• Title/Summary/Keyword: 연소최고압력

Search Result 40, Processing Time 0.025 seconds

Effect of pre-post injection timing of diesel fuel for naval vessel on the combustion and emission characteristics in an optically-accessible single cylinder diesel engine (단기통 디젤엔진에서 함정용 디젤유의 전·후 분사시기가 연소 및 배출가스 특성에 미치는 영향)

  • Lee, Hyungmin
    • Journal of Advanced Marine Engineering and Technology
    • /
    • v.38 no.7
    • /
    • pp.868-876
    • /
    • 2014
  • The objective of this study is focused on the analyzing combustion, carbon monoxide and hydrocarbon emission characteristics of marine diesel oil, utilized for naval propulsion engine, with varying pre-post injection timing of an optically accessible single cylinder engine. And also the combustion process is analyzed by means of a high speed camera visualization. On the result of retarding pre-injection timing toward main injection timing, the mean effective pressure and maximum pressure of combustion chamber are increased; however, the heat release rate is decreased. Furthermore, the emission rates of carbon monoxide and hydrocarbon are reduced in this case. In hence, when a post-injection timing is advanced, the mean effective pressure and maximum pressure are increased, because the combustion has been performed under the high temperature and high pressurized environment during main injection time, and the emission rates of carbon monoxide and hydrocarbon are increased. From the experimental results, it considered that retarding of pre-injection timing affects to shorten the ignition delay of main injection clearly, and to raise the flame intensity comparing to the advanced state. The ignition delay during post-injection is not appeared at any post-injection time, but the flame intensity has been weakened gradually according to the retarding of post-injection timing.

A Study on Synthesis and Characterization of TiZrB$_2$ Composite by SHS Microwave (SHS 마이크로파에 의한 TiZrB$_2$ 복합재료의 합성 및 특성연구)

  • 이형복;윤영진;오유근;안주삼
    • Journal of the Korean Ceramic Society
    • /
    • v.36 no.1
    • /
    • pp.7-14
    • /
    • 1999
  • TiZrB2 solid solution was synthesized using fine powders of Ti, Zr and B by SHS microwave process. The characterization of the synthesized powder and sintered bodies ws investigated. The combustion temperature and rate were increased with increasing the mole ratio of Zr in temperature profile, and showed the maximum combustion temperature and velocity values of 285$0^{\circ}C$ and 14.6mm/sec in Ti0.2Zr0.8B2 composition. Phase separation has been occured into a composite with TiB2 and ZrB2 phases from TiZrB2 solid solution, which was hot pressed sintering at 30 MPa for an hour at 190$0^{\circ}C$. At the composition of Ti0.8Zr0.2B2 the best properties has been obtained in relative density, bending strength, fracture toughness and hardness, with 99%, 680 MPa, 7.3MPa.m1/2 and 2750 Kg/$\textrm{mm}^2$ respectively.

  • PDF

Thermal Analysis of Exhaust Diffuser Cooling Channels for High Altitude Test of Rocket Engine (로켓엔진 고공환경 모사용 디퓨져의 냉각 채널 열 해석)

  • Cho, Kie-Joo;Kim, Yong-Wook;Kan, Sun-Il;Oh, Seung-Hyub
    • Aerospace Engineering and Technology
    • /
    • v.9 no.2
    • /
    • pp.193-197
    • /
    • 2010
  • Water cooling ducts are installed in the exhaust diffuser for high altitude tests of rocket engine to protect diffuser from high-temperature combustion gas. The mass flow rate and pressure of cooling water is designed to prevent boiling of cooling water in the ducts. Therefore, the estimation of maximum temperature of duct wall is important parameter in design of cooling system, especially pressure of cooling water. The method for predicting maximum temperatures of duct walls with variation of coolant flow rates was derived theoretically.

Flow Visualization by Light Emission in the Post-chamber of Hybrid Rocket (광도측정에 의한 하이브리드 로켓 후연소실의 유동 가시화)

  • Park, Kyung-su;Choi, Go Eun;Lee, Changjin
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.43 no.8
    • /
    • pp.677-683
    • /
    • 2015
  • Hybrid rocket combustion displays low frequency instability(LFI, 10~30Hz) at a certain condition. Vortex shedding in the post-chamber is suspected to cause the occurrence of LFI. This study focused on the visualization of flow image using light emissions from high temperature combustion gas. Results shows that combustion pressure oscillates at a frequency of about 18 Hz, which is in phase with oscillations of light emission. Since LFI is not a property of thermo-acoustic instability, this result suggested there exists a physical coupling of pressure fluctuations with light emissions proportional to chemical reaction. Also POD analysis shows that dominant symmetric spatial modes in the stable combustion shift suddenly into asymmetric spatial pattern with the appearance of LFI. Especially, the appearance of mode 3 is a typical change of flow dynamics in unstable combustion representing a rotational fluid motions associated with vortex shedding.

