• Title/Summary/Keyword: 수소 엔진

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티타늄 알루미나이드 합금의 산화연구

  • 이원식;이재희
    • Proceedings of the Korean Vacuum Society Conference
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    • 1999.07a
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    • pp.48-48
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    • 1999
  • 티타늄 알루미나이드 합금은 이들의 강도나 고온 특성 때문에 초음속 비행기의 구조물질이나 수소를 연료로 사용하는 비행기의 엔진물질로 각광받고 있다. 그러나 티타늄 알루미나이드 합금들은 이들이 갖는 규칙적인 미세구조로 인하여 실온에서 낮은 연성을 나타내는 단점이 있다. 실온에서 낮은 연성을 갖는 티타늄 알루미나이드 합금의 단점은 텅스텐, 물리브덴, 니오비움, 탄타륨, 바나디움 등의 베타 안정화 물질들을 첨가함으로서 어느정도 극복되고 있다. 따라서 티타늄 알루미나이드 합금이 초음속 비행기의 구조 물질이나 수소를 사용하는 엔진 물질로 사용되기 위해서는 이 물질들의 산화연구가 필수적이다. 지금까지 티타늄의 산화연구에서 알루미늄이나 니오비움의 역할에 대해서는 여러 연구자들이 연구를 한 바 있다. Chaze와 Coddet는 알루미늄이 티타늄에서 산소의 용해도를 감소시키고, Chen과 Rosa는 니오비움이 티타늄에서 산화물 형성율을 낮춘다는 것을 각각 알아냈다. 그러나 지금까지 티타늄 알루미나이드의 산화연구는 충분하지 못했다. 지금까지 티타늄 알루미나이드의 산화연구에서 밝혀진 산화운동학의 내용은 가열온도와 가열시간에 따라 크게 다른 두 개 혹은 그 이상의 산화물을 갖는다는 것이다. 본 연구의 목적은 여러 가지 티타늄 알루미나이드 합금의 산화특성을 밝히는 것이다. 이를 위하여 첫 번째 실험은 실온 공기 중에서 자연적으로 산화된 여러 가지 티타늄 알루미나이드 합금들($\alpha$2,$\beta$,${\gamma}$)을 초고진공($\leq$10-11Torr)속에 넣고, 시료의 온도를 실온에서 100$0^{\circ}C$까지 변화시키면서 AES(Auger Electron Spectroscopy)와 ISS(Ion Scattering Spectroscopy)를 사용하여 각각의 온도에서 여러 가지 시료들의 표면조성을 조사했다. 두 번째 실험은 티타늄 알루미나이드 시료를 고순도 공기(hydrocarbon$\leq$0.1^g , pp m) 중에서 각각 $600^{\circ}C$에서 100$0^{\circ}C$까지 가열하여 산화시켰다. 이 시료의 산화도는 각각의 가열온도에서 가열시간을 변하시키면서 TGA(Thermogravimetric Apparatus)로 측정했다. 실온 공기중에서 자연적으로 산화된 여러 가지 티타늄 알루미나이드 합금들을 초고진공속에 넣어 100$0^{\circ}C$까지 가열한 실험에서는 이들 시료에 포함된 알루미늄의 양에 따라서 표면 조성이 크게 다른 것을 알 수 있었다. 그리고 고순도 공기 중에서 100$0^{\circ}C$까지 가열하여 산화시킨 티타늄 알루미나이드 산화물의 산화기구는 명백한 3단계 포물선 산화의 특성을 나타냈다.

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A Study for Generating Power on Operating Parameters of Powerpack utilizng Linear Engine (리니어엔진을 이용한 파워팩의 운전조건에 따른 발전출력에 관한 연구)

  • Oh, Yong-Il;Kim, Gang-Chul;Lim, Ock-Taeck
    • Journal of Hydrogen and New Energy
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    • v.23 no.2
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    • pp.183-190
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    • 2012
  • The research shows the experiment results according to the combustion characteristics and configuration of the linear generator of powerpack for the generating power applying the 2-stroke compact linear engine. The powerpack used in this paper consists of 2-stroke linear engine, linear generator and air compressor parts. For identifying the combustion characteristics and generating power of linear engine, some parameters were varied sucha as electric load, fuel input calorie, spark timing delay and equivalence ratio. Also generating power was confirmed at each operation conditions, when the air gap length of linear generator part was changed as each 1.0 mm and 2.0 mm. During the all operations, intake air was inputted under the wide open throttle. Mass flow rate of air and fuel was changed using mass flow controller, after these were premixed by premixture device, and then premixed gas was supplied directly into each cylinder. As a result, piston frequency and combustion characteristics were different at each conditions according to parameters affecting the combustion such as fuel input calorie, resistive load, spark timing delay and equivalence ratio. Consequently, these had an effect on generating power.

