• 제목/요약/키워드: propellers

검색결과 248건 처리시간 0.023초

고차경계요소법을 이용한 정상 유동중의 프로펠러 해석 (Analysis of a Marine Propeller in Steady Flow by a Higher-Order Boundary Element Method)

  • 백광준;서성부;전호환
    • 대한조선학회논문집
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    • 제38권3호
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    • pp.31-40
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    • 2001
  • 일반적으로 특이점들을 분포하여 물체주위 유동장을 해석할 때 저차패널법(Low-Order Panel Method)이 유용하게 사용되어져 왔다. 저차패널법과는 다르게 적분방정식의 계산정도와 해의 수렴성을 높일 수 있는 방법으로서, 물체경계의 형상을 2차 이상의 고차곡면요소로 표현하고 각 곡면요소 내에서 물리량의 변화를 동일한 차수를 갖는 고차경계요소법을 사용할 수 있다. 본 연구에서는 물체표면의 곡면요소와 물리량의 변화를 9절점 라그란지안(Lagrangian) 형상함수를 사용하여 정상 포텐셜유동 중에 작동하는 프로펠러 주위의 유동을 해석하였다. 개발된 프로그램을 프로펠러의 해석에 앞서 원형 날개에 대하여 Jordan의 선형 해석해와 비교하였으며, 두께의 영향을 관찰하였다. 프로펠러의 해석을 위해 DTRC 4119 프로펠러와 DTRC 4842 프로펠러에 적용하여 실험치와 계산치를 비교 검토하였다.

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크루즈선의 횡동요 제어시스템에 미치는 포드 각속도의 영향 (The Effect of the Turning Rate of the Pod Propeller on the Roll Control System of the Cruise Ship)

  • 이성균;이재훈;이기표;최진우
    • 대한조선학회논문집
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    • 제49권1호
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    • pp.14-25
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    • 2012
  • Recently, the application and installation of the pod propeller to the cruise ship is dramatically increased. It is because pod propulsion system allows a lot of flexibility in design of the internal arrangement of a ship. To reflect this trend, many researches have conducted to use the pod propeller for the roll stabilization of a ship. In the paper, a roll stabilization controller is designed by using fins and pod propellers as the control actuators for cruise ships. Two kinds of control algorithms are adopted for the roll control system; LQR (Linear Quadratic Regulator) algorithm and frequency-weighted LQR algorithm. Through the numerical simulation, the effect of the turning rate of the pod propeller on the roll control system is analyzed. Analysis of the simulation results indicated that the turning rate of the pod propellers is one of the important parameters which give the significant effects on the roll stabilization.

Passive, semi-active, and active tuned-liquid-column dampers

  • Chen, Yung-Hsiang;Ding, Ying-Jan
    • Structural Engineering and Mechanics
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    • 제30권1호
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    • pp.1-20
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    • 2008
  • The dynamic characteristics of the passive, semi-active, and active tuned-liquidcolumn dampers (or TLCDs) are studied in this paper. The design of the latter two are based on the first one. A water-head difference (or simply named as water head in this paper) of a passive TLCD is pre-set to form the so-called semi-active one in this paper. The pre-set of water head is released at a proper time instant during an earthquake excitation in order to enhance the vibration reduction of a structure. Two propellers are installed along a shaft inside and at the center of a passive TLCD to form an active one. These two propellers are driven by a servo-motor controlled by a computer to provide the control force. The seismic responses of a five-story shear building with a passive, semiactive, and active TLCDs are computed for demonstration and discussion. The responses of this building with a tuned mass damper (or TMD) are also included for comparison. The small-scale shaking-table experiments of a pendulum-like system with a passive or active TLCD to harmonic and seismic excitations are conducted for verification.

Numerical analysis of sheet cavitation on marine propellers, considering the effect of cross flow

  • Yari, Ehsan;Ghassemi, Hassan
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제5권4호
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    • pp.546-558
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    • 2013
  • The research performed in this paper was carried out to investigate the numerical analysis of the sheet cavitation on marine propeller. The method is boundary element method (BEM). Using the Green's theorem, the velocity potential is expressed as an integral equation on the surface of the propeller by hyperboloid-shaped elements. Employing the boundary conditions, the potential is determined via solving the resulting system of equations. For the case study, a DTMB4119 propeller is analyzed with and without cavitating conditions. The pressure distribution and hydrodynamic performance curves of the propellers as well as cavity thickness obtained by numerical method are calculated and compared by the experimental results. Specifically in this article cavitation changes are investigate in both the radial and chord direction. Thus, cross flow variation has been studied in the formation and growth of sheet cavitation. According to the data obtained it can be seen that there is a better agreement and less error between the numerical results gained from the present method and Fluent results than Hong Sun method. This confirms the accurate estimation of the detachment point and the cavity change in radial direction.

박용프로펠러 생산정보시스템 개발 (Developmen tof a Production lnformation System for Marine Propellers)

  • 박재성;김동수;전차수;박정환;주상윤
    • 한국경영과학회:학술대회논문집
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    • 한국경영과학회/대한산업공학회 2003년도 춘계공동학술대회
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    • pp.194-199
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    • 2003
  • Developed m this research is a production information system for marie propellers. The paper deals with surface modeling and tool path generation modules of the system. Since the input point data may have some errors, the data is examined using the 2nd divided difference. The point data is interpolated to a $G^2$ chord-length spline surface with some end-conditions. The effects of the various end-conditions on the interpolated surface are discussed in the paper. The tool paths for blade, fillet, and boss of the propeller are generated. Some illustrative examples from an industry are presented.

