• Title/Summary/Keyword: micro turbine

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Rotordynamic Design of the Micro Gas Turbine Supported by Air Foil Bearings (공기포일베어링에 지지된 마이크로가스터빈의 회전체동역학적 설계)

  • Kim, Young-Cheol;Han, Jung-Wan;Kim, Kyung-Woong;Kim, Soo-Yong
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.662-667
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    • 2003
  • This paper presents a performance analysis of the 1st generation bump foil journal bearings for the micro gas turbine TG75. Static performances such as load capacity and attitude angle are estimated by using soft elasto-hydrodynamic analysis technique, and dynamic performances such as stiffness and damping coefficients are estimated by perturbation method. Rotordynamic analysis for TG75 is performed by using the bearing analysis results. TG75 rotor has 2 horizontal and vertical directional natural modes due to the bearing stiffness characteristics. TG75 rotor will be stably operated between the 1st bending mode at 33000cpm and the 2nd bending mode at 85500cpm. Unbalance response analysis results satisfy the API vibration criteria.

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Performance Characteristics and Efficiencies of Micro-Hydro Pelton Turbine with Nozzle Diameter Variation (노즐 구경에 따른 초소수력 펠턴 터빈의 효율 및 성능 특성)

  • Jo, In Chan;Park, Joo Hoon;Shin, Youhwan;Kim, Kwang Ho;Chung, Jin Taek;Kim, Dong Ik
    • The KSFM Journal of Fluid Machinery
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    • v.18 no.3
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    • pp.60-65
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    • 2015
  • This paper deals with performance characteristics and efficiencies of Pelton turbine can be applied as one of ERDs (Energy Recovery Devices) of PRO (Pressure Retarded Osmosis) system for desalination. The objective of this study is experimentally estimating the performance of micro-scale Pelton turbine for PRO pilot plant. Especially the performance characteristics with variations of jet nozzle diameter of Pelton turbine are discussed in detail. In order to do this, lab scale test rig of Pelton turbine was made for performance test, which includes water tank, Pelton wheel with buckets, jet nozzle and torque brake and so on. The parameter effects related on Pelton turbine's efficiency were investigated and discussed on the influence of the variations of load and speed ratio.

Development of the Micro Tool Dynamometer for Micro Machining (미세가공을 위한 마이크로 공구동력계 개발)

  • Kwon D.H.;Hwang I.O.;Kang M.C.;Kim J.H.;Kim J.S.;Ahn J.H.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2006.05a
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    • pp.217-218
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    • 2006
  • This paper presents an investigation on the characteristics for new micro tool dynamometer by using the ultrahigh-speed air turbine spindle. Recently, the ultrahigh-speed micro flat endmilling has been investigated actively due to request of accuracy improvement and productivity of die and mould manufacturing. To perform efficient ultrahigh-speed micro flat endmilling, evaluation of ultrahigh-speed machinability must be studied preferentially and it can be identified by investigation of cutting force. The cutting forces in ultrahigh-speed micro flat endmilling can be measured by micro tool dynamometer. But general dynamometer has low natural frequency and so is improper for measuring very high frequency cutting forces in ultrahigh-speed micro flat endmilling. In this study, the micro tool dynamometer which has very high natural frequency is newly designed.

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Micro Power System Development (마이크로 파워 시스템의 개발)

  • Park, Kun-Joons;Jeon, Byung-Sun;Min, Hong-Seok;Song, Seung-Jin;Min, Kyoung-Doug;Joo, Young-Chang
    • 유체기계공업학회:학술대회논문집
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    • 2001.11a
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    • pp.381-386
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    • 2001
  • This paper reports on the development of micro power system under way at Seoul National University. The interdisciplinary tin consists of members with various backgrounds of mechanics and materials. The need for micro power systems is explained, and a turbine under development is described. Design, and fabrication are introduced, and technical challenges in each phase are described. Furthermore, the interaction between the available fabrication methods and design is explained. Design involves use of commercially available codes to analyze flow fields, and fabrication takes advantage of the silicon wafer etching processes used to manufacture semiconductor devices.

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Analysis of Design and Part Load Performance of Micro Gas Turbine/Organic Rankine Cycle Combined Systems

  • Lee, Joon-Hee;Kim, Tong-Seop
    • Journal of Mechanical Science and Technology
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    • v.20 no.9
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    • pp.1502-1513
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    • 2006
  • This study analyzes the design and part load performance of a power generation system combining a micro gas turbine (MGT) and an organic Rankine cycle (ORC). Design performances of cycles adopting several different organic fluids are analyzed and compared with performance of the steam based cycle. All of the organic fluids recover greater MGT exhaust heat than the steam cycle (much lower stack temperature), but their bottoming cycle efficiencies are lower. R123 provides higher combined cycle efficiency than steam does. The efficiencies of the combined cycle with organic fluids are maximized when the turbine exhaust heat of the MGT is fully recovered at the MGT recuperator, whereas the efficiency of the combined cycle with steam shows an almost reverse trend. Since organic fluids have much higher density than steam, they allow more compact systems. The efficiency of the combined cycle, based on a MGT with 30 percent efficiency, can reach almost 40 percent. hlso, the part load operation of the combined system is analyzed. Two representative power control methods are considered and their performances are compared. The variable speed control of the MGT exhibits far better combined cycle part load efficiency than the fuel only control despite slightly lower bottoming cycle performance.

