• Title/Summary/Keyword: Nozzle Tip

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Experimental investigations and development of mathematical model to estimate drop diameter and jet length

  • Roy, Amitava;Suneel, G.;Gayen, J.K.;Ravi, K.V.;Grover, R.B.
    • Nuclear Engineering and Technology
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    • v.53 no.10
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    • pp.3229-3235
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    • 2021
  • The key process used in nuclear industries for the management of radiotoxicity associated with spent fuel in a closed fuel cycle is solvent extraction. An understanding of hydrodynamics and mass transfer is of primary importance for the design of mass transfer equipment used in solvent extraction processes. Understanding the interfacial phenomenon and the associated hydrodynamics of the liquid drops is essential for model-based design of mass transfer devices. In this work, the phenomenon of drop formation at the tip of a nozzle submerged in quiescent immiscible liquid phase is revisited. Previously reported force balance based models and empirical correlations are analyzed. Experiments are carried out to capture the process of drop formation using high-speed imaging technique. The images are digitally processed to measure the average drop diameter. A correlation based on the force balance model is proposed to estimate drop diameter and jet length. The average drop diameter obtained from the proposed model is in good agreement with experimental data with an average error of 6.3%. The developed model is applicable in both the necking as well as jetting regime and is validated for liquid-liquid systems having low, moderate and high interfacial tension.

Establishment of Low Temperature Environment System Using Polar Environment Performance Test Construction (극지환경성능시험설비를 활용한 저온환경 시스템 구축)

  • Sung, Ki-Young;Han, Seong-Jong;Lee, Jung-Hee
    • Journal of the Korean Society of Industry Convergence
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    • v.25 no.5
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    • pp.843-851
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    • 2022
  • This paper was conducted to study the conditions for the manufacture and operation of artificial snow removal and ice-making test facilities so that the test equipment can be tested in a low-temperature environment using the polar environment performance test facility. The polar environment performance test Facility is designed to artificially simulate extreme environments up to -65 ℃, and is a mid-to-large low-temperature environment test facility that can perform performance tests on offshore plant equipment, ships, leisure, and offshore structures. To verify the safety of deck work of ships operating in polar environments, artificial snow removal and artificial ice making devices were manufactured, and we conducted research on various operating environments using these facilities. For the efficient operation of artificial snow and ice making facilities, it is important to continuously supply dry air, and it has been found that installing an additional heater at the tip of the nozzle is effective in preventing freezing.

Characteristics and Biocompatibility of Electrospun Nanofibers with Poly(L-lactide-co-ε-caprolactone)/Marine Collagen (전기 방사법을 통해 제조된 Poly(L-lactide-co-ε-caprolactone)/Marine Collagen 나노파이버의 특성 및 세포친화력 평가)

  • Kim, Woo-Jin;Shin, Young-Min;Park, Jong-Seok;Gwon, Hui-Jeong;Kim, Yong-Soo;Shin, Heung-Soo;Nho, Young-Chang;Lim, Youn-Mook;Chong, Moo-Sang
    • Polymer(Korea)
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    • v.36 no.2
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    • pp.124-130
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    • 2012
  • The uniform nanofibers of poly(L-lactide-$co$-${\varepsilon}$-caprolactone) (PLCL) with different contents of marine collagen (MC) were successfully prepared by electrospinning method. The effects of the major parameters in electrospinning process such as tip to target distance (TTD), voltage, nozzle size and flow rate on the average diameter of the electrospun nanofiber were investigated in generating composite nanofiber. The diameter and morphology of the nanofibers were confirmed by a scanning electron microscopy (SEM). Also, we measured a water contact angle to determine the surface wettability of the nanofibers. The average diameter of the nanofibers decreased as the value of TTD, MC contents, and voltages increased in comparison with that of pristine PLCL nanofiber. In contrast, the diameter of the nanofibers increased as the flow rate and inner diameter of nozzle increased in comparison with that of pristine PLCL. In addition, the hydrophilicity of the nanofiber and attachment of MG-63 cells on the sheets increased as incorporated collagen contents increased. Therefore, the marine collagen would be a potential material to enhance cellular interactivity of synthetic materials by mimicking the natural tissue.

