• Title/Summary/Keyword: 부분 분사

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Effect of Particle Loading Ratio on Fluid Characteristics and Particle Distribution in Particle-laden Coaxial Jet (입자부상 동축 분사기에서 입자로딩비가 유동 특성과 입자분포에 미치는 영향에 대한 연구)

  • Yoon, Jungsoo;Yoon, Youngbin
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.3
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    • pp.9-19
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    • 2015
  • Experimental research on characteristics of particle-laden jet by using a coaxial injector was conducted in order to design fuel and oxidizer injectors of the supercavitation underwater vehicle. $1{\mu}m$ and $42{\mu}m$ particles was simultaneously injected to obtain particle and fluid velocity. Small particles($1{\mu}m$) and large particles represent fluid and fuel characteristics respectively. Small particles, which was processed using PIV algorithms, and one for the large particles processed using PTV algorithms. Fluid phase axial velocity increases according to particle loading ratio increases, and particles are located at the outside of the high vorticity region in a mixing layer of a coaxial injector.

Design of Venturi Dump Surface for Pre-filming Airblast Injector (예막 공기충돌형 분사기의 벤추리 덤프면 설계)

  • Shin, Dongsoo;Choi, Myunghwan;Radhakrishnan, Kanmaniraja;Koo, Jaye;Jung, Seungchai
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.4
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    • pp.44-54
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    • 2018
  • In a spray experiment using a venturi mounted on a lean premixed LPP injector, droplets appear to have non-uniform distributions. To solve this problem, the exit angle of the venturi was changed to form a dump surface on the nozzle neck. The dump surface improved the atomization performance and minimized droplet loss while forming recirculation zone in the venturi exit. In order to solve the non-uniform spray of the injector, the flow characteristics inside the venturi and SMD of the spray are compared. Finally, an optimum venturi shape is selected to minimize the spray loss and improve the spray performance.

Measurements and Calculation of Injection Mass Rate of LFG for Intake Injection in Spark Ignition Engines (불꽃점화 엔진의 흡기관 분사를 위한 매립지가스 분사량의 측정 및 계산)

  • Kim, Kyoungsu;Choi, Kyungho;Jeon, Wonil;Kim, Bada;Lee, Daeyup
    • Journal of the Korean Institute of Gas
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    • v.25 no.4
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    • pp.36-42
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    • 2021
  • When the landfill gas generated at the landfill site is released into the atmosphere, methane gas with a high global warming potential is emitted, which adversely affects climate change. When methane contained in landfill gas is used as fuel for internal combustion engines and burned to generate electricity, it is emitted into the atmosphere in the form of carbon dioxide, which can contribute to lowering the global warming potential. Therefore, in order to use the landfill gas as fuel for power generation using an internal combustion engine, it is important to increase the thermal efficiency of the engine. Thus, it is necessary to use a fuel supply system in which gas is injected using an electronically controlled injector at an intake port for each cylinder rather than a fuel supply technology using the conventional mixer technology. In order to use the electronically controlled gas injection method, it is important to accurately measure the mass flow rate according to the conditions of using landfill gas. For this, a study was conducted to measure the injection amount and calculate them in order for the intake port gas injection of landfill gas.

PILC Characterization Study for SCR catalyst (SCR 촉매용 PILC 특성 연구)

  • 성희제;이성영
    • Proceedings of the Korea Air Pollution Research Association Conference
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    • 2003.05b
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    • pp.99-99
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    • 2003
  • 육상에서 발생하는 공해 물질뿐만 아니라 해상에서 발생하는 공해 물질에 대한 관심이 높아진 가운데 선박에서 발생하는 탄화수소, 질소산화물, 일산화탄소, 이산화황 및 입자상 물질의 규제에 관한 방안이 가시화되고 있는 현실이다. 선박엔진에서 발생하는 질소산화물 제거 연구를 위해서 당사에서는 엔진 연료 분사 시스템에 관한 연구와 더불어 후처리 설비인 SCR 연구를 병행하고 있다. 본 연구는 당사 개발 촉매인 PILC(Pillared Interlayer Clay)를 이용한 SCR 적용에 관한 연구 결과중 촉매 특성에 관한 부분이다. (중략)

