• Title/Summary/Keyword: Regenerative Pump

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Simulation of a geothermal power generation system using the Kalina cycle (칼리나 사이클을 이용한 지열발전 시스템의 시뮬레이션)

  • Chang, Ki-Chang;Baik, Young-Jin;Kim, Min-Sung;Lee, Young-Soo;Park, Seong-Ryong;Ra, Ho-Sang
    • 한국신재생에너지학회:학술대회논문집
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    • 2008.05a
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    • pp.626-629
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    • 2008
  • In this study, a geothermal power generation system using the Kalina cycle was investigated by the simulation method. The Kalina cycle system can be used for the utilization of a low-temperature heat sources such as geothermal and industrial waste heat that are not hot enough to produce steam. The sea/river water can be considered as a cooling media. A steady-state simulation model was developed to analyze and optimize its performance. The model contains a turbine, a pump, an expansion valve and heat exchangers. The turbine and pump were modelled by an isentropic efficiency, while a condenser, an evaporator and a regenerative heat exchanger were modeled by UA-LMTD method with a counter-flow assumption. The effect of the ammonia fraction at the separator inlet on the cycle performance is investigated in detail.

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Modeling of Liquid Rocket Engine Components Dynamics at Transient Operation (액체로켓엔진 천이작동 예측을 위한 구성품 동특성 모델링)

  • Kim, Hyung-Min;Lee, Kuk-Jin;Yoon, Woong-Sup
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.1
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    • pp.35-44
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    • 2011
  • Mathematical modelling for liquid rocket engine(LRE) main components were conducted to predict the dynamic characteristics when the LRE operates at the transient condition, which include engine start up, shut down, or thrust control. Propellant feeding system is composed of fuel and oxidizer feeding components except for regenerative cooling channel for the fuel circuit. Components modeling of pump, pipe, orifice, control valve, regenerative cooling channel and injector was serially made. Hydraulic tests of scale down component were made in order to validate modelling components. The mathematical models of engine components were integrated into LRE transient simulation program in concomitant with experimental validation.

Power Circulation Characteristics of Hydro-Mechanical transmission System in Steering (정유압 기계식 변속기의 조향시 동력 순환 특성)

  • Kim, J. S.;Kim, W.;Jung, Y. H.;Jung, S. B.;Kim, H. S.
    • Transactions of the Korean Society of Automotive Engineers
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    • v.5 no.2
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    • pp.13-22
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    • 1997
  • Power flow characteristics of a hydro-mechanical transmission system(HMT) are investigated for tracked vehicle in steering. A HMT consisting of two hydrostatic pump motors(HST), several planetary gear trains and steer differential gear is considered. In order to obtain the direction and magnitude of the power flow of the HMT, network theory for the general power transmission is used. Network model for the HMT in steering is developed, which consists of shafts, nodes and transmission elements such as clutch, gear, etc. Power flow analysis procedure consists of two stages : (1) traction force analysis in steering, (2) power flow analysis in HMT. Torque and speed of every transmission element of the HMT is determined from the network analysis. Also, efficiency, mechanical and hydraulic power loss including HST, are obtained. In addition, the regenerative power flow resulting from steering can be studied in graphic display. The power flow analysis program(PCSTEER) developed in this work can be used as a useful design tool for the tracked vehicle with HMT.

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우주발사체용 터보펌프 액체추진기관 시스템 분석

  • Seo, Kyoun-Su;Joh, Mi-Ok;Choi, Young-In;Hong, Soon-Do;Oh, Bum-Seok
    • Aerospace Engineering and Technology
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    • v.2 no.2
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    • pp.151-156
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    • 2003
  • Liquid rocket engine system is classified into an engine of pressurization and turbo pump type by the way of fuel fed-supporting system. In the KSR-III sounding rocket, an engine of pressurization type was used, but there was lots of technical problems to be solved for a use as the first stage engine of space launch vehicle. So, an engine of turbo pump type was required to be developed to overcome the technical limitation of liquid rocket engine. In this research, the analysis of propellant of Kerosine-LOX and methane-LOX which are noticed as a future propellant was carried out for the purpose of studying the basic characteristics. And to review the basic characteristics of an engine of turbo pump type, among the sizing variant of the space launch vehicle, the ways of injecting a satellite to a direct orbit and transient orbit were discussed in this paper.

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Kilohertz Gain-Switched Ti:sapphire Laser Operation and Femtosecond Chirped-Pulse Regenerative Amplification (KHz 반복률에서의 Ti:sapphire 이득 스위칭 레이저 발진과 펨토초 처프펄스 재생 증폭)

  • Lee, Yong-In;Ahn, Yeong-Hwan;Lee, Sang-Min;Seo, Min-Ah;Kim, Dai-Sik;Rotermund, Fabian
    • Korean Journal of Optics and Photonics
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    • v.17 no.6
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    • pp.556-563
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    • 2006
  • We present a comprehensive study of a chirped pulse Ti:sapphire regenerative amplifier system operating at 1 kHz. Main constituents of the system are described in detail. The amplifier stage was first converted to a repetition rate-tunable kHz gain-switched nanosecond Ti:sapphire laser. Operation characteristics at different repetition rates such as build-up times of laser pulses, pump power-dependent output powers and pulse durations, damage thresholds, and tunability ranges were studied. Based on the results achieved, the switching time of the Pocket's cell used and the round trip numbers in the regenerative amplifier were optimized at 1 kHz. The output pulses with a pulse width of 50fs from a home-made Ken lens mode-locked Ti:sapphire oscillator were used as seed pulses. The pulses were expanded to 120ps in a grating stretcher prior to coupling into the 3-mirror amplifier cavity. After amplification and recompression, a stable 1kHz Ti:sapphire regenerative amplifier system, which delivers 85-fs, $320-{\mu}J$ pulses, was fully constructed.