The Experimental Studies of Vacuum Residue Combustion in a Small Scale Reactor (소규모 반응로를 이용한 감압 잔사유지 연소실험)

  • Park Ho Young;Kim Young Ju;Kim Tae Hyung;Seo Sang Il
    • Journal of Energy Engineering
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    • v.14 no.4 s.44
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    • pp.268-276
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    • 2005
  • Vacuum Residue (VR) combustion tests were carried out with a 20 kg/hr (fuel feed rate) small scale reactor. The nozzle used was a steam atomized, internal mixing type. Compared to heavy oil, vacuum residue used in this work is extremely high viscous and contains high percentages of sulfur, carbon residue and heavy metals. To ignite atomized VR particles, it was necessary to preheat the reactor, and it has been done with LP gas. The axial and radial gas temperature, major species concentrations and solid sample were analyzed when varying the fuel feed rate. The main reaction zone of atomized VR-air flame in a reactor was anticipated within about 1 m from the burner tip by considering the profiles oi gas temperature, species concentration and particle size measured along with the reactor. At downstream, the thermally, fully developed temperature distribution was obtained. SEM photographs revealed that VR carbon particles collected from the reactor are porous and have many blow-holes on the particle surface.

A Study on Partial Admission Characteristics of a Multi-Stage Small-Scaled Turbine (다단 소형 터빈에서의 부분분사 특성에 관한 연구)

  • Cho, Chong-Hyun;Jeong, Woo-Chun;Kim, Chae-Sil;Cho, Soo-Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.9
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    • pp.943-954
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    • 2010
  • In this study, a radial inflow type turbine was applied and the outer diameter of the turbine rotor was 108 mm. The turbine blade on a circular plate disc was designed as an axial-type because its partial admission rate was 1.4-4.1%. The turbine consisted of three stages. The performance test has been conducted with various admission rates, tip clearances and nozzle flow angles. The turbine output power was measured on each stage. The turbine performance was obtained in a wide rotational speed range in order to compare its performance according to various operating conditions. The net specific output torque was also measured to compare its overall performance. Computational analysis was conducted for predicting turbine performance. The computed results were in good agreement with the experimental results.

Study on Spray Visualization and Atomization Characteristics of Air-assist Type Injector for Scramjet Engine (스크램제트 엔진용 공기 보조형 인젝터의 분무 가시화 및 미립화 특성에 관한 연구)

  • Lee, Jinhee;Lee, Sanghoon;Lee, Kyungjae;Kim, Jaiho;Yang, Sooseok
    • Journal of the Korean Society of Propulsion Engineers
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    • v.21 no.5
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    • pp.88-96
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    • 2017
  • As a part of the development procedures of scramjet engine with a regenerative cooling system, this experiment was performed using air-assist type injectors for scramjet engine. Two types of injectors were used in this experiment with the 90 and 60 degrees of the injection angle to the main flow. Mie-scattering was used for spray visualization and PDPA was used for the measurement of the atomization characteristics. It was found that increasing the pressure of supplied gas and the distance from nozzle tip led to the enhancement atomization characteristics and the injector with 60 degrees injection angle has better atomization characteristics than 90 degrees injector.

Experimental Study on the Spray Characteristics of the Diesel Single Hole Type Nozzle (디젤단공노즐의 분무특성에 관한 실험적 연구)

  • 안병규;송규근;윤소남;최병오
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2003.06a
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    • pp.764-767
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    • 2003
  • The characteristics of diesel spray have much effect on the engine performances such as power. fuel consumption rate and emissions. Therefore, the measurement of fuel spray characteristics is very important for the improvement of heat engine. The factors which control diesel spray characteristics are injection pressure, ambient temperature and density etc. Spray behaviors are visualized by using the high speed video camera and spray angle, spray penetration are measured. Experimental equations of spray penetration and spray angle were derived by using the experimental results. 1) Ambient temperature and density influence on the characteristics of diesel spray. 2) Experimental equation of spray penetration is expressed as follows 0<t< $t_{b}$ ; $S_1$=11.628$\Delta$ $P^{0.485}$ $\rho$$_{a}$ $^{-0.478}$ $t^{1.337}$, $t_{b}$ <t; $S_2$=7.457$\Delta$ $P^{0.523}$ $\rho$$_{a}$ $^{-0.382}$ $t^{0.548}$ 3) Experimental equation of spray Angie is expressed as follows $T_{a}$ =293K; Tan($\theta$/2)=059($\rho$$_{a}$ / $\rho$$_{f}$ )$^{0.437}$, $T_{a}$ =473K; Tan($\theta$/2)=0588($\rho$$_{a}$ / $\rho$$_{f}$ )$^{0.404}$_{f}$ )$^{0.404}$