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3단형 과학로켓(KSR-III)엔진 기본설계 및 성능검증 계획

  • 채연석;이수용;류철성;설우석
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1999.10a
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    • pp.5-5
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    • 1999
  • 3단형 과학로켓(KSR-III)의 기본형 및 응용형에 공통으로 사용되는 주엔진은 액체산소를 산화제로, 케로신을 연료로 사용하는 액체추진기관이다. 엔진 기본설계를 통하여 로켓 임무 요구사항에 부합되도록 엔진 각 부분의 기본제원을 설정하였고, 엔진의 형상을 결정하였다. 설계된 엔진의 성능검증 작업은 분사시험용 엔진, 축소형 엔진, 엔지니어링 모델 및 비행시험모델의 설계/제작/시험을 통하여 순차적으로 수행할 계획이다. 본 연구는 3단형 과학로켓 엔진의 기본설계 및 성능검증 계획에 관한 것이다.

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VMT Corporation

  • 박성렬
    • Proceedings of the Korean Vacuum Society Conference
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    • 2000.02a
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    • pp.43-43
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    • 2000
  • 당사는 (주)포스콘 진공 사업 부분이 분사하여 1999년 1월 진공 장비 및 제어계측 분야 독립 법인체를 설립하였으며 당사의 주력 제품은 초고진공용 Ion pump 및 controller로서 국산화 개발하여 생산 판매하고 있다. Ion pump 와 controller는 10-4 ~ 10-10 Torr 범위의 초고진공으로 진공 시스템을 배기할 수 있는 장비로서 무소음, 무진동, 저전력의 특성을 가진 초정밀, 초청정 진공 실험에 없어서는 안 될 펌프이다. 현재 당사는 과학기술부의 특정연구개발 과제를 극고진공(XHV)용 Ion Pump를 개발하고 있는 중이다.

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STUDY ON HEAT RELEASE RATE BY COMBUSTION IN DIESEL ENGINE (Diesel기관의 연소에 의한 열발생율의 연구)

  • AHN Soo Gil
    • Korean Journal of Fisheries and Aquatic Sciences
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    • v.8 no.3
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    • pp.150-156
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    • 1975
  • This paper dealt itself with the relation of the heat release rate with crank angle in combustion process by adjusting the injection time, injection amount and engine speed of diesel engine. The result of test were obtained by analyzing indicator diagram of KUBOTA 2LKE diesel engine, where the indicator was used Tertronix oscilloscope. The combustion period of diesel engine is composed of premixed burning time and combustion controlled time. The larger the premixed burning region, the higher efficiency was obtained with the higher maximum pressure than at the time of the normal smooth operation. The longer the combustion controlled time, the lower the maximum pressure than the period of the normal operation, but the efficiency was decreased. The region of premixed burning was principally controlled by injection delay, but combustion controlled time was affected when oxygen and fuel were mixed. Efficiency of engine was increased at the time of earlier injection time under the constant injection amount, and engine speed, but the pressure increasing was observed higher than the efficiency increasing.

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Influence of airborne-particle abrasion on flexural strength of fiber-reinforced composite post (미세입자 분사마모 표면처리가 Fiber-Reinforced Composite 포스트의 굴곡 강도에 미치는 영향)

