han, Sang-Yeop;Kwon, Se-Jin
    • 유체기계공업학회:학술대회논문집
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    • 2006.08a
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    • pp.509-512
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    • 2006
  • The propellant mixture ratio of gas generator changes when thrust control valve operate to change LRE thrust level. The mixture ratio change of gas generator result in gas temperature change and failure of turbine blade or deterioration of LRE specific impulse. The mixture ratio stabilizer has been developed to maintain propellant mixture ratio of gas generator. This article deals with design and static/dynamic characteristic of stabilizer. Also gas generator system simulation test has shown that the stabilizer can maintain propellant mixture ratio effectively within tolerable range.

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Transient performance behaviour of the CRW type UAV propulsion system during flight mode transition considering valve operation (CRW형식 무인항공기 추진시스템의 밸브 작동을 고려한 비행모드 전환에 따른 천이 성능특성 연구)

  • Kong Chanduk;Park Jong-Ha;Yang Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.219-224
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    • 2005
  • In order to investigate transient behaviour of the CRW(Canard Rotor Wing) type UAV(Uninhabited Aerial Vehicle) propulsion system during flight mode transition considering flow control valve operation, the propulsion system was modelled using SIMULINK commercial program. For transient simulation of the main engine system, the ICV(Inter-Component Volume) method was applied. The valve system is to control the gas flow of the rotary duct system and the main duct system, and the analysis was performed with an assumption that the total gas mass flow of the main engine is the same as summation of the rotary duct flow and the main duct flow, and with consideration of valve loss, flow rate and effective area in valve angle variation. The performance analysis was carried out during flight mode transitions from the rotary flight mode to the fixed wing flight mode and vice versa mode at altitude of 1Km, flight Mach number 0.1 and maximum engine rpm.

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Transient performance behaviour of the CRW type UAV propulsion system during flight mode transition considering valve operation (CRW형식 무인항공기 추진시스뎀의 밸브 작동을 고려한 비행모드 전환에 따른 천이 성능특성 연구)

  • Kong Changduk;Park Jongha;Yang Sooseok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.9 no.3
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    • pp.127-132
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    • 2005
  • In order to investigate transient behavior, of the CRW(Canard Rotor Wing) type UAV(Uninhabited Aerial Vehicle) propulsion system during flight mode transition considering flow control valve operation, the propulsion system was modelled using SIMULINK commercial program. The valve system is to control the gas flow of the rotary duct system and the main duct system, and the analysis was performed with an assumption that the total gas mass flow of the main engine is the same as summation of the rotary duct flow and the main duct flow, and with consideration of valve loss, flow rate and effective area in valve angle variation. The performance analysis was carried out during flight mode transitions from the rotary flight mode to the fixed wing flight mode and vice versa mode at altitude of 1km, flight Mach number 0.1 and maximum engine rpm.

Orientation dependence of GM-type pulse tube refrigerator (GM형 맥동관 냉동기의 저온부 경사도에 따른 냉각 성능 특성 연구)

  • Ko, Jun-Seok;Kim, Hyo-Bong;Park, Seong-Je;Hong, Yong-Ju;Yeom, Han-Kil;Lee, Chung-Soo;Kang, In-Su;Koh, Deuk-Yong
    • Progress in Superconductivity and Cryogenics
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    • v.14 no.3
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    • pp.48-52
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    • 2012
  • This paper describes experimental study on the orientation dependence of GM-type pulse tube refrigerator with helium and neon as working gas. A pulse tube refrigerator generates refrigeration work with gas expansion by gas displacer in the pulse tube. The pulse tube is only filled with working gas and there exists secondary flow due to large temperature difference between cold-end and warm-end. The stability of secondary flow is affected by orientation of cold-head and thus cooling performance is deteriorated by gas mixing due to secondary flow. In this study, a single stage GM-type pulse tube with orifice valve as a phase control device is fabricated and tested. The fabricated pulse tube refrigerator is tested with two different working gases of helium and neon. First, optimal valve opening and operating frequency are determined with experimental results of no-load test. And then, the variation of no-load temperature as orientation angle of cold-head is measured for two different working gases. Effect of orientation dependence of cold-head as working gas is discussed with experimental results.

The Throttle Valve Control of engine Dynamometer system Using Fuzzy Look-up Table (퍼지 Look-up Table을 이용한 엔진 다이나모메타 시스템의 트로틀 벨브 제어)

  • 이상윤;이팔진;신위재;김치원
    • Proceedings of the Korean Institute of Intelligent Systems Conference
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    • 1995.10b
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    • pp.125-130
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    • 1995
  • Recently, the vehicle engine requried precision control of Air-Fuel rate and rigid restriction of exhaust gas. Therefore, we demanded excellent measuring equipment so as to improve of engine performance. Specially, throttle valve control is very important part in the engine control, because structure of engine dynamometer system is very important part in the engine control, because structure of engine dynamometer system is very complicate and it has nonlinear elements which is influenced of disturbance about vibration, a heat, a cooling, energy loss so on. In this study, we propose the method that the control technique using Fuzzy Look-up table and we obtained the satisfying result from realized the control system.

