• Title/Summary/Keyword: 예비분사

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Effects of pilot injection timing on the Combustion and Emission Characteristics in a Common Rail Diesel Engine with Bio-diesel blended fuel (바이오디젤 혼합 연료에 커먼레일 디젤기관에서 예비 분사시기가 연소 및 배기 특성에 미치는 영향)

  • Yoon, Sam-Ki;Choi, Nag-Jung
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.15 no.5
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    • pp.2573-2578
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    • 2014
  • 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 using bio-diesel blended fuel. 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 fuel of bio-diesel blended rate 20%. In these experimental results, IMEP was shown maximum pressure at pilot injection timing BTDC$10^{\circ}$ combustion pressure and heat release rate were decreased in proportion to increase of EGR rate under the same pilot injection timing conditions. The NOx emission was decreased with increasing the EGR rate without influence on pilot injection timing. However, soot emission was reduced to a minimum at pilot injection timing BTDC$20^{\circ}$.

The LAE Burn Strategy Planning for Geostationary Satellite (정지궤도 위성의 LAE Burn Strategy Planning)

  • Kim, Bang-Yeop;Lee, Ho-Hyoung
    • Aerospace Engineering and Technology
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    • v.6 no.2
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    • pp.96-103
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    • 2007
  • A program for LAE (liquid Apogee Engine) firing strategy calculation was developed. This program can be used as the first stage of transfer orbit analysis, which process receives input parameters as like initial orbit elements, ground TT&C stations positions, satellite performances and makes firing user-selectable strategies. The developed program is dedicated to GEO satellites which using LAE generally and it can calculate six back-up strategies and deals situation its maximum firing number is six. The MS-EXCEL software was used for the input and output process. And the numerical calculation part was embodied with MATLAB functions.

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Preliminary Results on Plasma Counterflow Jets for Drag Reduction of a High Speed Vehicle (초고속 비행체 항력 감소를 위한 플라즈마 분사장치에 대한 예비 결과)

  • Kang, Seungwon;Choi, Jongin;Lee, Jaecheong;Huh, Hwanil
    • Journal of the Korean Society of Propulsion Engineers
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    • v.20 no.6
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    • pp.101-112
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    • 2016
  • The characteristic analysis and fundamental test of a plasma generator is performed for drag reduction of a high speed vehicle. In high pressures, thermal plasmas is suitable for generating plasmas. The appropriate plasma torch is selected and used to generate thermal plasmas. The plasma torch, which can emit high-speed and high-pressure plasma jet, is suitable for generating plasma counterflow jet. In this study, the fundamental test and analysis for the plasma torch is summarized. Results show that supplying gas pressures and electrode gap of plasma torch are considered as critical parameters for generating plasma jets.

Preliminary Combustion Tests in Bi-Swirl Coaxial Injectors Using Gaseous Methane/Gaseous Oxygen Propellants (기체메탄/기체산소 추진제를 이용한 동축 와류형 분사기에서의 예비 연소실험)

  • Hwang, Donghyun;Bak, Sujin;Ahn, Kyubok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.23 no.4
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    • pp.70-80
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    • 2019
  • Combustion tests using six bi-swirl coaxial injectors with different shapes and recess lengths were performed in a model combustion chamber capable of flame visualization. By utilizing gaseous methane and gaseous oxygen instead of actual propellants, the effects of injector design and experimental conditions on the flame structure and combustion stability were analyzed. It was found that not only the experimental conditions but also the injector geometry such as the recess length and orifice diameter had a considerable influence on the combustion stability. In addition, it was confirmed that the heat release pattern changed with the occurrence of combustion instability.

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.

