• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.279-282
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• 2002

Recently, gas turbines for power generation adopt multistage DLN(Dry Low NOx) type combustion, where diffusion combustion is applied at low load and, with increase in load, the combustion mode is changed to lean premixed combustion to reduce NOx emissive concentration. However, during the mode changeover from diffusion to premixed flame, unfavorable phenomena, such as flashback, high amplitude combustion oscillations, or thermal damage of combustor parts could frequently occur. In the present study, to apply for the analysis of such unfavorable phenomena, three-dimensional CFD investigations are carried out to compare the detailed flow characteristics and temperature distribution inside the gas turbine combustor before and after combustion mode changeover. The fuel considered here is pure methane gas. A standard $k-{\varepsilon}$ turbulence model with wall function and a P-N type radiation heat transfer model, have been utilized. To analyze the complex geometric effects of combustor parts on combustion characteristics, fuel nozzles, a swirl vane f3r fuel-air mixing, and cooling air holes on the combustor liner wall, are included in this simulation.

• 대한토목학회논문집
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• 제40권3호
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• pp.315-320
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• 2020

목재 부산물 등을 활용하여 제조되는 목재펠릿(pellet)은 가공되는 방식과 추가되는 부산물의 종류, 목재펠릿난로의 종류에 따라 완전연소가 아닌 불완전연소가 일어나는 경우가 있다. 이에 본 연구에서는 불완전연소로 인한 환경오염과 에너지 낭비를 줄이기 위해 목재펠릿난로 연소 작용의 핵심부인 연소기를 개발하였다. 현재 시중에서 유통되고 있는 목재펠릿난로의 연소 작용을 담당하고 있는 연소기의 한계점을 넘기 위해 다층구조(Multi Layer)방식이라 명명하는 새로운 구조의 연소기 방식을 창안하고, CAD (Computer Aided Design) program으로 설계 후 3D 프린터를 활용하여 실현 가능성을 검증하였다. 검증된 데이터를 바탕으로 다층구조(Mulit Layer)방식의 목재펠릿난로의 연소 작용을 담당하는 연소기의 시제품(Prototype)을 설계, 제작하여 실험을 진행하였다. 실험의 신뢰도를 위해 동일한 날짜, 장소, 연료를 사용하여 현재 시중에서 유통되어 판매되고 있는 목재펠릿난로의 연소기와 본 연구에서 개발한 목재펠릿난로의 연소기를 비교실험하였다. 실험의 결과로 환경적인 측면에서 일산화탄소(Carbon Monoxide) 배출량의 감소를 확인하였고, 에너지 효율면에서 상대적으로 높은 열효율 결과를 도출하여 긍정적인 결과를 나타냈다.

• 대한기계학회논문집B
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• 제33권2호
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• pp.141-148
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• 2009

Axial-flow compressor is one of the most important parts of gas turbine units with axial turbine and combustor. Therefore, precise prediction of performance is very important for development of new compressor or modification of existing one. Meanline analysis is a simple, fast and powerful method for performance prediction of axial-flow compressors with different geometries. So, Meanline analysis is frequently used in preliminary design stage and performance analysis for given geometry data. Much correlations for meanline analysis have been developed theoretically and experimentally for estimating various types of losses and flow deviation angle for long time. In present study, meanline analysis program was developed to estimate compressor losses, incidence angles, deviation angles, stall and surge conditions with many correlations. Performance prediction of one stage axial compressors is conducted with this meanline analysis program. The comparison between experimental and numerical results show a good agreement. This meanline analysis program can be used for various types of single stage axial-flow compressors with different geometries, as well as multistage axial-flow compressors.