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A Study on the Fluid Interception Valve According to Non Rubbing Top and Bottom operation Shaft (무마찰 상하작동 축에 의한 유체차단 밸브에 관한 연구)

  • Cho, Myung-Hyun
    • Journal of the Institute of Electronics Engineers of Korea TE
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    • v.42 no.4
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    • pp.27-32
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    • 2005
  • Liquid valve is divided into cylinder and liquid part or composed of a single body structure. It becomes a connected structure to cylinder head after inserting stainless(STS) shaft to Teflon packing. In injecting and intercepting fluid, working efficiency becomes low because of the top and bottom round trip operation the friction between Teflon packing and STS shaft fluid leakage, decline of working environment, and each part replacement. And so target value is unattainable in productivity liquid valve design, quality, and structure change are studied. In this paper, designed to solve the existing problems basically, to prevent friction of Piston by developing diaphragm linked with piston, to satisfy long life, and to provide the prevention of leakage. The objective of the study is also to prevent remains fluid at nozzle tip after dispensing fluid, and bell close with the suction function in piston retreating.

A Study on the Particle Size and Velocity Profile on a Gasoline Port Injector Using a Phase Doppler Particle Analyzers (PDPA) (위상 도플러 입자 분석기(PDPA)를 이용한 가솔린 포트 인젝터의 입자 크기 및 속도 프로파일에 관한 연구)

  • KIM, HYOJIN;JO, HYUN;TONGCHAI, SAKDA;LIM, OCKTACKE
    • Transactions of the Korean hydrogen and new energy society
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    • v.28 no.3
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    • pp.300-307
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    • 2017
  • This study is to investigate particle size and velocity profile of gasoline port injector using Phase Doppler Particle Analyzer (PDPA). In this experiment, a GV 250 Delphi port injector used for motorcycles was used for liquid injection. The injector consists of four holes and has a static flow rate of 2.13 g/s. The fuel used in the injection was N-heptane, which is similar to gasoline, as an alternative fuel. The test fuel was injected at an atmospheric temperature of $20^{\circ}C$ and an open atmosphere of 1 atm. The injection time was 10 ms and the injection pressure was 3.5 bar in PDPA experiment. The experimental target position was fiexd at 30, 50 and 75 mm from the nozzle tip and data were collected for a total of 10,000 samples. The experimental results show that the length diameter (D10), the Sauter mean diameter ($D_{32}$), and the mean droplet velocity (MDV) are $45-54{\mu}m$, $99-115{\mu}m$ and 15-21 m/s, respectively.

An Experimental Study on the Damage of the Data Process Equipment When $CO_2$ is Discharged ($CO_2$ 소화설비 방사시 정보저장장치의 저온손상에 관한 연구)

  • 이수경;김종훈;김영진;최종운
    • Fire Science and Engineering
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    • v.13 no.3
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    • pp.19-26
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    • 1999
  • $CO_2$ extinguishing system is the most $\phi$pular among the gas extinguishing system. $CO_2$ is usually stored with liquified state. But, it gasifies at the tip of nozzle when $CO_2$ was released through the pipe and head. A ro$\alpha$n temperature is very low when $CO_2$ was released. So electrical instrument, magnetic storage equipment and memory semiconductor are electrically or physically injured by cooling effect in a few minutes. So, we intend to find out temperature profile and electrical damage in compartment area, and supply basic d data for research and making standards and code through the full scale experiment. As result of experiment on the damage due to cooling effect from $CO_2$ extinguishing system, i instantaneous discharging temperature. was $-82.5^{\circ}C$ in average. An average temp. in the compartment after discharging $CO_2$ was $-40^{\circ}C$.

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