• Title/Summary/Keyword: Metal Powder Combustor

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Conceptual Design of the Slag Removal Method in the Metal Powder Combustor and Condition Tests for the Water Film Formation (금속분말 연소기의 slag 제거기법 개념 설계 및 Water Film 형성 조건 기초실험)

  • Kim, Kwang-Yeon;Shmelev, V.;Ko, Hyun;Lee, Sung-Woong;Cho, Yong-Ho
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.554-557
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    • 2011
  • One of the issues that occurs in development of a combustor using Metal Powder as a fuel is an alumina slag processing. A water film formed inside the combustor is expected to be able to solve this issue. The experiments about the formation of a water film were carried out as a preliminary study. As the tangential velocity of water jet is increasing, the angle derivation from horizontal is decreasing for the test model. Results of the experiments showed that the thin water film on the inner surface appeared at the velocity of 10~15 m/s.

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Feeding Rate Measurement of Pintle Injector Type Fuel Feeder for Metal Powder Combustor (금속분말 연소기를 위한 핀틀인젝터형 연료 공급 장치의 입자 분사량 측정)

  • Ko, Tae-Ho;Kim, Hyung-Min;Lee, Do-Hyung;Yoon, Woong-Sup
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.405-409
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    • 2010
  • 금속분말을 청정 에너지원으로 이용하기 위해 금속분말 소형 연소기의 구현이 필요하다. 이를 위한 선행연구로 연료 공급 시스템인 핀틀인젝터형(pintle injector type) 금속분말 공급장치의 중요 성능인 분사량을 실험적으로 측정하였다. 분사량 측정 시험에 앞서 간단한 금속분말 공급 시험으로 확인된 문제점을 장치의 변경을 통해 해결하였다. 측정 시험의 결과, 연료 공급 장치에 이송 가스 압력이 상승함에 따라 많은 질유량의 금속분말이 분사되었고 압력에 따른 정량적 분사량을 확인하였다. 이송 가스와 금속분말의 혼합 성능을 개선하여 균일한 분사를 하고자 이송 가스를 25 Hz로 가진 하여 공급하였고 가진이 없는 경우의 실험결과와 비교하였다.

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Flame Standing of Magnesium-Steam in Swirl Combustor (와류 연소기에 의한 Mg-Steam 화염 안정화)

  • Ko, Tae-Ho;Lee, Sang-Hyup;Yoon, Woong-Sup
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.139-143
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    • 2011
  • 금속분말을 청정 에너지원으로 이용하기 위해 금속분말 소형 연소기의 구현이 필요하다. 이를 위한 기초 연구로서 점화성이 뛰어나면서도 경제적인 수십 마이크로 크기의 마그네슘(Mg) 분말을 대상으로 고온 증기(steam)와의 연소 현상 대해 연구하였다. 본 연구에서는 연소실 내 체류시간 및 혼합 효율을 증가시키기 위해 와류 유동을 연소기에 적용하였고 아르곤(Ar) 이송가스를 이용해 마그네슘 분말을 공급하였다. 안정한 화염을 유지시키기 위하여 이송가스의 유량을 변화시켜 공급되는 마그네슘의 양을 조절하였고, 고온 증기의 공급량은 니들 밸브의 개도를 조정하거나 우회시킨 관로로 증기의 일부를 배출함으로써 조절하였다. 고온의 점화원을 사용하여 증기 분위기 내 마그네슘 분말을 점화시켜, 대기압 환경에서 마그네슘/증기/아르곤의 지속적인 화염을 구현하였다.

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Ignition Characteristics of Aluminum Metal Powder Fuel with Thermal Plasma (플라즈마를 이용한 분말형 금속 연료 알루미늄의 점화 특성)

  • Lee, Sang-Hyup;Lim, Ji-Hwan;Yoon, Woong-Sup
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.737-744
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    • 2011
  • The success of continuous aluminum powder combustion with steam plasma is different from hydrocarbon ignition source. Ignition characteristics of aluminum powder with high temperature thermal plasma is studied with oxidizer-free environment. Experiment with argon plasma has same temperature conditions at 4500 K and particle feeding condition for previous combustion test with steam plasma and swirl combustor. The temperature of the plasma was measured using Optical Emission Spectroscopy method. Ignition characteristics were analyzed by SEM image and EDS. Aluminum powder with plasma has rapid evaporation mechanism contrast to hydrocarbon ignition source. It enhances to aluminum powder effective ignition characteristics.