  • Sim, Eun-Ju;Kim, Jin-Woo;Cho, Kyung-Mo;Park, Se-Hee
    • Journal of Dental Rehabilitation and Applied Science
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    • v.32 no.1
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    • pp.24-31
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    • 2016
  • Purpose: Many studies have shown that airborne-particle abrasion of fiber post can improve the bonding strength to resin cement. But, airborne-particle abrasion may influence the property of fiber post. The purpose of this study is to evaluate the influence of airborne-particle abrasion on flexural strength of fiber post. Materials and Methods: Two fiber-reinforced posts; DT Light Post Size 2 (1.8 mm diameter, Bisco Inc) and RelyX Fiber Post Size 3 (1.9 mm diameter, 3M ESPE); were used in this study. Each group was divided into 3 subgroups according to different surface treatments; without pretreatment: $50{\mu}m$ aluminum oxide (Cobra$^{(R)}$, Renfert): and $30{\mu}m$ aluminum oxide modified with silica (Rocatec Soft$^{(R)}$, 3M ESPE). After airborne-particle abrasion procedure, three-point bending test was done to determine the flexural strength and flexural modulus. The diameter of each posts was measured to an accuracy of 0.01 mm using a digital micrometer. There was no diameter change before and after airborneparticle abrasion. The mean flexural moduli and flexural strengths calculated using the appropriate equations. The results were statistically analyzed using One-way ANOVA and Scheffe's post-hoc test at 95% confidencial level. Results: There was no significant difference on flexural strength between groups. Conclusion: In the limitation of this study, flexural strength and flexural modulus of fiber post are not affected by airborne-particle abrasion.

Combustion Characteristics and On-site Performance Test of a Double-cone Partial Premixed Nozzle with Various Fuel hole Patterns (이중 콘형 부분예혼합 GT 연료노즐의 연소특성 및 발전플랜트 실증)

  • Kim, Han Seok;Cho, Ju Hyeong;Kim, Min Kuk;Hwang, Jeongjae;Lee, Won June;Min, Kyungwook;Kang, Do Won
    • Journal of the Korean Institute of Gas
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    • v.25 no.6
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    • pp.22-28
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    • 2021
  • Combustion characteristics were examined experimentally for a swirl-stabilized double cone premixed burner nozzle used for industrial gas turbines for power generation. An original model and a variant with a different fuel injection pattern are tested to compare their combustion characteristics such as NOx, CO and stability in pressurized conditions with single burner-flame and in an ambient multi-flame conditions with multi-burners. Test results show that NOx emissions are smaller for the variant, whose number of fuel holes is reduced with the same total area of fuel holes, in ambient and pressurized single-flame conditions with single burner, which results from enhanced fuel/air mixing due to a higher penetration of fuel into the air stream. The multi-burnerflame test results show that NOx emissions are smaller for the variant due to reduced flame interactions, which, on the contrary, slightly reduces the stability margin. On-site test results fromin an actual power plants also show that NOx emissions are reduced for the variant, compared with the original one, which is in agreement with the lab test results stated above.

The Effects of Partially Premixed Pilot Injection Timing on the Combustion and Emission Characteristics in a Common Rail Diesel Engine (커먼레일식 디젤기관의 부분 예혼합 분사시기가 연소 및 배기특성에 미치는 영향)

  • Yoon, Sam-Ki;Choi, Nag-Jung
    • Journal of Power System Engineering
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    • v.17 no.6
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    • pp.18-24
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    • 2013
  • An experimental study was performed to investigate the characteristics of combustion pressure and exhaust emissions when the pilot injection timing and EGR rate were changed in a CRDI 4-cylinder diesel engine. The pilot injection timing and EGR rate have a significant impact on the combustion and emission characteristics of diesel engine. In this study, the pilot injection timing and EGR rate variation were conducted to 2000rpm of engine speed with torque 50Nm. Combustion pressure and heat release rate were decreased under high EGR rate conditions but increased under the pilot injection timing $20^{\circ}$(BTDC). IMEP and the maximum pressure in cylinder(Pmax) were decreased under the same injection timing with the increase of EGR rate. The NOx emission was decreased with increasing the EGR rate. On the other hand, in the same injection timing conditions, CO, HC, $CO_2$ emissions were increased with increasing the EGR rate.