Numerical Study on Auto-ignition and Combustion Emissions Using Gasoline/Ethanol Surrogates (휘발유/에탄올 혼합연료의 자연발화 및 연소배기가스 특성에 관한 수치적 연구)

  • Lee, Eui Ju
    • Fire Science and Engineering
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    • v.30 no.3
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    • pp.1-6
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    • 2016
  • More than five thousands transportation fires occurannually in Korea and the resulting destruction of property and loss of life is huge and results in traffic and environmental pollution. The recent development of automobile technology such as the hybrid concept and use of bio fuels makes fire protection even more difficult due to a lack of understanding of the new adapted system including vehicle engines. In this study, a numerical simulation was performed on a PSR (perfectly Stirred Reactor) to simulate an automobile engine and to clarify the effect of gasoline/ethanol surrogates as a fuel. The temperature, NOx and soot emissions were predicted to decrease with increasing ethanol content, but that of unburned hydrocarbons was found to increase dramatically. The result will provide not only the basic thermal characteristics for engines and their after-treatment systems, but also make it possible to assess the potential for fire events in these systems when an ethanol mixed fuel is used in gasoline vehicles.

An Experimental Study on the Possibility of Biogas Reforming using the Waste Heat of a Small-Sized Gas Engine Generator (소형 가스엔진 발전기의 배기가스 폐열을 이용한 바이오가스 개질 가능성에 관한 실험적 연구)

  • Cha, Hyo-Seok;Kim, Tae-Soo;Eom, Tae-Jun;Jung, Choong-Soo;Chun, Kwang-Min;Song, Soon-Ho
    • Journal of Hydrogen and New Energy
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    • v.23 no.3
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    • pp.236-242
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    • 2012
  • This study has been carried out the experiment for the possibility of biogas reforming using waste heat. The source of this waste heat is the exhaust gas from a small-sized gas engine generator. For recovering the waste heat, Two-stage heat exchanger is manufactured. The two-stage heat exchanger is composed of a heat exchanger for the exhaust gas and a heat exchanger for the water. This two-stage heat exchanger is used for reforming the biogas by means of on-site hydrogen production at the small-sized gas engine generator. The two-stage heat exchanger is coupled with the biogas reformer which is a kind of catalytic reformer. To confirm a heat recovery efficiency of the two-stage heat exchanger, temperature differences of inlet and outlet locations are measured. Also, the variations of syngas concentrations with various biogas flow rates are investigated. As a result using manufactured two-stage heat exchanger, the biogas can be reformed from waste heat recovery. This experiment suggests that the exhaust gas heat exchanger is available for reforming the biogas.

A Technical Review of Endothermic Fuel Use on High Speed Flight Cooling (흡열연료를 이용한 고속비행체 냉각기술 동향)

  • Kim, Joong-Yeon;Park, Sun-Hee;Chun, Byung-Hee;Kim, Sung-Hyun;Jeong, Byung-Hun;Han, Jeong-Sik
    • Journal of the Korean Society of Propulsion Engineers
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    • v.14 no.2
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    • pp.71-79
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    • 2010
  • As hypersonic flight speeds and engines efficiencies increase, heat loads on an aircraft and it's engine increase. Because the temperature of the air flow is too high to cool the aircraft structure at hypersonic flight speeds, it is essential to use the aircraft fuel as the primary coolant. Endothermic fuels are liquid hydrocarbon aircraft fuels which are able to absorb the heat loads by undergoing endothermic reactions, such as thermal and catalytic cracking. The endothermic reactions are improved by catalysts which change the extent of reaction and product distribution. At high temperature, liquid hydrocarbons would lead to coke formation that can reduce the effectiveness of heat exchanger and cause rapid degradation of the catalyst, thus endothermic capacity of endothermic fuels is limited to the temperature at which coke doesn't form. In this study, the essential cooling technologies by applying endothermic fuels and the properties of the endothermic fuels are described.

A Study on Combustion and Emission Characteristics of Diesel-DME Blended Fuels in D.I Compression-Ignition Engine (직접분사식 압축착화엔진에서 Diesel-DME 혼합연료의 연소 및 배기특성에 관한 연구)

  • Jeong, Jaehoon;Lim, Ocktaeck;Jeon, Jong Up;Lee, Sangwook;Pyo, Youngduck;Lee, Youngjae;Suh, Hocheol
    • Journal of Hydrogen and New Energy
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    • v.23 no.5
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    • pp.530-537
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    • 2012
  • This work experimentally investigates that Diesel-DME blended fuel influences combustion characteristics and emissions (NOx, CO, HC, smoke) in a single-cylinder DI diesel engine. Diesel is used as a main fuel and DME is blended for the use of its quick evaporating characteristics. Diesel and DME are blended by the method of weight ratio. Weight ratios for Diesel and DME are 95:5 and 90:10 respectively and the both ratios have been used altogether in blended fuel. The experiments are conducted in this study single cylinder engine is equipped with common rail and injection pressure is 700 bar at 1200 rpm. The amount of injected fuels is adjusted to obtain the fixed input calorie value as 972.2 J/cycle in order to compare with the fuel conditions. DME is compressed to 15 bar by using nitrogen gas thus it can be maintained the liquid phase. In this study, different system compared others paper is common rail system, also there is combustion and emission about compared DME and diesel fuel. It is expected to be utilized about blended fuel.