Modular Program for Conceptual Design of Liquid Rocket Engine System, Part I : Essential Components Design (액체 로켓 엔진시스템 개념설계를 위한 모듈화 프로그램 Part I : 주요 구성품 설계)

  • Yang, Hee-Sung;Park, Byung-Hoon;Yoon, Woong-Sup
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.9
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    • pp.805-815
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    • 2007
  • In order to build a conceptual design program for a liquid rocket engine system, performance based sub-programs for each core component of the engine system were made. Parts included were the combustion chamber, supersonic nozzle, centrifugal pump, and impulsive turbine. Simple mathematical models based on classical thermodynamic and inviscid theories were adopted with proper tuning by empirical data. In Part I, aiming to validate each sub-program, we examined the results of each program qualitatively, and parametrically investigated the sensitivity due to the change in design parameters.

Specific Impulse Variation of a Liquid Rocket Engine by Film Cooling (막냉각에 의한 액체로켓엔진의 비추력 변화)

  • Cho, Won-Kook;Park, Soon-Young;Seol, Woo-Seok
    • Aerospace Engineering and Technology
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    • v.8 no.2
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    • pp.133-139
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    • 2009
  • An analysis has been performed on the specific impulse for a liquid rocket engine of gas generator cycle. The present analysis method has been validated through the comparison of the optimal specific impulse for the 300t thrust conceptual engine against the published data. The engine specific impulse can be increased by applying film coolant decreasing the fuel pump head for regenerative cooling despite the decrease of specific impulse of the combustion chamber when the film coolant participates combustion more than the critical amount. The improved condition shows that higher combustion chamber pressure is achieved with less fuel pump head rise by additional film cooling.

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Simulation of the Kalina cycle for a Geothermal Power Generation (지열발전을 위한 칼리나 사이클의 시뮬레이션)

  • Baik, Young-Jin;Kim, Min-Sung;Chang, Ki-Chang;Lee, Young-Soo;Park, Seong-Ryong;Ra, Ho-Sang
    • Proceedings of the SAREK Conference
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    • 2008.06a
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    • pp.782-787
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    • 2008
  • The Kalina cycle simulation study was carried out for a preliminary design of a geothermal power generation system. The Kalina cycle system can be used for the utilization of a low-temperature heat sources such as geothermal and industrial waste heat that are not hot enough to produce steam. The sea/river water can be considered as a cooling media. A steady-state simulation model was developed to analyze and optimize its performance. The model contains a turbine, a pump, an expansion valve and heat exchangers. The turbine and pump were modelled by an isentropic efficiency, while a condenser, an evaporator and a regenerative heat exchanger were modeled by UA-LMTD method with a counter-flow assumption. The simulation results show that the power generation efficiency over 10% is expected when a heat source and sink inlet temperatures are $100^{\circ}C$ and $10^{\circ}C$ respectively.

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A Case of Aggravated Hyperplastic Gastric Polyps after Treatment with Long-term Proton Pump Inhibitors (양성자 펌프 억제제 투여로 악화된 과증식 위용종 1예)

  • Kim, Ho Tae;Park, Jong Wan;Eom, Seok Hyeon;Kwak, Tae Yeung;Hwang, Hong Suk;Kim, Yeung Sung;Kwak, Dong Hyup;Kim, Jung Hee
    • Journal of Yeungnam Medical Science
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    • v.30 no.2
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    • pp.141-144
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    • 2013
  • Hyperplastic gastric polyps (HPPs) are the most common type of gastric polyps. They are assumed to be caused by chronic inflammation and regenerative proliferation, although this has not been clearly investigated yet. Many studies suggested the development of fundic gland polyps and carcinoid during long-term proton pump inhibitor (PPI) therapy, but the relationship between PPIs and HPPs is still unclear. We encountered a patient who showed aggravation of HPPs after long-term use of PPIs. A 58-year-old male patient with liver cirrhosis visited our hospital because of hematemesis. We started PPI medication after confirming esophageal variceal bleeding and duodenal ulcer with blood clot in its base via emergency endoscopy. He took PPIs for three years because of an intractable duodenal ulcer. There was a marked increase in the size of the pre-existing polyps and in the development of new polyps. We presumed that the PPIs caused the aggravation of the HPPs, so we stopped their administration. After five months, the HPPs shrank and the polyps were partially degraded. More prospective studies are needed to investigate the relationship between HPPs and PPIs.

COP Improvement of Heat Pump with Regenerative Cycle (열재생 사이클을 이용한 히트펌프의 난방 성능 향상에 관한 연구)

  • 유영선;장진택;김영중;윤진하;이건중
    • Proceedings of the Korean Society for Agricultural Machinery Conference
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    • 1999.07a
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    • pp.320-325
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    • 1999
  • 세계기후협약으로 인하여 우리나라는 화석연료 사용량을 최소한 2010년까지 2000년 수준으로 감축시켜야할 처지에 놓여 있다. 따라서 지구 온난화의 주 요인이 되고 있는 이산화탄소 배출량을 2010년 예상배출량의 21%정도를 감축해야 하며, 경제활동은 1/4이상이 축소되는 영향을 받게 된다(차재호, 1998). 따라서 현재의 화석에너지에 의존하는 난방법은 자연에너지 또는 전기에너지 등으로 대부분이 전환되어야 할 것으로 전망하고 있다 그러나 농업에 이용되고 있는 난방에너지는 화석에너지에 집중되어 있으며, 온실, 축사, 버섯재배사 등에서 겨울철 난방에 소요되는 에너지 비용은 총경영비의 10-40%를 차지하고 있다. (중략)

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