A Study on the Emission Characteristics in 4 Stroke Large Propulsion Diesel Engine (4행정 대형 디젤엔진의 배기 배출특성에 관한 연구)

  • 김현규;전충환;장영준
    • Transactions of the Korean Society of Automotive Engineers
    • /
    • v.9 no.5
    • /
    • pp.38-45
    • /
    • 2001
  • Environmental protection on the ocean has been interested and nowadays the International maritime organization(IMO) has advanced on the prevention of air pollution from ships. This study presents the emission characteristics of 4 stroke propulsion diesel engine in E2 cycle (constant speed) and E3 cycle (propeller curved speed). Also the effects of important operating parameters in terms of intake air pressure and temperature, and maximum combustion pressure are described on the specific emissions. Emissions measurement and calculation are processed according to IMO technical code. The results show that NOx emission level in E3 cycle is higher than E2 cycle due to lower engine speed and lower maximum combustion pressure by retarding fuel injection timing. Intake air temperature has strong influence on NOx emission production. And CO, HC emissions are not affected by maximum combustion pressure and intake air pressure and temperature.

  • PDF

A Study on the Characteristic of NOx Emissions by IMO Operating Modes in a Four Stroke Marine Power Generation Diesel Engine (선박 발전용 4행정 디젤엔진의 IMO 운전모드에 따른 NOx 배출특성에 관한 연구)

  • 김현규;김규보;전충환;장영준
    • Journal of Advanced Marine Engineering and Technology
    • /
    • v.28 no.3
    • /
    • pp.457-465
    • /
    • 2004
  • Environmental protection on the ocean has been interested and nowadays the International Maritime Organization(IMO) has advanced on the prevention of air pollution from ships. This study presents the performance and the emission characteristics of 4 stroke marine diesel engines for generation application in D2 cycle(IMO mode). The effects of important operating parameters, such as intake air pressure. intake air temperature and maximum combustion pressure on NOx emissions were also described. Emissions measurement and calculation are processed according to IMO Technical Code. The results show that the maximum combustion pressure by fuel injection timing control and intake air temperature has strong influence on NOx emission production. But NOx emission is not affected by intake air pressure and exhaust gas back pressure.

A Study on Combustion Characteristics of the Methane-Hydrogen Lean Mixture by Using Multiple Spark Capacity Discharge in a CVCC (I) (반복점화장치 사용시 정적연소실내 메탄-수소 희박혼합기의 연소특성 연구(I))

  • 김봉석
    • Journal of Energy Engineering
    • /
    • v.12 no.2
    • /
    • pp.124-130
    • /
    • 2003
  • In the present study, the combustion characteristics of methane and hydrogen-supplemented methane as alternative fuels for automotive vehicles were investigated at various hydrogen substitution rate, ignition position and ignition methods in a CVCC. As a result, it is possible to decrease the total burning time and to obtain the reduction of NO concentration by using MSCDI device under the lean mixture conditions without deteriorating combustion characteristics such as combustion efficiency, maximum combustion pressure etc.. And by mixing hydrogen into methane, it was found that the reduction of the total burning time was obtained, in comparison with the use of methane only ; and at the same time, the combustion promotion rate was improved remarkably in comparison with the use of methane only.

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
    • /
    • v.8 no.3
    • /
    • pp.150-156
    • /
    • 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.

  • PDF

Improvement of combustion efficiency for marine auxiliary diesel engine (선박발전기용 디젤엔진의 연소효율 개선에 관한연구)

  • Jung, Kyun-Sik
    • Journal of Advanced Marine Engineering and Technology
    • /
    • v.38 no.3
    • /
    • pp.233-239
    • /
    • 2014
  • The accurate engine output is basically one of important factors for the analysis of engine performance. Nowadays in-cylinder pressure analyzer in internal combustion engine is also an indispensable tool for engine research and development, environment regulation and maintenance of engine. The combustion analysis is desperately needed in order to induce a correct judgment on the condition of the engine and suggest the specific ways to improvement as well as the correct engine output. And these tool is advantageous to reduce fuel consumption and maintenance of the engine. In this study, using the developed measuring kit, combustion analysis of marine generator engine which was adapted as test engine was carried out. It was verified that the good operation condition of the engine as well as contributing to fuel savings by checking and readjusting accurately the irregular combustion of the test engine were accomplished. From the results all above, it was recognized that the measuring kit by new method for engine output was developed and verified for its utilities.

Study of Aluminum Agglomeration Model During Solid Propellant Combustion (고체추진제 연소 중 알루미늄 응집 모델 연구)

  • Yoon, Jisang;Lee, Kookjin;Kim, Daeyu;Park, Namho;Ko, Seungwon;Yoon, Woongsup
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.23 no.2
    • /
    • pp.78-86
    • /
    • 2019
  • Aluminum, which is a metal fuel contained in the composite solid propellant, is not ignited and burned on the combustion surface by the oxide film, and it partially melts and coalesces with surrounding aluminum particles. For the evaluation and design of the propellant performance, modeling was performed to predict the size and distribution of agglomerated particles, and the size and distribution of agglomerates were compared and verified through experiment. The predicted values showed the tendency to decrease with pressure as in the experiment, but the error increased as the pressure increased. The agglomerated particle distribution graph showed a difference in the volume fraction although the diameter at the peak was the same.