Prediction of Power and Efficiency Requirement of Motor/generator for 500W Class Micro Gas Turbine Generator Considering Losses (손실을 고려한 500W급 마이크로 가스터빈 발전기용 전동발전기의 요구동력 및 요구효율 선정)

  • Park, Cheol-Hoon;Choi, Sang-Kyu;Ham, Sang-Yong
    • The KSFM Journal of Fluid Machinery
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    • v.14 no.5
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    • pp.24-30
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    • 2011
  • 500W class MTG(Micro turbine generator) operating at 400,000 rpm is under development. From the cycle analysis, it is decided that the self-sustaining speed of MTG is 200,000rpm and the generating speed is 400,000 rpm. Therefore, motor should be designed so that it is able to rotate the rotor up to 200,000rpm and generator should designed so that it is able to generate 500W output at 400,000rpm. First step to design motor/generator is to determine the power and efficiency requirement. Not only the power into the compressor and from the turbine at the operating speed but also the mechanical and electrical losses should be considered in determining the power and efficiency requirement. This study presents the procedure and the results of determining the power and efficiency requirement considering the mechanical and electrical losses depending on the rotating speed which is measured from the experiment.

The Low NOx Characteristics of the Primary Zone in Micro Turbine Combustor (마이크로 터빈 연소기 주연소영역의 저 NOx 생성 특성)

  • Son, M.G.;Ahn, K.Y.;Lee, H.S.;Yoon, J.J.
    • Proceedings of the KSME Conference
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    • 2001.11b
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    • pp.155-160
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    • 2001
  • The low NOx characteristics have been investigated to develop the combustor for micro turbine. The lean premixed combustion technology was applied to reduce the NOx emission. The test was conducted at the condition of high temperature and ambient pressure. The combustion air which has the temperature of $450\sim650K$ were supplied to the combustor through the air preheater. The temperature and emissions of NOx and CO were measured at the exit of combustor, The exit temperature and NOx were increased and CO was decreased with increasing inlet air temperature. The premixing chamber can be operated very lean condition of equivalence ratio around 0.35. The NOx was decreased with decreasing the equivalence ratio. The CO was decreased with decreasing the equivalence ratio, but the CO was increased with decreasing the equivalence ratio below 0.4. But, at the very lean condition of equivalence ratio below 0.35 both NOx and CO were increased because of the flame unstability. The NOx was decreased and CO was increased with increasing inlet air flowrate. This results can be used to determine the size of combustor. Consequently the performance of combustor shows the possibility of the application to the gas turbine system.

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The Energy Performance & Economy Efficiency Evaluation of Micro Gas Turbine Installed in Hospital (대형병원 건물에 마이크로 가스터빈 적용을 위한 에너지성능 및 경제성 평가)

  • Kim, Byoung-Soo;Hong, Won-Pyo
    • Journal of the Korean Solar Energy Society
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    • v.29 no.5
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    • pp.8-13
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    • 2009
  • Feasibilities of the application of a micro gas turbine cogeneration system to a large size hospital building are studied by estimating energy demands and supplies. The energy demand for electricity is estimated by surveying and sorting the consumption records for various equipment and devices. The cooling heating, and hot water demands are further refined with TRNSYS and ESP-r to generate load profiles for the subsequent operation simulations. The operation of the suggested cogeneration system in conjunction with the load data is simulated for a time span of a year to predict energy consumption and gain profile. The simulation revealed that the thermal efficiency of the gas turbine is about 30% and it supplies 60% of the electricity required by the building. The recovered heat can meet 56% of total heating load and 67% of cooling, and the combined efficiency reaches up to 70%.

Analysis of Operation Performance of a Micro Gas Turbine Generator System (마이크로 가스터빈 발전시스템의 운전성능 분석)

  • Lee, J. J.;Kim, T. S.
    • The KSFM Journal of Fluid Machinery
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    • v.8 no.5 s.32
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    • pp.13-21
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    • 2005
  • This study aims to analyze operating performance of a micro gas turbine with the aid of detailed measurements of various system parameters. In addition to embedded measurements, parameters such as exhaust temperatures, engine inlet temperatures and fuel flow rates are measured. Variations in measured data and estimated performance parameters are analyzed. Those data are processed to calculate losses along the power transmission line and the net gas turbine performance (power and efficiency based on the gas turbine shaft end) is isolated from the overall system performance. A method to estimate characteristic parameters such as component efficiencies, based on the comparison between measured and predicted performance data, is suggested and exemplified for the full load condition.

Performance Characteristics and Prediction on a Partially Admitted Single-Stage Axial-Type Micro Turbine (부분분사 축류형 마이크로터빈에서의 성능예측 및 성능특성에 관한 연구)

  • Cho, Chong-Hyun;Cho, Soo-Yong;Choi, Sang-Kyu
    • 유체기계공업학회:학술대회논문집
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    • 2005.12a
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    • pp.324-330
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    • 2005
  • For axial-type turbines which operate at partial admission, a performance prediction model is developed. In this study, losses generated within the turbine are classified to windage loss, expansion loss and mixing loss. The developed loss model is compared with experimental results. Particularly, if a turbine operates at a very low partial admission rate, a circular-type nozzle is more efficient than a rectangular-type nozzle. For this case, a performance prediction model is developed and an experiment is conducted with the circular-type nozzle. The predicted result is compared with the measured performance, and the developed model quite well agrees with the experimental results. So the developed model could be applied to predict the performance of axial-type turbines which operate at various partial admission rates or with different nozzle shape.

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