• Title/Summary/Keyword: Flame stable region

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A Study on the Development of Low NOx Condensing Gas Boiler(I) -Design of Cylindrical Multi-Hole Premixed Burner- (저 NOx 응축형 가스보일러 개발에 관한 연구(I) -원통형 다공 예혼합 연소기 설계-)

  • Lee, Chang-Eon;Geum, Seong-Min;Jeong, Yeong-Sik;Lee, Gyu-Yeong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.2
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    • pp.235-243
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    • 2001
  • This paper describes a design study of the cylindrical multi-hole premixed burner to be used for condensing gas boiler which can raise performance and reduce NOx emission. In this study, specifications of the multi-hole burner (hole diameters and arrangement) are investigated using model flat burners in terms of flame stability, and combustion characteristics for stability and NOx emission are examined for cylindrical multi-hole burner. As a result, the equivalence ratio for optimum operation condition of the cylindrical burner is around 0.72(0.7∼0.75). In this condition, turn-down ratio becomes 3 : 1 at least which is suitable for proportional control. The NOx and CO emission is less than 40ppm and 25ppm(0$_2$0% basis), respectively. This burner can be applied LPG as well as NG because there is no difference for stable combustion region.

Stability Rating Tests for Optimization of Axial Baffle Length (배플 길이의 최적화를 위한 연소 안정성 평가 시험)

  • Kim, Hong-Jip;Lee, Kwang-Jin;Seo, Seong-Hyeon;Kim, Seung-Han;Han, Yeoung-Min;Seol, Woo-Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.1
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    • pp.69-77
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    • 2005
  • To optimize and limit the axial length of the baffle of the KSR-III engine, stability rating tests using pulse gun as one of artificial disturbance devices have been done. Generally a rocket engine can be considered to be dynamically stable if a certain imposed external perturbation or pressure oscillation in rocket combustion chamber could be suppressed within a short time period. Decay time and other parameters for the evaluation of stabilization ability of an engine to external perturbation have been analyzed to quantify stabilization capacity of engine, in other words, dynamic stability margin. Baffle not covering flame zone enough which can be considered as collision region of injector wasn't be able to suppress external perturbation sufficiently. The limit of combustion stability margin of engine is assumed to be 50 mm length baffle of the KSR-III engine.

Effects of Hydrogen in SNG on Gas Turbine Combustion Characteristics (합성천연가스의 수소함량 변화에 따른 가스터빈 연소특성 평가)

  • Park, Se-Ik;Kim, Ui-Sik;Chung, Jae-Hwa;Hong, Jin-Pyo;Kim, Sung-Chul;Cha, Dong-Jin
    • Transactions of the Korean hydrogen and new energy society
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    • v.23 no.4
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    • pp.412-419
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    • 2012
  • Increasing demand for natural gas and higher natural gas prices in the recent decades have led many people to pursue unconventional methods of natural gas production. POSCO-Gwangyang synthetic natural gas (SNG) project was launched in 2010. As the market price of natural gas goes up, the increase of its price gets more sensitive due to the high cost of transportation and liquefaction. This project can make the SNG economically viable. In parallel with this project, KEPCO (Korea Electric Power Corporation) joined in launching the SNG Quality Standard Bureau along with KOGAS (Korea Gas Corporation), POSCO and so on. KEPCO Research Institute is in charge of SNG fueled gas turbine combustion test. In this research, several combustion tests were conducted to find out the effect of hydrogen contents in SNG on gas turbine combustion. The hydrogen in synthetic natural gas did not affect on gas turbine combustion characteristics which are turbine inlet temperature including pattern factor and emission performance. However, flame stable region in ${\Phi}$-Air flow rate map was shifted to the lean condition due to autocatalytic effect of hydrogen.

Characteristics of a Plasma-Dump Combustor for VOC Destruction (VOC 분해 플라즈마-덤프 연소기 특성)

  • Kim, Eun Hyuk;Chun, Young Nam
    • Journal of Korean Society of Environmental Engineers
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    • v.37 no.8
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    • pp.492-497
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    • 2015
  • VOCs (Volatile Organic Compounds) are generally generated in the painting process, or at the company and laundry where use organic solvents. The VOCs consist of various hydrocarbons and has low calorific value due to its dilution with atmospheric air. Therefore, the VOCs are difficult to burn by a conventional fuel combustor. In this study, a novel plasma dump combustor was proposed for the treatment of low calorific VOC gases. This combustor was designed a combination of the characteristics in a plasma burner, a dump combustor and a 3D matrix burner. The combustor has good structure for maintaining enough residence time and reaction temperature for stable flame formation and VOC destruction. For investigating the performance characteristics of the plasma dump combustor, an experiment was achieved for VOC feed rate, VOC injector position, etc. Toluene was used as a surrogate of VOC. The novel combustor gave better performance than a conventional combustor, showing that VOC destruction rate and energy efficiency were 89.64% and 12.27 kg/kWh respectively, at feeding rate of 450 L/min of VOC of 3,000 ppm of toluene concentration.