• Title/Summary/Keyword: Micro combustion

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Design Criterion for the Size of Micro-scale Pt-catalytic Combustor in Respect of Heat Release Rate (열 방출률에 대한 마이크로 백금 촉매 연소기의 치수 설계 기준)

  • Lee, Gwang Goo;Suzuki, Yuji
    • Journal of the Korean Society of Combustion
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    • v.19 no.4
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    • pp.49-55
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    • 2014
  • Design criterion for the size of micro Pt-catalytic combustor is investigated in terms of heat release rate. One-dimensional plug flow model is applied to determine the surface reaction constants using the experimental data at stoichiometric butane-air mixture. With these reaction constants, the mass fraction of butane and heat release rate predicted by the plug flow model are in good agreement with the experimental data at the combustor exit. The relationship between the size of micro catalytic combustor and mixture flowrate is introduced in the form of product of two terms-the effect of fuel conversion efficiency, and the effect of chemical reaction rate and mass transfer rate.

Evaluation of Combustion Mechanism of Droplet Cluster in Premixed Spray Flame by Simultaneous Time-Series Measurement (동시 시계열 계측에 의한 예혼합 분무화염 내 유적군 연소기구의 평가)

  • Hwang, Seung-Min
    • Journal of Korean Society of Environmental Engineers
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    • v.31 no.6
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    • pp.442-448
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    • 2009
  • To evaluate the combustion mechanism of each droplet cluster downstream of the premixed spray flame, the simultaneous time-series measurements were conducted by using optical measurement system consisting of laser tomography, multi-color integrated Cassegrain receiving optics (MICRO) and phase Doppler anemometer (PDA). Furthermore, the group combustion number of droplet cluster was estimated experimentally, and the combustion mechanism of droplet cluster was examined applying the theoretical analysis. The group combustion number, $G_c$, was experimentally estimated about all droplet cluster verified by planar images, and it was classified into the internal group combustion mode and the external group combustion mode according to the theoretical analysis. It is found that there are cases in which the group combustion number estimated experimentally for droplet cluster agree or disagree with the classification by theoretical analysis. The reason of disagreement is considered due to that the group combustion number was only estimated by the geometrical arrangement of droplets in cluster, and that the actual phenomenon is three-dimensional but the measurement system is two-dimensional.

Flame Stabilization and Structures in Narrow Combustion Space (좁은 연소공간에서의 화염 안정화와 화염구조)

  • Kim, Nam Il
    • 한국연소학회:학술대회논문집
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    • 2012.11a
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    • pp.159-162
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    • 2012
  • Combustion in a narrow space has been interested as a model of meso-scale combustors (or micro-combustors). Premixed flames have been used to overcome flame quenching in a narrow space and non-premixed flames have been used to improve flame stabilization. In this study, overall characteristics of premixed flame and non-premixed flame in narrow combustion spaces were reviewed. Various effects such as the flow velocity distribution, thermal interaction, enhanced mass diffusion were discussed and an eventual structure of the flame at the extinction limit was introduced.

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Facile Synthesis of Hydroxyapatite by Hydrothermal and Solvent Combustion Methods

  • Bramhe, Sachin N;Lee, Hyun Chul;Chu, Min Cheol;Ryu, Jae-Kyung;Balakrishnan, Avinash;Kim, Taik Nam
    • Korean Journal of Materials Research
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    • v.25 no.9
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    • pp.492-496
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    • 2015
  • Hydroxyapatite (HA), which is an important calcium phosphate mineral, has been applied in orthopedics, dentistry, and many other fields depending upon its morphology. HA can be synthesized with different morphologies through controlling the synthesis method and several parameters. Here, we synthesize various morphologies of HA using two simple methods: hydrothermal combustion and solution combustion. The phase purity of the synthesized HA is confirmed using X-ray diffractometry. It demonstrates that pure phased hydroxyapatite can be synthesized using both methods. The morphology of the synthesized powder is examined using scanning electron microscopy. The effects of pH and temperature on the final powder are also investigated. At $140^{\circ}C$, using the hydrothermal method, nano-micro HA rods with a hexagonal crystal structure can be synthesized, whereas using solution combustion method at $600^{\circ}C$, a dense cubic morphology can be synthesized, which exhibits monoclinic crystal structures.

An Investigation on Combustion Characteristics of Hydrogen-Air Premixture in a Sub-millimeter Scale Catalytic Combustor using Infrared Thermography (적외선 열화성 온도 측정법을 이용하여 살펴본 서브밀리미터 스케일 촉매 연소기에서의 수소-공기 예혼합 가스의 촉매 연소 특성)

  • Choi, Won-Young;Kwon, Se-Jin
    • Journal of the Korean Society of Combustion
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    • v.10 no.3
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    • pp.17-24
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    • 2005
  • A sub-millimeter scale catalytic combustor with a simple plate-shaped combustion chamber was fabricated. A porous ceramics support coated with platinum catalyst was placed in the chamber. The combustor has a gallium arsenide window on the top that is transparent to infrared ray. The temperature distribution in the combustion chamber was measured using infrared thermal imager while hydrogen-air premixture is steadily supplied to the combustor. The area where the catalytic reaction took place broaden for higher flow rate and lower equivalence ratio made activated area in the combustion chamber broaden. The amount of coated platinum catalyst did not affect the reaction. Stop of reaction, which is similar to flame quenching of conventional combustion, was investigated. Large content of heat generation and broad activated area are essential criteria to prevent stop of reaction that has a bad effect on the combustor performance.

