• Title/Summary/Keyword: 혼합연료

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Effect Study of Fuel Specifications on Biofuels Policy in Transport Sector (수송용 바이오연료 정책에 따른 품질기준 영향에 관한 연구)

  • Park, Jo-Yong;Kim, Jae-Kon;Min, Kyong-IL;Park, Cheon-kyu;Ha, Jong-Han
    • Journal of the Korean Applied Science and Technology
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    • v.32 no.4
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    • pp.767-780
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    • 2015
  • Transport biofuels produced from biomass can be substituted for petroleum fuels due to GHG reduction, sustainability and environmental friendly. Mandates and targets of biofuels are announced in the European union, United states and other countries worldwide and promoted by the government policies. This paper reviewed current status of the national biofuels policies and fuel specifications in transport sector. EU biofuels policy shifted and GHG emission reduction became the main focus of the policy. There are specification requirements for biofuels in the U.S. under the RFS2, but there are other polices as well that serve to promote the uptake of biofuels both at the federal and state level. Korea government has allowed 2.3% oxygen in gasoline to come from oxygenates, increased the biodiesel blend mandate from B2 to B2.5 effective from Jul. 31, 2015.

Mixing Performance of Unlike Doublet Impinging Liquid Jets (이중 충돌제트의 혼합 성능 연구)

  • Jo, Yong Ho;Lee, Seong Ung;Yun, Ung Seop
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.4
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    • pp.82-91
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    • 2003
  • Experiments to investigate the mixing performance of unlike doublet impinging jets are conducted. Reynolds number of simulants used in this study rages from 1.0 to 1.5 Cold flow test is performed to investigate the hydrodynamic effect and spray of the impinging jets are collected locally and calculated by using Rupe's mixing efficiency equation. Momentum exchanges and relative velocity ratio between two jets are taken as the main parameter to represent the effect of enlargement of the orifice diameter. As diameter ratio increases, the corresponding momentum ratio where maximum mixing efficiency occurs and relative velocity at the maximum mixing efficiency ranges 0.6 to 0.7, respectively. Penetration depth can be taken as a prominent parameter to estimate the mixing efficiency.

Mixing and Penetration Studies of Transverse Jet into a Supersonic Crossflow (초음속 유동 내 공동을 이용한 수직 분사 혼합 및 연료 침투거리에 관한 연구)

  • Kim, Chae-Hyoung;Jeong, Eun-Ju;Jeung, In-Seuck;Kang, Sang-Hun;Yang, Soo-Seok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.2
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    • pp.24-32
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    • 2008
  • A non-reacting experimental study on a normal injection into a Mach 1.92 crossflow which flows over various geometries(flat plate, small cavity, large cavity) was carried out to investigate the effect of the momentum flux ratio(J). The aft ramp of the cavity advances the increase of the penetration height and the strong two-dimensional shock from recompression region mainly affects the shock structure and mixing layer at the downstream flow. As flow runs downward, the transverse penetration height increases with increasing J(J = 0.9, 1.7, 3.4). However, above some critical ratio, jet penetration height growth with increasing J is not appeared in flow-field. Large scale cavity has a good mixing efficiency but it increases the drag loss in the combustor.

Experimental Study on Fuel/Air Mixing using the Cavity in the Supersonic Flow (초음속 유동장 내의 공동을 이용한 연료/공기 혼합에 관한 실험적 연구)

  • Kim Chae-Hyoung;Jeong Eun-Ju;Jeung In-Seuck
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2005.11a
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    • pp.64-71
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    • 2005
  • To achieve efficient supersonic combustion within a manageable length, a successful fuel injection scheme must provide rapid mixing between fuel and airstream. In former days, various injection concepts have been investigated. Cavity flow is the open type, that is, length-to-depth ratio L/D=4.8, aft ramp angle is $22.5^{\circ}$. An experimental study on a transverse cross jet injection into a Mach 1.92 supersonic main stream which flows over a cavity was carried out to investigate the effect of the momentum flux ratio(J), the jet interaction characteristics, and the pressure distribution in the combustor and using the primary diagnostics : schlieren visualization and wall static pressure measurements. Fuel penetration height and jet interaction characteristics depend strongly on the momentum flux ratio.

