• Title/Summary/Keyword: 2단 원심압축기

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Centrifugal Compressor Performance Assessment by Experiments and Numerical Simulations (수치해석 및 성능시험을 통한 원심압축기 성능 평가)

  • Kang, Young-Seok;Park, Tae-Choon;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.341-344
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    • 2009
  • 본 연구에서는 허브 대 팁의 비가 큰 원심형 압축기의 성능시험을 수행하였으며, 이를 수치해석 결과와 비교하였다. 압력비의 경우 작동 회전수에서 성능시험과 수치해석의 결과의 경향이 일치하는 것을 확인하였다. 성능시험에서 임펠러의 성능은 매우 높게 나타났으나, 1단 및 2단 디퓨져에서 손실이 발생하여 전체적인 압력비 및 효율이 떨어지는 것을 확인하였다. 수치해석을 통해 내부 유동장을 확인한 결과 1단 디퓨져 및 2단 디스월러에서 격렬한 2차 유동으로 인한 유로차폐효과가 주 손실원인임을 확인하였다.

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Numerical Analysis Techniques and Flow Characteristics of Two-Stage Centrifugal Compressor for R134a Turbo-Chiller (R134a 터보 냉동기용 2단 원심 압축기의 수치해석 기법과 내부유동 특성)

  • Park, Han-Young;Oh, Hyun-Taek;Shin, You-Hwan;Lee, Yoon-Pyo;Kim, Kwang-Ho;Chung, Jin-Taek
    • The KSFM Journal of Fluid Machinery
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    • v.10 no.4
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    • pp.29-38
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    • 2007
  • In this study, flow structure in a two-stage centrifugal compressor for a turbo-chiller with the refrigerant, R134a, was numerically investigated at the design point of the compressor using a commercial code. Flow characteristics in the passages of impeller, diffuser and return channel were analyzed in detail including velocity vector, secondary flow, Mach number and pressure contours in blade spanwise and meridional plane for each stage. The estimation on the one-dimensional output from the preliminary design and three-dimensional shape of the impeller blade and the meridional shape of the return channel were performed through the flow analysis, while some numerical schemes and techniques including Multiple Frames of Reference technique, real gas property data and inlet boundary condition changes, which were used in CFD, were compared with their features. The results will be used as reference data for a new design of 3-D impeller shape to improve R134a compressor performance.

Instrumentation for Performance Test of Turbo Compressor (터보 압축기 성능시험을 위한 계측기기 선정)

  • Park, Tae-Choon;Kang, Young-Seok;Yang, Soo-Seok
    • Aerospace Engineering and Technology
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    • v.7 no.2
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    • pp.46-52
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    • 2008
  • The instrumentation was studied in order to measure aerodynamic performance and efficiency of a compressor as a component of a 5MW-class gas turbine for power generation. In case of an axial compressor, the distributions of static pressure on a casing can be obtained by averaging at each stage and those of total pressure and temperature in the flow field of the compressor can be measured with a Kiel temperature probe. In case of a centrifugal compressor, the static pressures at the hub and the tip, respectively, of an impeller exit are considerably different, so the pressures need to be measured at both positions and thereafter averaged. The distributions of static pressures in a diffuser and a deswirler are measured at ten positions along five streamlines in one pitch. In addition the flow field can be measured in detail by 5-hole Pitot tube in order to analyze the flow characteristics of the core flow region and wake region and the rotor-stator interaction of the compressor.

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A Steady-State Simulation and Experimental Study of Turboshaft Engine with Free Power Turbine (분리축방식 터보축 엔진의 정상상태 모사 및 실험연구)

  • 공창덕;기자영;고광웅
    • Journal of the Korean Society of Propulsion Engineers
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    • v.1 no.2
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    • pp.84-90
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    • 1997
  • The turboshaft engine with the free power turbine has been used for various purposes, for instance electric power generator, emergency power source, helicopter powerplant and so on. Steady-state simulation program was developed and experimental tests was carried out for comparing with computer simulation results. The test unit was composed of 1-stage centrifugal compressor, the can type combustor chamber, 1-stage radial type compressor turbine, and radial type free power turbine, and its output power is obtained from 3-phase AC generator. Main component characteristics which was used for the steady state simulation program, were obtained from the manufacturer of the test unit, and modified from experimental results of test unit. In comparison between computer simulation and experimental test results even though the test unit has the operational limit, deviation of component performance characteristics in simulation were within 6% range of experimental results.

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INFLUENCES OF DRY METHODS OF RETROCAVITY ON THE APICAL SEAL (치근단 역충전와동의 건조방법이 폐쇄성에 미치는 영향)

  • Lee, Jung-Tae;Kim, Sung-Kyo
    • Restorative Dentistry and Endodontics
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    • v.24 no.1
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    • pp.166-179
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    • 1999
  • Apical sealing is essential for the success of surgical endodontic treatment. Root-end cavity is apt to be contaminated with moisture or blood, and is not always easy to be dried completely. The purpose of this study was to evaluate the influence of dry methods of retrocavity on the apical seal in endodontic surgery. Apical seal was investigated through the evaluation of apical leakage and adaptation of filling material over the cavity wall. To investigate the influence of various dry methods on the apical leakage, 125 palatal roots of extracted human maxillary molar teeth were used. The clinical crown of each tooth was removed at 10 mm from the root apex using a slow-speed diamond saw and water spray. Root canals of the all the specimens were prepared with step-back technique and filled with gutta-percha by lateral condensation method. After removing of the coronal 2 mm of filling material, the access cavities were closed with Cavit$^{(R)}$. Two coats of nail polish were applied to the external surface of each root. Apical three millimeters of each root was resected perpendicular to the long axis of the root with a diamond saw. Class I retrograde cavities were prepared with ultrasonic instruments. Retrocavities were washed with physiologic saline solution and dried with various methods or contaminated with human blood. Retrocavities were filled either with IRM, Super EBA or composite resin. All the specimens were immersed in 2% methylene blue solution for 7 days in an incubator at $37^{\circ}C$. The teeth were dissolved in 14 ml of 35% nitric acid solution and the dye present within the root canal system was returned to solution. The leakage of dye was quantitatively measured via spectrophotometric method. The obtained data were analysed statistically using one-way ANOVA and Duncan's Multiple Range Test. To evaluate the influence of various dry methods on the adaptation of filling material over the cavity wall, 12 palatal roots of extracted human maxillary molar teeth were used. After all the roots were prepared and filled, and retrograde cavities were made and filled as above, roots were sectioned longitudinally. Filling-dentin interface of cut surfaces were examined by scanning electron microscope. The results were as follows: 1. Cavities dried with paper point or compressed air showed less leakage than those dried with cotton pellet in Super EBA filled cavity (p<0.05). However, there was no difference between paper point- and compressed air-dried cavities. 2. When cavities were dried with compressed air, dentin-bonded composite resin-filled cavities showed less apical leakage than IRM- or Super EBA-filled ones (p<0.05). 3. Regardless of the filling material, cavities contaminated with human blood showed significantly more apical leakage than those dried with compressed air after saline irrigation (p<0.05). 4. Outer half of the cavity showed larger dentin-filling interface gap than inner half did when cavities were filled with IRM or Super EBA. 5. In all the filling material groups, cavities contaminated with blood or dried with cotton pellets only showed larger defects at the base of the cavity than ones dried with paper points or compressed air.

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