• Title/Summary/Keyword: nozzle geometry

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Effect of Internal Geometry of Nozzle on the Velocity and Droplet Size of Twin Spray (노즐이 내부형상이 이중분무의 유속과 입경에 미치는 영향)

  • Kim, Young-Jin;Jung, Ji-Won;Kim, Duck-Jool
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.1522-1527
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    • 2004
  • The purpose of this study is to investigate the effect of swirler angle and swirl chamber aspect ration of nozzle on the characteristics of single and twin spray. The performances of nozzle has been investigated by measurements of spray angle, droplet size, velocity and Weber number at a water pressure 0.4MHz. Visualization of spray was conducted to obtain the spray angle and breakup process. The spray characteristics such as droplet size and velocity were measured by Phase Doppler Anemometry(PDA). It was found that the smaller swirler angle, the larger axial velocity became. It was also shown that the larger aspect ratio, the smaller droplet diameter became.

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A Numerical Investigation on the Isentropic Efficiency of Steam Turbine Nozzle Stage with Different Nozzle Vane Thickness and Mass Flow Rate (증기 터빈 노즐 베인의 두께 변화와 유량별 등엔트로피 효율 변화에 관한 수치해석)

  • Lee, Jong Hyeon;Park, Hee Sung;Jung, Jong Yun;Kim, Joon Seob;Jung, Ye Lim;Park, Sung Won
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.10
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    • pp.685-691
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    • 2017
  • In this study, the influence of mass flow rate on the isentropic efficiency of the steam turbine nozzle stage is investigated. A realistic three-dimensional numerical model, which is based on the compressible Navier-Stokes equations, is developed for the steam phase. The comprehensive conservation laws and a kinetic model for steam are investigated. With two different models for the three-dimensional geometry of the nozzle stage, the pressure and temperature distributions, velocity, Mach number. and Markov energy loss coefficient are calculated. A maximum efficiency of 96.66% is found at a mass flow rate of 0.9 kg/s in model A. In model B, a maximum efficiency of 97.32% is found at a rate of 1.6 kg/s. It is determined that the isentropic nozzle efficiency increases as the Markov energy loss coefficient decreases through a nearly linear relationship.

Experimental Study of Discharge Coefficient and Cavitation for Different Nozzle Geometries (노즐 오리피스 형상에 따른 Discharge Coefficient와 Cavitation에 관한 실험적 연구)

  • Kim, Sung-Ryoul;Ku, Kun-Woo;Hong, Jung-Goo;Lee, Choong-Won
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.10
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    • pp.933-939
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    • 2010
  • The purpose of this study is to investigate the generation and development of cavitation in circular and elliptical nozzles. In order to investigate the influence of cavitation, the experiment was conducted with a set of elliptical nozzles that had the same cross-sectional area, different orifice aspect ratios (a/b). Each nozzle was made of acrylic so that visualization was possible. With the injection pressure, the internal flow of the nozzle was classified into the no-cavitation, cavitation, and hydraulic-flip regions. Regardless of the nozzle geometry, with the injection pressure, the flow rate in the no-cavitation and cavitation regions increased and the discharge coefficient decreased. However, the flow rate was constant in the hydraulic-flip region. In the elliptical nozzles, the generation and development of cavitation occurred at higher cavitation number than that in the case of a circular nozzle.

Fatigue Assessment of Reactor Vessel Outlet Nozzle Weld Considering the LBZ and Welding Residual Stress Effect (국부 취화부와 용접 잔류응력 효과를 고려한 원자로 출구노즐 용접부의 피로강도 평가)

  • Lee, Se-Hwan
    • Journal of Welding and Joining
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    • v.24 no.2
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    • pp.48-56
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    • 2006
  • The fatigue strength of the welds is affected by such factors as the weld geometry, microstructures, tensile properties and residual stresses caused by fabrication. It is very important to evaluate the structural integrity of the welds in nuclear power plant because the weldment undergoes the most of damage and failure mechanisms. In this study, the fatigue assessments for a reactor vessel outlet nozzle with the weldment to the piping system are performed considering the welding residual stresses as well as the effect of local brittle zone in the vicinity of the weld fusion line. The analytical approaches employed are the microstructure and mechanical properties prediction by semi-analytical method, the thermal and stress analysis including the welding residual stress analysis by finite element method, the fatigue life assessment by following the ASME Code rules. The calculated results of cumulative usage factors(CUF) are compared for cases of the elastic and elasto-plastic analysis, and with or without residual stress and local brittle zone effects, respectively. Finally, the fatigue life of reactor vessel outlet nozzle weld is slightly affected by the local brittle zone and welding residual stresses.

Determination of Diesel Sprays Characteristics in Real Engine In-Cylinder air Density and Pressure Conditions

  • Payri Raul;Salvador F. J.;Gimeno J;Soare V.
    • Journal of Mechanical Science and Technology
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    • v.19 no.11
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    • pp.2040-2052
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    • 2005
  • The present paper centers on the establishment of a quantified relationship between the macroscopic visual parameters of a Diesel spray and its most influential factors. The factors considered are the ambient gas density, as an external condition relative to the injection system, and nozzle hole diameter and injection pressure as internal ones. The main purpose of this work is to validate and extend the different correlations available in the literature to the present state of the Diesel engine, i.e. high injection pressure, small nozzle holes, severe cavitating conditions, etc. Five mono-orifice, axi-symmetrical nozzles with different diameters have been studied in two different test rigs from which one can reproduce solely the real engine in-cylinder air density, and the other, both the density and the pressure. A parametric study was carried out and it enabled the spray tip penetration to be expressed as a function of nozzle hole diameter, injection pressure and environment gas density. The temporal synchronization of the penetration and injection rate data revealed a possible explanation for the discontinuity observed as well by other authors in the spray's penetration law. The experimental results obtained from both test rigs have shown good agreement with the theoretical analysis. There have been observed small but consistent differences between the two test rigs regarding the spray penetration and cone angle, and thus an analysis of the possible causes for these differences has also been included.

