• 제목/요약/키워드: Inlet-Air Temperature

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직결형 초음속 연소기 시험 설비 개발 (Development of a Direct-Connected Supersonic Combustor Test Facility)

  • 양인영;이경재;이양지;김형모
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.290-293
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    • 2017
  • 스크램젯 엔진용 초음속 연소기 연구를 위한 직결형, 연속식 연소 시험 설비를 개발하였다. 비행체 속도 마하 5, 연소기 입구 유속 마하 2를 가정하고, 시험 대상 연소기의 유로 단면은 높이 32 mm, 폭 70 mm로 가정하여 설비 요구 조건을 결정하였다. 이에 따라 설비는 유동 전압력 548 kPaA, 전온도 1,320 K, 유량 0.776 kg/s로 설계하였다. 설비는 터보형 압축기, 전기 가열기 및 연소식 가열기와 그 하류에 유동 가속을 위해 장착한 마하 2의 2차원 노즐로 구성하였다. 노즐 상류에서 산소를 추가 공급하여 연소식 공기 가열에 의한 산소 감소를 보상하도록 하였다. 배기는 별도의 감압은 하지 않았다. 저압, 저유량에서의 시운전을 수행하였으며, 설계점 운전은 향후 계획 중에 있다.

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無燃炭 燃燒에 關한 硏究 (第 1 報). 一酸化炭素 燃燒反應 및 燃燒裝置 (Studies on the Combustion of Anthracite (I). Combustion of Carbon Monoxide and the Furface)

  • 신병식;신세건
    • 대한화학회지
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    • 제19권3호
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    • pp.186-192
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    • 1975
  • 燃炭을 燃燒시킬 때 흙통중에서 一定量의 煉炭을 一定時間 燃燒를 持續시키기 위하여 空氣의 供給을 制限하게 되므로 많은 量의 一酸化炭素가 發生한다. 그러므로 一酸化炭素의 發生을 抑制하는 基本實驗으로 窒素, 酸素 및 一酸化炭素의 混合가스 및 炭素의 存在下에서 一酸化炭素의 燃燒率을 測定한 結果 一酸化炭素 燃燒溫度는 $700^{\circ}C$以上이고 空氣의 供給이 增加 할수록 一酸化炭素의 燃燒率이 改善됨을 알았다. 이러한 事實에서 燃燒時間의 延長과 一酸化炭素의 發生 抑制는 서로 相反되므로 두 가지 條件을 滿足시키는, 보다 效果的 燃燒裝置를 考案하였다. 즉 內徑이 다른 二重鐵筒으로 暖爐를 만들어 若干의 二次空氣가 에어자켓 下部에서 들어가 上部의 작은 구멍에서 나오게끔 하면 燃燒中인 煉炭과 熱交換되어 燃燒雰圍氣의 溫度는 低下된다. 따라서 燃燒時間은 길어지면 또 二重鐵筒을 通하여 上昇하는 豫熱空氣는 一酸化炭素의 再演燒를 促進시키게 되므로 一酸化炭素의 發生量은 흙통을 使用하였을때 보다도 1/20 程度로 減少된다.

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공급 유량 및 당량비 변화에 따른 초소형 가스터빈 연소실 내 수소/공기 연소의 수치해석 연구 (Numerical Study of Hydrogen/Air Combustion in Combustion Chamber of Ultra Micro Gas Turbine by Change of Flow Rate and Equivalence Ratio)

  • 권길성;황유현;강호;김대중
    • 대한기계학회논문집B
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    • 제37권2호
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    • pp.103-109
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    • 2013
  • 본 연구에서는 초소형 가스터빈 연소기에서의 수소/공기 연소에 대한 수치해석을 연소기 입구에서의 공급 유량 및 유체의 수소/공기 혼합비 변화에 대하여 수행하였다. 수치해석은 상용화 프로그램인 STAR-CCM 을 이용하였다. 유체의 공급 유량의 변화는 연소기 내 화염의 위치와 온도, 입구와 출구의 압력비 등에 상당한 영향을 주었다. 유체의 공급 유량이 증가할 때, 연소기 내의 화염은 점점 출구 방향으로 위치하였고, 화염의 온도 및 입구와 출구의 압력비는 단조적으로 증가하였다. 유체의 수소/공기 혼합비 변화는 화염의 위치에는 큰 영향을 주지 않았고, 이론공연 상태에서 연소실 내에 가장 높은 화염온도를 가졌다.

지열원 히트펌프시스템의 실사용을 통한 난방성능연구 (Heating Performance of a Ground Source Heat Pump System through Actual Operation)

  • 구경민;정영만;황유진;이재근;장세용;김인규;진심원;이동혁
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.1341-1346
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    • 2008
  • This paper presents the heating performance of a water-to-refrigerant type ground source heat pump system (GSHP) installed in a school building. The evaluation of the heating performance has been conducted under the actual operating conditions of GSHP system in the winter. Ten units with the capacity of 10 HP each were installed in the building. Also, a closed vertical typed-ground heat exchanger with 24 boreholes of 175 m in depth was constructed for the GSHP system. For analyzing the heating performance of the GSHP system, we monitored various operating conditions, including the outdoor temperature, the ground temperature, and the water temperature of inlet and outlet of the ground heat exchanger. Simultaneously, the heating capacity and the input power were evaluated for determining the heating performance of the GSHP system. The average heating coefficient of performance (COP) of the heat pump was found to be 5.1 at partial load of 46.9%, while the overall system COP was found to be 4.2.