The Effect of HHO Gas on the Performance of Industrial Diesel Engine Using Biodiesel Blended Fuel (흡기중의 HHO 가스 첨가가 바이오 디젤 혼합연료를 사용한 산업용 디젤기관의 성능에 미치는 영향)

  • Park, Kweon-Ha;Kim, Ju-Youn;Kim, Chul-Jung;Lee, Eun-June;Son, Kwon;Park, Sung-Hoon
    • Journal of Advanced Marine Engineering and Technology
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    • v.35 no.8
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    • pp.1022-1027
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    • 2011
  • A diesel engine works in high compression ratio due to injection of diesel fuel after compression of air. Therefore the engine has a high thermal efficiency, while nitrogen oxide is produced a lot in high flame temperature regions. In order to solve the problem this study HHO gas is added into the intake air of the industrial diesel engine. The test conditions are loads of 0%, 50% and 100% and engine speeds of 700 to 1900 rpm. The results show the maximum torque and pressure is increased, fuel consumption, smoke and CO emissions are decreased and NOx emission is remained at same level.

Study of Combustion Characteristics with Compression Ratio Change in Ultra-Lean LPG Direct Injection Engine (압축비 변화에 따른 초희박 직접분사식 LPG엔진의 연소특성 연구)

  • Cho, See Hyeon;Yoon, Jun Kyu;Park, Cheol Woong;Oh, Seung Mook
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.10
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    • pp.837-844
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    • 2014
  • Automotive manufacturers have recently developed various technologies for improving fuel economy and satisfying enhanced emission regulations. The ultra-lean direct injection engine is a promising technology because it has the advantage of improving thermal efficiency through the deliberate control of ignition. A conventional LPG engine has been redesigned to an ultra-lean-burn LPG direct injection engine in order to adopt combustion system of ultra-lean-burn. This study is aimed at investigating the effect of a change in the compression ratio on the performance and emission characteristics of a lean-burn LPG engine. The fuel consumption, heat release rate, combustion pressure, and emission characteristics are estimated depending on changing the effect of compression ratio. When the compression ratio is increased, it is difficult to improve the fuel consumption owing to an unstable combustion state, but the total hydrocarbon and nitrogen oxide emissions are reduced.

Design and Cold Flow Test of a Multi-injector Engine using Hydrogen Peroxide/Kerosene (과산화수소/케로신을 이용한 다중 분사기 엔진 설계 및 수류 실험)

  • Lee, Yang-Suk;Jeon, Jun-Su;Ko, Young-Sung;Kim, Yoo;Kim, Sun-Jin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.16 no.1
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    • pp.36-44
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    • 2012
  • Multi-injector rocket engine using high-concentrated hydrogen peroxide and kerosene was designed and manufactured. Design requirements of a rocket engine were determined and main geometrical parameters of rocket engine were determined on the basis of fundament. Six coaxial swirl injectors were mounted on the multi-injector engine. Flow analysis in the hydrogen peroxide manifold was performed to minimize stagnation and recirculation zones. Finally, the optimized hydrogen peroxide manifold was manufactured and cold flow test was carried out to confirm mass flow rate per uni-element, spray pattern and atomization characteristics. The results of cold flow test showed that the mixing head design process was successful and enough to use as a essential database for the development of a full-scale engine.

Characteristics of Combustion and Emission for Synthetic Natural Gas in CNG Engine (CNG엔진에서 합성가스 연료의 연소 및 배기 특성 평가)

  • Lee, Sungwon;Lim, Gihun;Park, Cheolwoong;Choi, Young;Kim, Changgi
    • Journal of the Korean Institute of Gas
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    • v.19 no.6
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    • pp.8-14
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    • 2015
  • Synthetic natural gas(SNG), acquired from coal, is regarded as an alternative to natural gas since a rise in natural gas due to high oil price can be coped with it. In the present study, 11-liter heavy duty compressed natural gas(CNG) engine was employed in order to examine the combustion and emission characteristics of SNG. The simulated SNG, made up 90.95% of methane, 6.05% propane and 3% hydrogen was used in the experiment. Power output, thermal efficiency, combustion stability and emission characteristics were compared to those with CNG at the same engine operating conditions. Knocking phenomenon was also analyzed at 1260 rpm, full load condition. Combustion with SNG was more stable than CNG. Nitrogen oxides emissions increased while Carbon dioxides emissions decreased. Anti-knocking characteristics were improved with SNG.