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Numerical Simulation on Particle Dispersion in Axisymmetric Sudden-Expansion by Tracer Method (입자추적법에 의한 축대칭 급확대부의 입자확산현상 수치해석)

  • Park, Ounyoung;Yang, Hee Sung;Yim, Chung Sik
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.766-774
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    • 2017
  • Software has been developed for simulating particle dispersion in a circular pipe with sudden-expansion, which models the fuel feeding system of a combustor that uses metal powder like aluminum as fuel. The Lagrangian based discrete tracer point method was employed for a plug flow of particles that satisfies local turbulent velocity fluctuations. A radial velocity component was created to improve the flow turning outwards in the recirculation zone. The particle distribution patterns from both with and without the component were directly compared with the experiments near the reattachment.

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A Study of Alkali Metal Vapor Adsorption Behavior by Using Pressurized Reactor (가압반응기를 이용한 알칼리금속증기 흡착특성에 관한 연구)

  • 전수한;최병철;김형택
    • Journal of Energy Engineering
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    • v.11 no.2
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    • pp.114-121
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    • 2002
  • Alkali metal compounds existed in original coal or sorbents are exhausted as vapor or small particle at the outlet of combustor when operating PFBC power plant. These compounds can be removed with dust removal equipment, but total generation efficiency will be decreased because of lower operating temperature of dust removal equipment. Alkali metal contained in vapor phase is initially deposited onto turbine blade results in serious corrosion. The concentration of alkali vapor in the PFBC flue gas is 20∼40 ppm which is dependent on mineral characteristics and composition as well as operating condition of PFBC. However, the allowance limit of alkali metal vapor is assigned as less than 50 ppb for gas turbine when coal or oil is used as fuel. Therefore, alkali metal vapor in PFBC or IGCC process should be removed by solid sorbents to prevent corrosion of turbine blade and improve plant efficiency. In the present investigation, powder of Bauxite, Kaolinite and Limestone is used in the preparation of cylinder-type pellet which is inserted into the pressurized alkali removal reactor for the alkali absorption experiment. Experimental results showed that the alkali removal efficiency in the order of Bauxite, Kaolinite and Limestone. Alkali vapor removal efficiency is related with reaction temperature, porosity of pellet and alkali vapor concentration of flue gas.

Study on Anti-oxidization Coating for Staged Combustion Cycle Rocket Engine (다단연소 사이클 엔진 적용을 위한 내산화 코팅에 관한 연구)

  • Kim, Young-June;Byon, Eung-Sun;Rhee, Byong-ho;Han, Yeoung-Min;Noh, Yong-Oh;Bae, Byung-Hyun;Hyun, Seong-Yoon;Cho, Hwang-Rae;Bang, Jeong-Suk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.864-870
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    • 2017
  • The propellants are burned in the pre-burner of the staged combustion cycle engine, and the resulting hot gas drives the turbine, and the turbine operates the turbo pump. The burned gas passing through the turbo pump is supplied to the combustor at high temperature and high pressure, where the gas is supplied in an excess of fuel or an excess of oxidant depending on the amount of fuel or oxidant. When the cycle works at oxidizer-rich staged combustion, its metal pipe can ignite or explode by the impact of even small particles. In this study, we develop the powder combinations for anti-oxidation coating through the analysis of other coating materials and establish the coating process.

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A Study on Anti-oxidization Coating for Staged Combustion Cycle Rocket Engines (다단연소 사이클 엔진 적용을 위한 내산화 코팅에 관한 연구)

  • Kim, Young-June;Rhee, Byong-ho;Noh, Yong-Oh;Bae, Byung-Hyun;Hyun, Seong-Yoon;Cho, Hwang-Rae;Bang, Jeong-Suk;Byon, Eung-Sun;Han, Yeoung-Min
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.125-131
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    • 2018
  • Some propellants in a liquid rocket engine are burned in the pre-burner of a staged combustion cycle engine, resulting hot gas drives the turbine. The burned gas passing through the turbine is supplied to the combustor at high temperature and pressure. The form of the gas can be fuel rich or oxidizer rich dependent upon the mixture ratio or the engine scheme. When the cycle works at oxidizer-rich condition, the metal pipes composing the engine can be ignited or even exploded by an impact of very a small particle. In this study, we developed the powder combination and processes for an anti-oxidation coating through the analysis of various coating materials.