CFD Investigation of Rocket Nozzle Plume for Flame Deflector Preliminary Analysis (화염유도로 예비 해석을 위한 로켓노즐 플룸의 CFD 해석 검증)

  • Jun, Doo-Sung;Kim, Jae-Woo;Kim, Jong-Rok;Kim, Woo-Kyeom;Kim, Seung-Cheol;Moon, Hee-Jang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.313-316
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    • 2011
  • This paper investigates CFD investigation on single phase supersonic nozzle flow and 2-phase subson ic flow prior to rocket nozzle supersonic 2-phase flow with water injection within the flame deflector. Numerical results of supersonic nozzle single phase flow showed no notable unrealistic behavior as it captures the usual shock cell structures. Three-dimensional 2-phase flow analysis has also been performed to verify whether the approach can grab the droplet behavior during cooling by water injection. It is expected these basic studies will enhance the cooling problem analysis of supersonic 2-phase rocket plume in the future.

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Effect of Diesel-ethanol Blended Fuel on the Vibration and Emission Characteristics in a Diesel Engine (디젤 엔진의 디젤-에탄올 혼합연료 적용이 엔진 진동 및 배기가스 특성에 미치는 영향)

  • Lee, Doo-Gin;Roh, Hyun-Gu;Lee, Chang-Sik
    • Journal of ILASS-Korea
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    • v.17 no.1
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    • pp.1-8
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    • 2012
  • This study described the effect of the multiple injections and diesel-ethanol on the NVH, combustion and emission characteristics of 4 cylinder common rail diesel engine. In order to investigate the influence of diesel-ethanol blended fuel in a light-duty common rail diesel engine, the injection strategy was varied with pilot injection, double pilot injections, and one main injection at various operating conditions. The results showed that diesel-ethanol blended fuel had longer ignition delay than that of the ultra low diesel fuel(ULSD). Also, in the case of multiple injections, the combustion pressure is increased smoothly near the TDC and the NVH are decreased. In the emission characteristics, diesel-ethanol blended fuel produced lower indicated specific nitrogen oxides(IS-NOX) and indicated specific Soot(IS-soot) emissions, however, indicated specific unburned hydrocarbon(IS-HC) and indicated specific carbon monoxide(IS-CO) emissions are slightly increased.

Study on the Effect of Gas Pressure on Bottle Wall Thickness in the Blow Molding Process (블로우 몰딩 공정에서 분사 압력이 성형 두께에 미치는 영향에 관한 연구)

  • Kim, Dong-Hwan;Seol, Sang-Seok
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.19 no.4
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    • pp.36-44
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    • 2020
  • This study analyzed the deformation behavior of the high density polyethylene (HDPE) bottle in the blow molding process. We carried out finite element (FE) simulations using ANSYS Polyflow. First, the axisymmetric model was executed by 2D FE-simulation to determine the change of bottle wall thickness during the molding process. Then, the square model of the bottle was executed by 3D FE-simulation to gauge the effects of gas pressure on the change of wall thickness. The experiment results showed that the FE-simulations were able to upgrade the quality of the HDPE bottle in the blow molding process. These results can be used as guidance in adjusting gas pressure, as well as be extended for further study to determine process parameters such as temperatures, forming velocity, parison shape, etc.

Design and Validation Test of Rocket Engine Head Generating High Temperature and High Pressure Steam (고온고압 증기 발생장치의 설계 및 예비운용시험)

  • Park, Jinsoo;Yu, Isang;Oh, Junghwa;Ko, Youngsung;Kim, Kyungseok;Shin, Dongsun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2017.05a
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    • pp.637-642
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    • 2017
  • In this study, cold flow and combustion tests are conducted and analyzed to validate designed rocket engine head generating high temperature/pressure steam. At first, uni-injector was designed and manufactured, and cold flow test was conducted. Through this, differential pressure that can supply designed flow rate was confirmed. Also, Each injector's spray pattern were confirmed by patternator. Based on cold flow test results, we selected injectors among the candidates and arranged them on engine head, and cold flow and propellant spray tests were conducted. Finally, combustion test was carried out to analyze the flow rate, pressure, combustion efficiency. As a result, validation of rocket engine head for the development of the high temperature and high pressure steam generator has been completed.

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