• Title/Summary/Keyword: Pressure-feed System

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Development of a constant pressure feed system using a constant pressure proportional control mode (정압비례제어방식을 적용한 정압급수장치의 개발)

  • 김주명;김광열;이건기
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.7 no.5
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    • pp.1026-1031
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    • 2003
  • Automatic feed pumps are operated and stopped by a pressure switch. Thus, because of repeated operations and stops of the pumps according to fluctuations of water volume, operation with constant rate and pressure is impossible. Moreover, because of repeated running of the pump, keeping up of constant pressure is impossible and damage and energy loss are weak points of the pimps. To make up for defects of an automatic feed pump, this paper designed and made a static pressure feed system which was composed of a feed water control valve, a flow sensor and a control system. The valve device plays an important part in reducing load of pumps by constant water supply regardless of outflow of water. Outflow of water is determined by infrared diode of the flow sensor. The control system is made of a 8 bit micro-processor and the pump was controled by a specific control algorithm. With the constant pressure feed system, discharge pressure was kept at fixed pressure, accurate operations and stops were smoothly accomplished and the pump was operated with constant pressure. Thus, the constant pressure feed system can be considered as an advanced system which made up for the weak points in the current automatic feed systems.

Papers : Application of Cavitating Venturi for Stable propellant feed system (논문 : 안정적인 액체연료 공급을 위한 Cavitating Venturi 의 응용)

  • Park,Hui-Ho;Kim,Yu;Jang,Eun-Yeong;Lee,Su-Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.1
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    • pp.88-94
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    • 2002
  • For the pressurized propellant supply system of liquid rocket, feed pressure is determined with respect to the chamber pressure of normal combustion state. However, during ignition period the initial chamber pressure is atmosopheric. This may cause overflow, hard-start and even critical damage for the engine. This paper proposes an improved propellant feed system for the stable combustion of liquid rocket. The proposed system utilizes the cavitating venturi to provide stable mass flow rate. Cavitating venturi offers unique flow control capabilities at normal and abnormal combustion state, because flow rate is soley dependent on the upstream absolute pressure and fluid properties, but independent on th downstream condition. Experimental variables are propellant feed pressure and chamber pressure. The effectiveness of cavitating venturi increased when the ratio of actual feed pressure to the cavitating venturi design pressure is increased. It is also found that Kerosene if more effective to supply stable mass flow rate than LOx.

Optimal feed compositon of pressure swing distillation system to separate methanol and acetone (메탄올-아세톤 분리를 위한 압력 변환 증류 공정에서 환류를 통한 유입 조성 최적화)

  • Yoon, Young Gak;Seo, Sung Kwon;Lee, Chul-Jin
    • Plant Journal
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    • v.13 no.3
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    • pp.26-29
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    • 2017
  • In this research, the composition of the feed stream is optimized in pressure swing distillation for separating of methanol-acetone. It is well known that the composition of feed stream in pressure swing distillation system has a great influence on the feasibility to separate mixture. The workscope of this study is to show better separation efficiency at specified pressure by controlling the composition of feed stream with recycle of two products. Based on the base case without recycle flow, two processes are designed that methanol and acetone are recycled to feed stream, respectively. Each processes are compared with total annual cost and as a result, the base case without recycle flow are most favorable.

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A Study on the Flow Control for Stable Combustion of Liquid Rocket (액체로켓의 연소안정을 위한 유량공급에 관한 실험적 연구)

  • Jang, Eun-Young;Park, Hee-Ho;Kim, Sun-Ki;Kim, Yoo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.4 no.2
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    • pp.6-11
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    • 2000
  • In the pressurized propellant feed system of liquid rocket, feed pressure is decided chamber pressure of normal combustion state. However, during ignition period the initial chamber pressure is atmosphere. So, it may have overflow, hard-start and even critical damage of engine. This paper proposes an improved propellant feed system for the stable combustion of liquid rocket. Hot test were already performed to verify the presented propellent feed system. The proposed propellant feed system uses two steps - pre and main combustion - to prevent large pressure increase and uses cavitating venturis for stable flow rate in whole combustion. This system feeds the flow rate lesser than the designed flow rate, so combustion pressure reached pre-combustion pressure. Cavitating venturis offer unique flow control capabilities at normal and abnormal combustion state, because flow rate is solely dependent on upstream absolute pressure and fluid properties, but independent on downstream condition.

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Experimental Study on Fresh Water Generation System with Low Pressure Evaporation (저압 증발기를 갖는 청수제조 장치에 관한 실험적 연구)

  • Chung, Han-Shik;Wibowo, Supriyanto;Lee, Gyeong-Hwan;Shin, Yong-Han;Jeong, Hyo-Min
    • Journal of Power System Engineering
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    • v.15 no.2
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    • pp.25-30
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    • 2011
  • A fresh water generation system is designed for converting brackish water or seawater into fresh water. In this paper fresh water generation by distillation process that evaporates feed water and subsequently condenses vapor as evaporation product to get fresh water was studied and city water was employed as feed water. The system uses the ejector to create a vacuum, under which liquid can be evaporated at lower temperature than it at normal or atmospheric condition, hence less energy consumption. The effect of various operating conditions i.e. temperature of feed water and different orifice diameters were studied experimentally to investigate the characteristic of the system. It was found that these parameters have significant effect in the performance of fresh water generation system with low pressure evaporation.

