• Title/Summary/Keyword: Nozzle Design

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Design of a Turbine System for Liquid Rocket Engine (액체로켓용 터빈시스템 설계)

  • Choi, Chang-Ho;Kim, Jin-Han;Yang, Soo-Seok;Lee, Dae-Sung;Woo, Yoo-Cheol
    • 유체기계공업학회:학술대회논문집
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    • 2000.12a
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    • pp.145-152
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    • 2000
  • A turbopump system composed of two pumps and one turbine is considered. The turbine composed of a nozzle and a rotor is used to drive the pumps while gas passes through the nozzle, potential energy is converted to kinematic energy, which forces the rotor blades to spin. In this study, an aerodynamic design of turbine system is investigated using compressible fluid dynamic theories with some pre-determined design requirements (i.e., pressure ratio, rotational speed, required power etc.) obtained from liquid rocket engine (L.R.E.) system design. For simplicity of turbine system, impulse-type rotor blades for open type L.R.E. have been chosen. Usually, the open-type turbine system requires low mass flow rate compared to close-type system. In this study, a partial admission nozzle Is adopted to maximize the efficiency of the open-type turbine system. A design methodology of turbine system has been introduced. Especially, partial admission nozzle has been designed by means of simple empirical correlations between efficiency and configuration of the nozzle. Finally, a turbine system design for a 10 ton thrust level of L.R.E is presented.

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Design of a Turbine System for Liquid Rocket Engines (액체로켓용 터빈시스템 설계)

  • Lee, Dae-Sung;Choi, Chang-Ho;Kim, Jin-Han;Yang, Soo-Seok
    • The KSFM Journal of Fluid Machinery
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    • v.5 no.4 s.17
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    • pp.11-18
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    • 2002
  • A turbopump system composed of two pumps and one turbine is considered. The turbine composed of a nozzle and a rotor is used to drive the pumps while gas passes through the nozzle and potential energy is converted to kinetic energy, which forces the rotor blades to spin. In this study, an aerodynamic design of turbine system is investigated with some pre-determined design requirements (i.e., pressure ratio, rotational speed, required power, etc.) following Liquid Rocket Engine (L.R.E.) system specifications. For simplicity of turbine system, impulse-type rotor blades for open-type L.R.E. have been chosen. Usually, the open-type turbine system requires low mass flow-rate compared to close-type system. In this study, a partial admission nozzle is adopted to maximize the efficiency of the open-type turbine system. A design methodology of turbine system was introduced. Especially, partial admission nozzle was designed by means of simple empirical correlations between efficiency and configuration of the nozzle. Finally, a turbine system design is presented for a 10 ton thrust level of L.R.E.

Optimum Design of Air Nozzle System for Automatic Car Wash Machine using CFD and DOE (CFD 및 DOE를 활용한 자동세차기 노즐시스템의 최적설계)

  • Jung, Uk-Hee;Choi, Young-Seok;Kwon, Oh-Myoung;Lee, Kyoung-Yong
    • The KSFM Journal of Fluid Machinery
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    • v.10 no.5
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    • pp.34-40
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    • 2007
  • An optimization approach is investigated for the design of new nozzle system in a automatic car wash machine. Three-dimensional computational fluid dynamics and design of experiment methods have been employed to know the mutual interaction between the nozzle shape in the automatic car wash machine and the airflow velocity distribution on the vehicle surface. The performances of air nozzle system were defined as the velocity magnitude and the uniformity of the velocity on the surface of the car. Predicted jet velocity distributions for the optimized geometry were compared with experimental data and the comparisons showed generally good agreements. Also, the performance of the dryer was improved with the optimized results.

A COMPUTATIONAL APPROACH TO DESIGN THE GEOMETRY OF THE AIR-TWIST NOZZLE (Air-twist 노즐 형상 설계의수치적 연구)

  • Juraeva, M.;Song, D.J.
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.67-70
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    • 2010
  • Spandex yarn requires a twisting process during winding and unwinding processes at the textile industry. The air-twist nozzle is widely used as part of the winding and unwinding. This paper describes computational approach to design the geometry of the air-twist nozzle. The nozzle has circular yarn-channel and the air-inlet which is perpendicularly connected to the yarn-channel with yarn-loading slit. The air-inlet of the nozzle is designed while measurements of the yarn-channel are fixed. The airflow inside the air-twist nozzle is simulated by using Computational Fluid Dynamic model. The Ansys CFX was used to perform steady simulations of the airflow for the air-twisting process. The vortical structure and the airflow pattern such as velocity streamline, vorticity, velocity of the air-twist nozzle are discussed. Computational results are compared with experimental results in this paper.

