• Title/Summary/Keyword: 엔진 내부 유동

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Numerical and Experimental Study to Improve Thermal Sensitivity and Flow Control Accuracy of Electronic Thermostat in the Engine for Hybrid Vehicle (하이브리드 자동차용 엔진 내부의 전자식 수온조절기의 감온성 및 유량제어 정확도 향상을 위한 수치 및 실험적 연구)

  • Jeong, Soo-Jin;Jeong, Jinwoo;Ha, Seungchan
    • Journal of ILASS-Korea
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    • v.26 no.3
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    • pp.135-141
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    • 2021
  • High-efficient HEV Engine cooling systems reflects variable coolant temperature because it can decrease the hydrodynamic frictional losses of lubricated engine parts in light duty conditions. In order to safely raise the operating temperature of passenger cars to a constant higher level, and thus optimize combustion and all accompanying factors, a new thermostat technology was developed : the electronically map-controlled thermostat. In this work, various crystalline plastics such as polyphthalamide (PPA) and polyphenylenesulfide (PPS) mixed with various glass fiber amounts were introduced into plastic fittings of automotive electronic controlled thermostat for the purpose of suppressing influx of coolant into the element and undesirable opening during hot soaking. Skirt was installed around element frame of automotive electronic controlled thermostat for improving thermal sensitivity in terms of response time, hysteresis and melting temperature. To validate the effectiveness and optimum shape of skirt, thermal sensitivity test and three-dimensional CFD simulation have been performed. As a consequence, important improvement in thermal sensitivity with less than 3℃ of maximum coolant temperature between opening and engine inlet was obtained.

Internal Flow Analysis of Urea-SCR System for Passenger Cars Considering Actual Driving Conditions (운전 조건을 고려한 승용차용 요소첨가 선택적 촉매환원장치의 내부 유동 해석에 관한 연구)

  • Moon, Seong Joon;Jo, Nak Won;Oh, Se Doo;Lee, Ho Kil;Park, Kyoung Woo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.3
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    • pp.127-138
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    • 2016
  • Diesel vehicles should be equipped with urea-selective catalytic reduction(SCR) system as a high-performance catalyst, in order to reduce harmful nitrogen oxide emissions. In this study, a three-dimensional Eulerian-Lagrangian CFD analysis was used to numerically predict the multiphase flow characteristics of the urea-SCR system, coupled with the chemical reactions of the system's transport phenomena. Then, the numerical spray structure was modified by comparing the results with the measured values from spray visualization, such as the injection velocity, penentration length, spray radius, and sauter mean diameter. In addition, the analysis results were verified by comparison with the removal efficiency of the nitrogen oxide emissions during engine and chassis tests, resulting in accuracy of the relative error of less than 5%. Finally, a verified CFD analysis was used to calculate the interanl flow of the urea-SCR system, thereby analyzing the characteristics of pressure drop and velocity increase, and predicting the uniformity index and overdistribution positions of ammonia.

Influence of a isolator in supersonic nozzle on thermal choking (초음속 노즐의 분리부가 열폐색에 미치는 영향)

  • Kim, Sangwoo;Kim, Youngcheol;Kim, Jangwoo
    • Journal of Energy Engineering
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    • v.21 no.3
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    • pp.237-242
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    • 2012
  • This study presents numerical solutions of the two-dimensional Navier-Stokes equations for supersonic unsteady flow in a convergent-divergent nozzle with a isolator. The TVD scheme in generalized coordinates is employed in order to calculate the moving shock waves caused by thermal choking. We discuss on transient characteristics, unstart phenomena, fluctuations of specific thrust caused by thermal choking and effects of isolator. The adverse pressure gradient caused by heat addition brings about separation of the wall boundary layers and formation of the oblique shock wave that proceed to upstream. The proceeding speed of the oblique shock wave to upstream direction for the convergent-divergent nozzle with isolator is lower than that for the nozzle without isolator.

Experimental Investigation on Water Hammer Phenomenon in the Recirculation Line of a Liquid Rocket Engine (액체로켓엔진 재순환 유로에서의 수격현상에 관한 실험적 연구)

  • Kim, Bokyem;Hong, Moongeun;Lee, Jisung;Kim, Junghan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.2
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    • pp.110-118
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    • 2021
  • In a liquid rocket engine system, the flow of oxidizer into the combustion chamber is controlled by the main oxidizer shut-off valve. When the valve is closed, the oxidizer flows via the recirculation line, not into the combustion chamber. In this situation, the measured pressure could be much higher than a design value because of the water hammer phenomenon. In this paper, the experiments on the water hammer in the recirculation line with different initial conditions were conducted in order to study the pressure wave produced in each case. According to the experimental results, characteristics of the pressure wave in the recirculation line depend on the initial condition. To be specific, the pressure surge is maximized in case that the shock is condensation-oriented in the end of the recirculation line.