Examination on High Vibration of Recirculation System for Feed Water Piping in Combined Cycle Power Plant (복합 발전소 주급수 재순환 배관계의 고진동 현상 및 대책)

  • Kim, Yeon-Whan;Kim, Jae-Won;Park, Hyun-Gu
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.04a
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    • pp.648-654
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    • 2011
  • The feed-water piping system constitutes a complex flow impedance network incorporating dynamic transfer characteristics which will amplify some pulsation frequencies. Understanding pressure pulsation waves for the feed-water recirculation piping system with cavitation problem of flow control valve is very important to prevent acoustic resonance. Feed water recirculation piping system is excited by potential sources of the shock pulse waves by cavitation of flow control valve. The pulsation becomes the source of structural vibration at the piping system. If it coincides with the natural frequency of the pipe system, excessive vibration results. High-level vibration due to the pressure pulsation affects the reliability of the plant piping system. This paper discusses the piping vibration due to the effect of shock pulsation by the cavitation of the flow control valves for the recirculation piping of feed-water pump system in combined cycle power plants.

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An Experimental Study on Water-Hammer Effect for Spacecraft Propulsion System (인공위성 추진계통 관로내의 수격효과에 관한 실험적 연구)

  • Kwon, Ki-Chul;Lee, Eun-Sang;Park, Sang-Min;Kang, Shin-Jae;Rho, Byung-Joon
    • Proceedings of the KSME Conference
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    • 2001.06e
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    • pp.288-293
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    • 2001
  • This paper presents the water-hammer effect due to the rapid opening and closing of isolation valve and thruster valve in the spacecraft propulsion system. The single propellant feed system was modeled to investigate the maximum peak pressure due to the water-hammer effect. The test parameters are tank supply pressure, shape and throat length of orifice and line length. Kerosene was used as the inert simulant propellant liquid instead of hydrazine. As downstream line length after isolation valve increased from 1.5 to 2.5m, the maximum line-filling water-hammer peak pressure decreased, but the average time interval between peak pressures increased. The maximum line-filling water-hammer peak pressure with orifice was lower than without orifice, and the maximum line-filling water-hammer peak pressure with orifice at the back of isolation valve was lower than with orifice in front of isolation valve. Without orifice, the maximum water-hammer peak pressure due to the rapid opening and closing of the thruster valve was about 126% of tank supply pressure. With orifice, it decreased. As orifice throat length increased, it decreased. The maximum water-hammer peak pressure due to the rapid closing of the thruster valve with converging-diverging orifice was lower than normal orifice. It was found that the orifice as a means of pressure drop was very effective to reduce the water hammer peak pressure at the thruster valve. The results of this study can be used for the design of spacecraft liquid propulsion feed system.

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A Study on the Revision of the National Fire Safety Codes of Sprinkler System (스프링클러설비 화재안전기준 개정에 대한 고찰)

  • Jeong, Keesin
    • Fire Science and Engineering
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    • v.27 no.5
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    • pp.32-37
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    • 2013
  • This paper suggested to revise unreasonable national fire safety codes of sprinkler system. Also proposed to modify the definition of "the gridded sprinkler system" and to add "the feed main" in terms of the definition of the pipes. In order to operate the regulations of discharge pressure of the sprinkler head efficiently, this paper checked the minimum criteria of pressure and flow for the pipe schedule sprinkler system of NFPA 13 and suggested to establish the similar minimum demand criteria. It proposed to be amended properly the pressure calculation formular in the pressure tank system and to use the correct K value due to change in pressure unit and to use the [bar] as a unit of pressure for the sake of using the existing K-factor etc.

Numerical Studies on the Effects of the Channel-Inlet-Pressure Difference in the Pressure-Retarded Osmosis (PRO) Power System (압력지연삼투(PRO) 발전 시스템에서 채널 입구 압력차의 영향에 대한 수치해석적 연구)

  • Hong, Sung Soo;Ryoo, Won;Chun, Myung-Suk;Chung, Gui Yung
    • Korean Chemical Engineering Research
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    • v.52 no.1
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    • pp.68-74
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    • 2014
  • In the spiral wound module of the pressure-retarded osmosis (PRO) system for the salinity gradient power generation, effects of the inlet pressure differences between feed-channel and draw-channel were studied. Fluxes of water and solute through membrane and power were estimated. The water flux through membrane decreased along the x-direction and increased along the y-direction with the increase of inlet pressure differences between two channels. On the other hand, the solute flux through membrane showed the opposite trend. The concentration of flow in the feed-channel increased a lot along the y-direction and that in the draw-channel decreased along the x-direction. In our system, for the inlet pressure differences of 1~11 atm, the flow rate in the feed-channel decreased about 8~13% and that in the draw-channel increased by the same amount. The power density increased and then decreased with the increasing inlet pressure difference.

Top-Feed Type Port Fuel Injector for Liquefied Petroleum Gas Liquid Phase Injection (Top-Feed Type 인젝터의 액상분사 LPG연료 분사장치 적용)

  • Yeom, Ki-Tae;Park, Jung-Seo;Bae, Choong-Sik;Park, Jeong-Nam;Kim, Sung-Kun
    • Transactions of the Korean Society of Automotive Engineers
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    • v.15 no.6
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    • pp.30-37
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    • 2007
  • The injection and spray characteristics of top-feed type injector was investigated under liquid phase injection fueled with liquefied petroleum gas (LPG). Different pressures and temperatures of fuel injection system were tested to identify the injection characteristics after hot soaking. MIE-scattering technique was used for verification of successful liquid phase injection after hot soaking. In case of bottom-feed type injector, the injection was accomplished at every experimental condition. In case of top-feed type injector, when the pressure of LPG was over 1.2 MPa, the injection was not executed. However, under the pressure were 1.2 MPa, the liquid phase injection after hot soaking was accomplished. The engine with top-feed type fuel injection equipment was restarted successfully after hot soaking.