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A Study on Design of Nozzle Tip for Airless Spray Coating (에어리스 스프레이 도장용 노즐 팁 설계에 관한 연구)

  • Kim, Dong-Keon;Kim, Soon-Kyung
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.11 no.6
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    • pp.183-188
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    • 2012
  • This study was carried out to design the spray nozzle tip for airless spray coating. Airless spray coating is the process of coating an object with a liquid spray of paint or other fluid. The nozzle tip controls the fluid flow rate and creates back pressure in the system. The nozzle tip also defines the spray pattern by the size and shape of the orifice. The spray pattern of nozzle tip was investigated numerically using ANSYS CFX ver. 14.0. It was observed that performance result of designed nozzle tip was correspond well, compared with that of GARCO nozzle tip.

A Study On Characteristics of Nozzle/Flapper Type Flow Control Servo Valve (노즐/플래퍼형 유량제어 서보밸브의 특성에 관한 연구)

  • 윤소남;강보식;성백주;김형의
    • Transactions of the Korean Society of Automotive Engineers
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    • v.8 no.1
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    • pp.54-62
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    • 2000
  • The purpose of this study is to bring out the optimal design factors which effect on dynamic characteristics in the design of flow control servo valve with high response characteristics, and to verify the validity of the design factors. In this study, force feedback type flow control valve with nozzle/flapper and with no drain is studied. And, the effect of the parameters, such as fixed orifice, nozzle diameter, and maximum displacement between nozzle and flapper are analyzed. We have done simulations using the optimal design factors and simulink(Matlab) as a simulation tool, and verified the validity of our simulations by means of comparison our simulation results with an experimental results of another similar valve.

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A Study of the Supersonic Free Jet Discharging from a Petal Nozzle (Petal 노즐로부터 방출되는 초음속 자유제트 유동에 관한 연구)

  • Lee Jun-Hee;Kim Jung-Bae;Kim Heuy-Dong
    • 한국가시화정보학회:학술대회논문집
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    • 2002.11a
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    • pp.109-112
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    • 2002
  • The supersonic jet discharging from a petal nozzle is known to enhance mixing effect with the surrounding gas because it produces strong longitudinal vortices due to the velocity difference from both the major and minor axes of petal nozzle. In the present study, the supersonic free jet discharging from the petal nozzle is investigated experimentally. The nozzles used are 4, 6, and 8 lobed petal nozzles with a design Mach number of 1.7, and the flow fields are compared with a circular nozzle with the same design Mach number. The pitot impact pressures are measured using a fine pilot probe. The flow fields are visualized using a Schlieren optical method. The results show that the petal nozzle has more increased supersonic length compared with the circular jet.

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Design Sensitivity Estimation of Injector Nozzle Hole Considering Cavitation (캐비테이션에 관한 인젝터 노즐 홀의 설계민감도 평가)

  • Yeom, Jeong Kuk;Ha, Hyeong Soo
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.37 no.11
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    • pp.1361-1369
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    • 2013
  • This study performs a computational fluid dynamics (CFD) analysis of the inner flow of a multihole injector nozzle by using ANSYS CFX 13.0. Based on the obtained results, a design of experiment (DOE) was performed and applied to investigate the effects of injector nozzle design parameters on cavitation. To analyze the design sensitivity and signal-to-noise ratio (S/N ratio), the hole diameter, hole length, hole angle, and K-factor of the nozzle hole were selected as design parameters, and the effect of these parameters was investigated at 16 experimental points. Consequently, it was found that the effect of the K-factor on the cavitation and inner flow of the injector nozzle is the greatest. Thus, the selection of a suitable K-factor is important in nozzle design considering cavitation flow.

DESIGN OF WATER INJECTION NOZZLE OF BIDET WITH COMPUTATIONAL FLUID DYNAMICS (유동해석을 통한 물 분사용 비데 노즐 설계)

  • Choi, Y.S.;Yang, S.S.;Jin, S.W.
    • Journal of computational fluids engineering
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    • v.12 no.3
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    • pp.8-12
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    • 2007
  • An optimized bidet nozzle design to form the required swirl water jet is proposed with the help of numerical analysis. The bidet can do the cleaning process of human body by water injection and the speed/pressure/injection angle/magnitude of swirl intensity of water jet determine the cleaning capability and personal subjective feeling. The objective of this research is to design optimal water injection nozzle to make stable swirl intensity. The effect of individual design variables are analyzed from the basic design and the final design is deduced to make high performance water jet within the pre-determined operation conditions.

DESIGN OF WATER INJECTION NOZZLE OF BIDET WITH COMPUTATIONAL FLUID DYNAMICS (유동해석을 통한 물 분사용 비데 노즐 설계)

  • Choi, Y.S.;Yang, S.S.;Jin, S.W.
    • 한국전산유체공학회:학술대회논문집
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    • 2007.04a
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    • pp.68-71
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    • 2007
  • An optimized bidet nozzle design to form the required swirl water jet is proposed with the help of numerical analysis. The bidet can do the cleaning process of human body by water injection and the speed/pressure/injection angle/magnitude of swirl intensity of water jet determine the cleaning capability and personal subjective feeling. The objective of this research is to design optimal water injection nozzle to make stable swirl intensity. The effect of individual design variables are analyzed from the basic design and the final design is deduced to make high performance water jet within the pre-determined operation conditions.

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