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Development of Low NOx Combustor for 55kw Class Micro Gasturbine (55kW급 마이크로터빈용 저공해 연소기 개발)

  • Kim Hyung-Mo;Park Young-Il;Park Poo-Min;Yang Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.318-321
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    • 2005
  • The design and performance test of a low NOx gas turbine combustor to be used in 55kW class micro-gasturbine engine was performed in KARI's combustion test facility. The combustor is reverse flow-can type for easy installation of injector and other parts and LNG is used as fuel. The performance targets are $99.5\%$ combustion efficiency, less 10ppm NOx, $30\%$ patten factor and $4\%$ pressure loss. Most of the performances required are satisfied.

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Combustion Characteristics of Wood Materials (1) (Mass Reduction and Ignition Delay) (목재의 연소특성(1) (질량감소와 착화지연))

  • Kim, Chun-Jung
    • Journal of the Korean Society of Combustion
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    • v.4 no.2
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    • pp.11-22
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    • 1999
  • Combustion characteristics of the wood chips(balsa chips) were experimentally investigated with respect to the thermal recycle system of the urban waste. The urban waste contains plastics, vegetable and wood materials. Wood was chosen as an example of the one of the component of urban dust. A small wood chip was burned in a electric furnace by the micro-electric balance. The mass reduction rate was normalized by the initial mass of test piece and the time of volatile combustion end. When the mass of the wood chips(balsa chips) was larger than 0.5g, the combustion similarity was found on the normalized mass reduction rate.

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Combustion Characteristics of Wood Chips(Flame Shape of Combustion and Ignition Delay) (목재의 연소 특성(2)(연소형태와 연소특성))

  • Kim, Chun-Jumg;ARAI, Masataka;Kang, Kyung-Koo
    • Journal of the Korean Society of Industry Convergence
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    • v.2 no.2
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    • pp.139-146
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    • 1999
  • Combustion Characteristics of the wood chips(balsa chips) were experimental studied as fundamental investigation of the thermal recycle system of the urban dust. The urban dust contains plastics vegetable and lot of wood material. Then, a wood was chosen as an example of the component of urban dust. A small wood chip was burned in a electric furnace and mass reduction rate during volatile and combustion states were recorded by the micro-electric balance and the combustion flame shape took a photograph by video camera at the mass of wood chips and ambient temperature in the furance. Ignition delay took the minimum value when the mass of the test chip was 0.3g. When a mass of the test chip was smaller then 0.001g, combustion with flame did not burnt.

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Experiment on the Limit Scale of Combustion in Constant Volume Micro Combustor (초소형 정적 연소기에서의 연소 한계에 대한 실험적 연구)

  • 나한비;권세진;김세훈;이대훈
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.4
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    • pp.27-32
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    • 2003
  • The Performance of micro combustor in various condition was exploited experimentally. Various geometric conditions of combustor were considered to figure out the performance of micro combustor. The micro combustor studied in this study was constant volume with cylindrical shape. Geometric parameters of combustor were defined to be combustor height and diameter. The effect of height was exploited parametrically with the size of 1mm, 2mm and 3mm. The effect of diameter was observed parameterized with 7.5mm and 15mm. Three different combustibles or Stoichiometric mixture of methane/air, hydrogen/air were used. Pressure transition during combustion process was recorded. The maximum pressure by combustion responded favorably with the change of height of combustor and the initial pressure. The flame propagation was visulized using Schlieren method. The flame propagation within combustor was observed when specific conditions such as combustor height and initial pressure over critical value was satisfied.

Design Methodology of an Annular Combustor for Micro Gas Turbines (마이크로가스터빈용 환형연소기 설계 기법)

  • Cho, Ju Hyeong
    • Journal of the Korean Society of Combustion
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    • v.19 no.4
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    • pp.21-27
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    • 2014
  • MGT (micro gas turbines) have been gaining particular attentions with a variety of commercial and military applications due to their advantages such as compact size, simple operability, easy maintenance, and low emissions. This study deals with development processes of an annular combustor applied to MGT. Preliminary design methodologies are used to size the main components of the combustor. Key design features such as liner temperatures and pressure losses are evaluated. Results show that the estimated liner temperatures are within acceptable range. Dominant factors for pressure losses are estimated to be air admission holes and burner swirlers.