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Vaned Wheel Atomization of CWM (Vaned Wheel Atomizer에 의한 CWM 미립화)

  • 김성준;김용선
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.16 no.5
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    • pp.974-982
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    • 1992
  • The atomizations of CWM slurry and water are done by a wheel atomizer which is designed and manufactured for this experiment. The variables of the experiment are the angle of vane, aspect ratio, particle loading and the mean size of coal particle distribution. The main purposes of the experiment are to know how the angle of vane and aspect ratio of vane influence the size distribution of CWM droplets. The experimental results say there are no appreciable effects on the mean size of CWM droplets from the change of loading of coal prticles in slurry. The mean size of coal particle in slurry, however, influence quite strongly the mean size of CWM droplets. The mean size of CWM droplets is quite strongly affected by the angle of vane. The size distribution of CWM droplets is controllable by the change of aspect ratio.

The application of twin-fluid atomizer to single point injection system (일점연료분사시스템의 연료분사밸브로서 2유체 분사밸브의 이용)

  • 전홍신
    • Journal of the korean Society of Automotive Engineers
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    • v.10 no.5
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    • pp.24-32
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    • 1988
  • 본 고에서는 일점연료분사시스템의 문제점을 해결하는 방안 및 장래 유망하다고 보여지는 희박혼합기상태에서 연소상태의 개선을 목적으로, 연료분사밸브로서 미립화특성이 좋은 2유체 분사밸브를 사용하기 위하여 기술하고자 한다.

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Characteristics of Dual Transverse Injection in Supersonic Flow Fields I-Mixing Characteristics (초음속 유동장 내 이중 수직분사의 특성에 관한 연구 I-혼합특성)

  • Shin, Hun-Bum;Lee, Sang-Hyeon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.6
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    • pp.53-60
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    • 2002
  • Based on the analyses of the single transverse injection in supersonic flow fields, the mixing characteristics of dual transverse injection of hydrogen in supersonic air flow are studied with computational methods. Three-dimensional Navier -Stokes and the k-$\omega$ SST turbulence model were used. A parametric study is conducted with the variation of the distance between two injectors. The flow patterns and the mixing characteristics of two injection flows are very different from each other, and the flow patterns and the mixing characteristics of the rear injection flow are strongly influenced by those of the first injection flow. The increase of the distance between two injectors up to a specific distance results in the increase of mixing rate and penetration of fuel. However, the increase of the distance over the specific distance results in the decrease of mixing rate and penetration of fuel. From the results it can be stated that there exists a distance between two injectors for optimum mixing characteristics.

Combustion Characteristics of Premixed Charge Compression Ignition Diesel Engine using Mixed Fuels (혼합연료를 이용한 예혼합 압축착화 디젤엔진의 연소특성)

  • 조병호;이기형;이창식
    • Transactions of the Korean Society of Automotive Engineers
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    • v.10 no.5
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    • pp.58-64
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    • 2002
  • A diesel engine has various merits such as high thermal-efficiency, superior fuel consumption and durability. Therefore the number of diesel engine in the world is increasing. As the seriousness of environmental pollution increases in the world, the method to reduce the noxious materials of CO2, NOx and P.M. is very important subject to correspond to exhaust gas regulations. A new concept, so called premixed charge compression ignition(PCCI), is focused among the various corresponding manners. In this study, we investigated the combustion characteristics of PCCI engine using a mixed fuels with that of commercial diesel engine. Finally we grasped a emission characteristics of PCCI engine. From this experiment, it could be found that NOx reduction is caused by the lower maximum temperature and soot reduction is caused by rapid combustion under diffusion combustion part. Also, it was found that 1st-combustion(cool flame) and 2nd-combustion(hot flame) is appeared in heat release curve, exhaust gas temperature is diminished and combustion variation is increased according to increasing of gasoline ratio.

A Study on the Variation of Physical & chemical Properties with Refining treatment and Additive mixture for Marine Fuel Oil (선박연료유의 정제처리 및 첨가제 혼합에 따른 물리.화학적 특성 변화에 관한 연구)

  • Han, Won-Hui;Nam, Jeong-Gil;Lee, Don-Chool;Park, Jeong-Dae;Kang, Dae-Sun
    • Proceedings of KOSOMES biannual meeting
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    • 2006.11a
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    • pp.291-297
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    • 2006
  • Recently it is a tendency that the use of the heavy fuel oil is investigated even from the middle&small class vessel in order to reduce the operating cost of vessel caused by with rise of international gas price. In this study, analyzed the physical & chemical properties and examined the effect of refining treatment and a fuel oil additive for MF30 fuel oil which is a mixture fuel oil mixed M.G.O and the heavy oil MF380 use to be possible in the middle&small class vessel. As a results, the effects of two of pre-refinery treatment methods as centrifugal purifier and heating & homogenizing system(M.C.H) are some feeble, but the pour point and the flash point came to be low more or less. The effect of property improvement which is caused by with the fuel oil additive did not appear positively.

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