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2축선의 프로펠러 레이싱 추정법에 관한 연구 (Propeller Racing of Ocean-going Ships with Twin Screw Propellers)

  • 박종헌
    • 동력기계공학회지
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    • 제11권1호
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    • pp.98-106
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    • 2007
  • This paper presents a statistical prediction procedure for the propeller racing of ships with twin screw propellers sailing in ocean waves. The propeller racing is one of the most important factors of seakeeping qualities in relation to the safety of main engine and shafting system. It is especially significant key word for designing the twin-screw-propeller-type ship in view of allowable maximum propeller diameter etc.. In former studies, the propeller racing generally means the situation (propeller exposed) in which the relative motion amplitude between ship hull and wave surface would exceed a depth of point in rotary disk propeller. Therefore, it seems that the magnitude of the amplitude and its exceeding frequency have been examined as a principal subject of study as usual. However, the time during which the amplitude exceeds a depth of point must be also one of most important factor affecting the trend of propeller racing. This paper proposes a simply practical method for estimating the time lasting of exposed propeller related to twin screw propeller racing in rough confused seas on the basis of the statistics. Then, it is confirmed that the practical method is useful and convenience for considering the propeller racing in the stage of the basic design.

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점성유동 수치해석법에 의한 선박용 추진기 단독성능 해석 (Analysis of Open-Water Characteristics of Marine Propeller by Computational Method for Viscous Flow)

  • 김덕수;김형태
    • 대한조선학회논문집
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    • 제39권3호
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    • pp.8-17
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    • 2002
  • RANS 방정식의 수치 해법을 사용해서 선박용 추진기 주의의 점성 유동을 계산함으로써 모형 프로펠러 3개(P4119, P4842, KRISO 포드 프로펠러)의 단독 성능을 해석하였다. 프로펠러 단독성능과 날개 압력 분포 그리고 프로펠러 근방의 평균 속도 분포에 대한 본 연구의 수치 해석 결과를 실험 결과와 비교하였으며, 대체로 두 결과가 서로 잘 일치하는 것이 확인되었다. 그러나, 프로펠러 날개 앞날의 압력과 포드 프로펠러의 단독 성능에 대한 본 연구의 결과는 실험 결과와 잘 맞지 않는 것으로 나타났다.

회전(回轉)하는 나선(螺旋)날개 위에서의 경계층(境界層) 해석(解析) (Numerical Calculation of Turbulent Boundary Layer on Rotating Helical Blades)

  • 오건제;강신형
    • 대한조선학회지
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    • 제21권2호
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    • pp.9-17
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    • 1984
  • Laminar and turbulent boundary layers on a rotating sector and a helical blade are calculated by differential method. The estimation of three dimensional viscous flows provide quite useful informations for the design of propellers and turbo-machinery. A general method of calculation is presented in this paper. Calculated laminar boundary layer on a sector shows smooth development of flows from Blasius' solution at the leading edge to von Karman's solution of a rotating disk at the down-stream. Eddy viscosity model is adopted for the calculation of turbulent flows. Turbulent flows on a rotating blade show similar characters as laminar flows. But cross-flow angle of turbulent flows are reduced in comparison with laminar boundary layers. Effects of rotation make flow structures significantly different from two-dimensional flows. In the range of Reynolds number of model scale propellers, large portion of the blade are still in the transition region from laminar to turbulent flows. Therefore viscous flow pattern might be quite different on the blade of model propeller. The present method of calculation is to be useful for the research of scale effects, cavitation, and roughness effects of propeller blades.

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세가지 다른 모형의 덕트 프로펠러의 CFD 해석과 시험에 관한 연구 (CFD Simulations and Experimental Tests for Three Different Ducted Propellers)

  • 정태환;정성재;이승건
    • 한국해양공학회지
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    • 제28권3호
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    • pp.199-208
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    • 2014
  • In this study, propeller open water characteristics ($K_P$, $K_T$ and ${\eta}_o$) were compared for three different ducted propellers using a Computational Fluid Dynamics (CFD) analysis, as well as an experimental test at a basin. The best shape of the duct was selected from the three types of specially designed ducts based on the CFD analysis results. The same propeller model (Kaplan type propeller) was used inside all three duct models, and the propeller open water characteristics were compared, predominantly at the design speed for an underwater vehicle. Finally, the results of the CFD test simulations for the selected duct case were verified by experimental open water tests in a towing tank.

Aerodynamic Design and Analysis of a Propeller for a Micro Air Vehicle

  • Cho Lee-Sang;Yoon Jae-Min;Han Cheol-Heui;Cho Jin-Soo
    • Journal of Mechanical Science and Technology
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    • 제20권10호
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    • pp.1753-1764
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    • 2006
  • A U-80 propeller and its modified version, U-75 propeller, are used for a micro air vehicle. The performance characteristics of a U-80 propeller and a U-75 propeller have not much known in the published literature. Thus, their aerodynamic characteristics are investigated using a lifting surface numerical method. The lifting surface method is validated by comparing computed results with measured data in a wind tunnel. From the computed results, it is found that the U-75 propeller produces larger thrust with higher efficiency than the U-80 propeller. To enhance the performance of these propellers, a new propeller is designed by following the sequential design procedures with the design parameters such as hub-tip ratio, maximum camber and its position, and chord length distribution along the radial direction. The performance of the designed propeller is shown to be improved much comparing with those of both the U-80 and U-75 propellers.