Simulation Study for the Performance Improvement of the Injector Module for Heavy-duty CNG Engines (대형 CNG 엔진용 인젝터 모듈의 성능 개선을 위한 연구)

  • Kim, Yong-Rae;Park, Won-A;Kim, Chang-Gi;Lee, Jang-Hee
    • Journal of the Korean Institute of Gas
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    • v.20 no.4
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    • pp.1-6
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    • 2016
  • A fuel supply system of heavy-duty CNG engine is composed as a module structure which is integrated by about 6 injectors. There are only one input and output passage for gas fuel supply in this injector module. The response performance for transient operation of an CNG engine is very poor because only one output fuel supply line is connected to the intake pipe after a throttle valve. In this study, a new guideline and internal flow design for the CNG injector module is suggested for the improvement of response performance by fluid dynamic simulations. As a result, the response performance of gas fuel supply can be improved by decreasing the total volume of internal flow passages and a same distance design from each injector to the exit of module shows good response performance and acquirement of linearity of fuel supply. But the injection order has little influence to injection performances.

Effect of Backhole on Spray Characteristics of Swirl Injectors in Liquid Propellants Rocket Engine (액체 추진제용 로켓 엔진 스월 인젝터의 백홀로 인한 분무 특성 연구)

  • 황성하;윤영빈
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.2
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    • pp.23-35
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    • 2003
  • "Backhole" is a new geometric parameter and is defined as an extra empty volume which is located behind the tangential entries at the rear part of the vortex chamber in the swirl injector. Backhole makes a difference to the spray characteristics of swirl injectors such as the spray angle, SMD, the mixing characteristics and so on. To find its characteristics, experiments are conducted by using a stroboscopic photography, a PDPA apparatus and a mechanical patternator. With the backhole, the mass flow rate of the swirl injector is increased and the center region of the injected flow has more large volume than that of without the backhole. Also the cone angle can be controlled by the backhole, so that the mixing efficiencies of swirl injectors are changed. Based on cold-flow tests, the swirl injector with the backhole may improve its performance.rformance.

Numerical Study of Turbulence Modeling for Analysis of Combustion Instabilities in Rocket Motor (로켓엔진의 연소 불안정 해석을 위한 난류 모델링의 수치적 연구)

  • 임석규;노태성
    • Journal of the Korean Society of Propulsion Engineers
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    • v.6 no.2
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    • pp.75-84
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    • 2002
  • A numerical analysis of unsteady motion in solid rocket motors with a nozzle has been conducted. The numerical formulation including modified $\kappa$-$\varepsilon$ turbulence model treats the complete conservation equation for the gas phase and the one-dimensional equations in the radial direction for the condensed phase. A fully coupled implicit scheme based on a dual time-stepping integration algorithm has been adopted to solve the governing equations. After obtaining a steady state solution, pulse and periodic oscillations of pressure are imposed at the head-end to simulate acoustic oscillations of a travelling-wave motion in the combustion chamber. Various steady and unsteady state features in the combustion chamber of a rocket motor has been analyzed as results of numerical calculations.

Buzz Suppression of Supersonic Air Inlet by Cowl Position Modification (카울 위치변화에 의한 초음속 공기흡입구의 버즈억제)

  • Shin, Phil-Kwon;Park, Jong-Ho;Lee, Yong-Bum
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.3
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    • pp.10-17
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    • 2005
  • An experimental study was conducted at a Mach number of 2.0 to investigate the buzz suppression method on an axisymmetric, external compression supersonic inlet. The inlet model has a fixed geometry with no internal contraction. The inlet configuration was altered by changing the cowling. Results show that source of buzz has been related to the existence in the flow field of velocity discontinuity across a vortex sheet which originates from a shock intersection point. With external compression inlet, buzz can be suppressed by positioning the oblique shock slightly inside or outside of the cowl.

A Passive Control of the Unsteady Shock-Boundary Layer Interaction in Propulsion Nozzle (추진 노즐에서 발생하는 비정상 충격파-경계층의 간섭현상의 피동제어)

  • Lee, Jong-Sung;Kim, Heuy-Dong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.211-214
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    • 2011
  • In the present work, a computational study was conducted to investigate characteristic of lateral force on the flow fields inside the propulsion nozzle with step. The unsteady, compressible, axisymmetric, Navier-Stocks equations with SST k-${\omega}$ turbulence model are solved using a fully implicit finite volume scheme. In order to simulate the shut-down process of the engine, NPR is varied from 100.0 to 10.0. It is observed that the separation point and Mach-disk strongly depend on the variation of NPR, and adjusting the step lead to significantly different characteristics in the lateral forces.

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Influences of Injector Nozzle Shape on Nozzle Internal Flow and Outlet Characteristics (인젝터 노즐 형상이 노즐 내부 유동 및 출구 특성에 미치는 영향)

  • Kim, Changhyun;Lee, Kangsoo;Park, Jaein;Baek, Jehyun
    • Transactions of the Korean Society of Automotive Engineers
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    • v.21 no.6
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    • pp.108-116
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    • 2013
  • Diesel engine injector is used for spraying the fuel into the cylinder chamber. Complex phenomenon like cavitation occurs from small scale domain, highly pressurized condition and rapid injection. Flow inside the nozzle affects the whole engine performance including combustion and exhaust, therefore understanding the flow inside the injector nozzle is very important. In this paper, cylindrical and convergent-divergent nozzles are suggested for nozzle types and their influences on nozzle internal flow and nozzle outlet characteristics will be analyzed by changing their outlet diameters.