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지열원 히트펌프시스템의 실사용을 통한 난방성능연구 (Heating Performance of a Ground Source Heat Pump System through Actual Operation)

  • 구경민;정영만;황유진;이재근;장세용;김인규;진심원;이동혁
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.788-793
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    • 2008
  • This paper presents the heating performance of a water-to-refrigerant type ground source heat pump system (GSHP) installed in a school building. The evaluation of the heating performance has been conducted under the actual operating conditions of GSHP system in the winter. Ten units with the capacity of 10 HP each were installed in the building. Also, a closed vertical typed-ground heat exchanger with 24 boreholes of 175 m in depth was constructed for the GSHP system. For analyzing the heating performance of the GSHP system, we monitored various operating conditions, including the outdoor temperature, the ground temperature, and the water temperature of inlet and outlet of the ground heat exchanger. Simultaneously, the heating capacity and the input power were evaluated for determining the heating performance of the GSHP system. The average heating coefficient of performance (COP) of the heat pump was found to be 5.1 at partial load of 46.9%, while the overall system COP was found to be 4.2.

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균일 열플럭스가 있는 $180^{\circ}C$ 원형단면 곡관의 선회유동 열전달특성 연구 (A study on the heat transfer characteristics of swirling flow in a circular sectioned $180^{\circ}C$bend with uniform heat flux)

  • 이상배;권기린;장태현
    • 대한기계학회논문집B
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    • 제21권5호
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    • pp.615-627
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    • 1997
  • An experiment was performed to local heat transfer coefficient and Nusselt number in the circular duct of 180.deg. bend for Re=6*10$^{4}$, 8*10$^{4}$ and 1*10$^{5}$ at swirling flow and non-swirling flow conditions. The test tube with circular section was made by stainless which has curvature ratio 9.4. The wall of test tube was heated directly by electrical power to 3.51 kw and swirling motion of air was produced by a tangential inlet to the pipe axis at the 180 degree. Measurements of local wall temperatures and bulk mean temperature of air are made at four circumferential positions in the 16 stations. The wall temperatures show particularly reduced distribution curve at bend for non-swirling flow but this effect does not appear for swirling flow. Nusselt number distributions for swirling flow which was calculated from the measured wall and bulk temperatures were higher than that of non-swirling flow. Average Nusselt number of swirling flow increased about 90 ~ 100% than that of non-swirling flow whole through the test tube. The Nu/N $u_{DB}$ values at the station of 90.deg. for non-swirling flow and swirling flow are respectively about 2.5 and 4.8 at Re=6*10$^{4}$. Also that is good agreement with Said's result for non-swirling flow. flow.

Performance Analysis of an Aircraft Gas Turbine Engine using Particle Swarm Optimization

  • Choi, Jae Won;Sung, Hong-Gye
    • International Journal of Aeronautical and Space Sciences
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    • 제15권4호
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    • pp.434-443
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    • 2014
  • A turbo fan engine performance analysis and the optimization using particle swarm optimization(PSO) algorithm have been conducted to investigate the effects of major performance design parameters of an aircraft gas turbine engine. The FJ44-2C turbofan engine, which is widely used in the small business jet, CJ2 has been selected as the basic model. The design parameters consists of the bypass ratio, burner exit temperature, HP compressor ratio, fan inlet mass flow, and nozzle cooling air ratio. The sensitivity analysis of the parameters has been evaluated and the optimization of the parameters has been performed to achieve high net thrust or low specific fuel consumption.

프로세스 배관계의 3차원 유동해석 (3-D Flow Simulation of Process Piping System)

  • 양희천;박상규
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.469-473
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    • 2001
  • It is very important that piping system shall meet the optimum design requirement as predicted in designing system. If the piping system proved not to meet the requirement in commission it shall be redesigned and corrected till the required capacity is satisfied. which costs much expense. The objective of this study is to understand steady 3-dimensional flow phenomena in a process piping system numerically. 3-dimensional numerical simulations with standard $k-{\epsilon}$ model were carried out by using ALGOR code for three cases of Reynolds number. 2500, 3500 and 4500, based on inlet pipe diameter and three cases of inflow air temperature, $20^{\circ}C,\;50^{\circ}C$ and $100^{\circ}C$.

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세라믹 가스 터빈용 촉매연소기의 연소특성 (Combustion Characterisitics of a Catalytic Combustorfor an Automotive Ceramic Gas Turbine)

  • 김영일
    • 한국산업융합학회 논문집
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    • 제1권2호
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    • pp.49-54
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    • 1998
  • In the catalytic combustor, combustion characteristic and deterioration of catalysts were affected by non-uniformity of pre-mixed gas, Therefore, formation of uniform pre-mixed gas is one of important subjects. In this study, the effect of uniformity and non-uniformity of pre-mixed gas supplied to the catalyst was examined to clarify reaction acceleration and combustion characteristic of the catalytic combustion. It was clarified that static mixer or vaporizer tube length of about 150mm and weak swirl to a combustion air were effictive expedient to make uniform pre-mixed gas. And catalystic inlet temperature needs more than $600^{\circ}C$ with rich pre-mixed gas to active reaction.

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상용 열유동 해석 소프트웨어를 이용한 다이캐스팅 칠벤트의 성능평가 (Evaluation on Performance of Chill Vent in High Pressure Die Casting by Using a Commercial Software)

  • 강복현;김태범;김기영
    • 한국주조공학회지
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    • 제32권3호
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    • pp.133-137
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    • 2012
  • Chill vent has a zigzag venting path which allows residual air or gases to exhaust out very quickly from the die cavity. However molten metal sometimes comes out through the gas venting surfaces causing flash. Effect of designing factors of chill vent and processing variables in high pressure die casting on the performance of chill vent was investigated through a series of calculations by using a commercial code. The most influential factor was the thickness of chill vent, followed by inlet velocity, vent width and die temperature.