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A Dynamic Model of a Gas Engine-Driven Heat Pump in Cooling Mode for Real-Time Simulation

  • Shin, Young-Gy;Yang, Hoon-Cheul;Tae, Choon-Seob;Jang, Cheol-Yong;Cho, Soo
    • International Journal of Air-Conditioning and Refrigeration
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    • v.14 no.3
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    • pp.85-93
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    • 2006
  • The present study has been conducted to simulate dynamics of a gas engine-driven heat pump (GHP) for the design of control algorithm. The dynamic model of a GHP was based on conservation laws of mass and energy. For the control of refrigerant pressures, actuators such as an engine throttle valve, outdoor fans, coolant three-way valves and liquid injection valves were controlled by P or PI algorithm. The simulation results were found to be realistic enough to be applied for the control algorithm design. The model could be applied to build a virtual real-time GHP system so that it interfaces with a real controller for the purpose of developing control algorithm.

Effects of Mixture Flow and Ignition Characteristics on the Engine Performance (혼합기의 유동과 점화특성이 기관성능에 미치는 영향)

  • 이중순;김진영;정성식;하종률;배충식
    • Transactions of the Korean Society of Automotive Engineers
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    • v.6 no.5
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    • pp.37-44
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    • 1998
  • Lean burn combustion is an important concept for improving the fuel consumption and exhaust emissions. However, the lean burning is associated with increased cycle-to-cycle combustion variations due to the ignition instabilities and redu- ced flame propagation rates. Engine stability under lean mixture conditions could be improved by increasing flame speed through enhanced flow characteristics and by securing ignitability with improvement of ignition systems. The effects of flow motion and ignition characteristics on the combustion performances were investigated in a 4-valve SI engine. Flow motions of tumble-swirl were varied with a swirl control valve attached at the inlet ports, while ignition energy and its distribution were controlled in a high -frequency ignition system by changing spark duration and spark frequency. The improvement of lean burn performance by the optimum flow motion and ignition characteristics is discussed.

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Nonlinear analysis of a pneumatic actuation system by digital simulation (전산모사에 의한 공압구동장치의 비선형 해석)

  • 조택동;신효필;문의준
    • 제어로봇시스템학회:학술대회논문집
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    • 1991.10a
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    • pp.1104-1109
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    • 1991
  • Recently, Pneumatic Actuation System (PAS) has been used increasingly as a high performance fin-control servo actuation systems because of the special advantages of pneumatic units: primarily their low cost, small size, light weight, and tolerance to broad temperature extremes. In this study, a nonlinear model of PAS is derived through the detailed analysis of the major components in the typical system. The model includes nonlinear flow-pressure relationships of the flow through the solenoid valve openings and orifices, PWM algorithm for driving two solenoid valves as a closed-center 3-way valve for minimum gas consumption, solenoid valve dynamics, saturation, and friction. Simulation results are compared with the experimental ones for square and sinusoidal inputs to see the validity of the model. Independent of the shape and magnitude of the input signals, both results are in good agreements with minor difference.

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A Study on a Precision Temperature Control of Oil Coolers with Hot-gas Bypass Manner for Machine Tools Based on Fuzzy Control (퍼지제어를 이용한 공작 기계용 오일 쿨러의 핫가스 바이패스방식 정밀 온도 제어에 관한 연구)

  • Lee, Sang-Yun
    • Journal of the Institute of Convergence Signal Processing
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    • v.14 no.3
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    • pp.205-211
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    • 2013
  • Recently, the needs of system performances such as working speed and processing accuracy in machine tools have been increased. Especially, the working speed increment generates harmful heat at both moving part of the machine tools and handicrafts. The heat is a main drawback to progress accuracy of the processing. Hence, a oil cooler to control temperature is inevitable for the machine tools. In general, two representative control schemes, hot-gas bypass and variable speed control of a compressor, have been adopted in the oil cooler system. This paper deals with design and implementation method of fuzzy controller for obtaining precise temperature characteristic of HB oil cooler system in machine tools. The opening angle of an electronic expansion valve are controlled to keep reference value and room temperature of temperature at oil outlet. Especially, the fuzzy controller is added to suppress temperature fluctuation under abrupt disturbances. Through some experiments, the suggested method can control the target temperature within steady state error of ${\pm}0.22^{\circ}C$.

A Study on the Chattering under Cryogenic Flow Test of a Oxidizer Shutoff Valve (산화제 개폐밸브의 극저온 유동시험에서 채터링의 고찰)

  • Lee, JoongYoup;Han, SangYeop;Lee, SooYong
    • Aerospace Engineering and Technology
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    • v.12 no.2
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    • pp.108-117
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    • 2013
  • The oxidizer shutoff valve of a gas generator controls the mass flow rate of the propellant of a rocket engine using pilot pressure and spring the force of the valve. The developing oxidizer shutoff valve can be shut off if the pilot pressure is removed from the actuator. Therefore, force balancing is necessary to analyze the characteristics of the forces with respect to the opening and closing of the valve in order to evaluate its performance. In light of this, the valve has been designed to adjust the control pressure required to open the poppet and to determine the working fluid pressure at which the valve starts to close. Under cryogenic flow test as a tests level of C.R.T(Control Random Test), the chattering phenomena occurred due to much leakage of a metal seat section. The pressure for chattering of the oxidizer valve is predicted at about 11 bar using force balancing analysis.