Analysis of Unsteady Cavitating Flows in Fuel Injection Nozzle of Piezo-driven Injector by Eulerian-Lagrangian Multi-phase Method (Eulerian-Lagrangian 다상 유동해석법에 의한 피에조 인젝터의 노즐 내부 비정상 캐비테이션 유동해석)

  • Lee, Jin-Wook;Min, Kyung-Duk;Kang, Kern-Yong;Gavaises, M.;Arcoumanis, C.
    • Journal of ILASS-Korea
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    • v.9 no.4
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    • pp.38-45
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    • 2004
  • This study describes the analysis results of unsteady cavitating flows behavior inside nozzle of the prototype piezo-driven injector. This piezo-driven injector has been recognised as one of the next generation diesel injector due to a higher driven efficiency than the conventional solenoid-driven injector. The three dimensional geometry model along the central cross-section regarding of one injection hole has been used to simulate the cavitating flows for injection time by at fully transient simulation with cavitation model. The cavitation model incorporates many of the fundamental physical processes assumed to take place in cavitating flows. The simulations performed were both fully transient and 'pseudo' steady state, even if under steady state boundary conditions. We could analyze the effect the pressure drop to the sudden acceleration of fuel, which is due to the fastest response of needle, on the degree of cavitation existed in piezo-driven injector nozzle

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Combustion Characteristics of CH4 Nonpremixed Flame with Recession Distance (메탄 비예혼합 화염의 후퇴거리에 따른 연소특성)

  • Kim, Jun-Hee;Ku, Kun-Woo;Hong, Jung-Goo;Lee, Choong-Won;Kim, In-Su;Cheong, In-Mo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.36 no.3
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    • pp.285-291
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    • 2012
  • A lot of research on the stability of nonpremixed flames has focused on the fuel-nozzle and quarl geometries. Of the work carried out, only a small amount has focused on the stability of the nonpremixed flame according to the recession distance and air-nozzle geometry. Therefore, in this study, a coaxial-diffusion-type gas burner with a swirler is designed for the systematic investigation of the combustion characteristics of a $CH_4$ flame depending on the recession distance and secondary air-nozzle geometry. 1st air is flowed through the swirler, and 2nd air is flowed through each nozzle. It is shown that the secondary air velocity greatly influences the flame length and shape. There is an optimum recession distance for each nozzle for the best combustion efficiency. In this study, it is shown that the optimized recession distance is nearly half the outer diameter of the air-supply nozzle.

Aerodynamic Three Dimensional Geometry and Combustor Design for the Compressor of the Medium Speed Diesel Engine Turbocharger (중형 엔진 터보차져의 원심압축기에 관한 공력학적 3차원 형상 및 구동용 연소기 설계)

  • Ryu, Seung-Hyup;Ghal, Sang-Hak;Ha, Ji-Soo;Kim, Seung-Kuk;Kim, Hong-Won
    • The KSFM Journal of Fluid Machinery
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    • v.9 no.2 s.35
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    • pp.30-38
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    • 2006
  • An aerodynamic design for centrifugal compressor which was applied to medium speed diesel engine has been done. First of all, exact compressor specifications must be defined by accurate engine system matching. This matching program has been developed. Using the meanline prediction method, geometric design and performance curves for compressor were established and verified by comparing three dimensional viscous CFD results. The deviation at the design point was about 2.3%. Combustor has been designed and manufactured for the performance test of medium speed diesel engine turbocharger. Fuel nozzle of combustor was designed and its characteristics was analyzed by PIV and PDPA test equipment. Through these results, spray characteristics were studied and flow coefficient equation was deduced.

Effect of Reentrant Type Bowl Geometry on Combustion Characteristics in Diesel Engine -Effect of Aspect Ratio(Bowl Diameter/Bowl Depth)- (리엔트런트형 연소실 형상이 디젤기관의 연소특성에 미치는 영향 -연소실 형상비(Bowl직경/Bowl깊이)의 효과-)

  • Kwon, J.B.;Kim, H.S.;Kwon, I.K.;Oh, K.J.
    • Journal of ILASS-Korea
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    • v.1 no.4
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    • pp.54-62
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    • 1996
  • Effect of reentrant type bowl geometry on combustion characteristics was investigated in a D.1.diesel engine. The main factor was the aspect ratio (Bowl Diameter/Bowl Depth) of bowl of combustion chamber, and the measured data include the cylinder pressure, engine performance and emissions of the engine using the 4 kinds of the combustion chamber. Experimental results indicate that the effect of dc/H and nozzle protrusion are relatively small and there exists an optimum dc/H according to the combustion conditions. It is also found that the smoke emission is quite sensitive the overall combustion time where the 90 percentage of the combustion heat is released. The smoke mission increases by shortening the 90% combustion time while it decreases by delaying the 90% combustion time.

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