• 한국추진공학회지
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• 제23권3호
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• pp.9-17
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• 2019

가스터빈 압축기의 가변정익은 다수의 정익을 동시에 회전시킬 수 있도록 하는 가변정익 링크메커니즘과 이를 동작시키는 구동시스템으로 구성된다. 본 연구에서는 총 3단으로 구성된 가변정익을 2개의 유압구동기로 작동시킬 수 있는 가변정익 구동시스템을 개발하였다. 가변정익의 공력하중과 링크메커니즘 기구분석을 통해 구동기의 요구 성능을 도출하고, 파워팩을 포함한 유압구동시스템을 개발하였다. 부하 시험장치를 이용하여 개발한 구동기의 성능을 평가하였으며, 최적의 제어 이득과 동기제어로직을 적용하여 항공용 가스터빈 시험을 위한 가변정익 구동시스템을 개발 완료하였다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2004년도 ICCAS
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• pp.1211-1214
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• 2004

In this paper, we propose to use variable inlet guide vane as a means of active surge control to solve above problems. There is some advantage. For example, since the inlet guide vanes are already present in POSCO, no additional actuation device is required. We can collect all data easily which is related to the test and can simulate new model using our compressors. We can obtain the result that blow-off valve is opened less 5% and can operate air compressor automatically and more efficiently. Through a simulation example, the effectiveness of the proposed schemes is illustrated.

• 대한기계학회논문집B
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• 제24권8호
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• pp.1077-1084
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• 2000

In this work, a modified stage-stacking method for the performance prediction of multi-stage axial flow compressors is proposed. The method is based on a simultaneous calculation of all interstage variables (temperature, pressure, flow velocity) instead of the conventional sequential stage-by-stage scheme. The method is also very useful in simulating the effect of changing angles of the inlet guide vane and stator vanes on the compressor operating characteristics. Generalized stage performance curves are used in presenting the performance characteristics of each stage. General assumptions enable determination of flow path data and stage design performance. Performance of various real compressors is predicted and comparison between prediction and field data validates the usefulness of the present method.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.979-984
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• 2001

As a preceding process for developing design technology and establishing operation technology, the design procedure of the SCR(Selective Catalytic Reduction) pilot plant that can handle $1,000Nm^{3}/hr$ of flue gas was reported in this paper. And we also considered several factors that might cause abnormality of the plant in the designing process. The plant was designed and fabricated to test the $DeNO_{x}$ performances in variable operating conditions in the range of $3,000{\sim}36,000hr^{-1}/hr$ in space velocities, $1.67{\sim}6\;m/s$ in linear velocities, $200{\sim}500^{\circ}C$ temperatures, $300{\sim}1,000Nm^{3}/hr$ flow rates, and $0{\sim}1.4:1\;NH_{3}/NO$ ratios. In order to maintain the flow uniformity, the guide vanes and flow straightener were designed and constructed in the plant. The SCR pilot plant can be operated by the automatic control system, which enable to obtain performance data in real time and to set up the operating technology. The catalyst reactor consists of 4 catalyst layers and surface area of each layer can be adjusted to be of small size. Arrangement of catalysts per layer is $3{\times}6$ with the catalyst dimensions of $150{\times}150{\times}500mm(L{\times}W{\times}H)$.