• 제목/요약/키워드: Propeller forces

검색결과 79건 처리시간 0.019초

有限要素法에 의한 推進軸系의 광振動計算에 관한 硏究 (Calculation of Transverse Vibration of Ship`s Propulsion Shaftings by the Finite Element Method)

  • 전효중;김희철
    • Journal of Advanced Marine Engineering and Technology
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    • 제3권1호
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    • pp.2-18
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    • 1979
  • Due to increasing ship dimensions and installed propulsive power, resonance frequencies of the propeller shaft system tend to decrease and they can appear in some cases within the operating range of the shaft revolution. For calculation of transverse shaft vibrations, various methods have been proposed but as they are mainly for approximate calculation, no contented results are obtained. For fairly accurate estimation of resonance frequencies in the design stage, one can use transfer matrix method of the finite element method and former is rather prefered in ordinary cases. In this study, the finite element method which is utilized for calculation of the propulsion shaft alignment, is introduced to derive the vibration equation of the ship's propulsion shaftings. The digital computer program is developed to solve the above equation, and the details of preparing the input data are described. The method presented in the underlying report was applied to the shafting of ship which has a lignumvitae bearing to verify its reliability and the results of calculation and those of the measurements on rotating shaft show a good agreement. Calculating methods of exciting of forces and damping forces are also discussed for future work.

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CFD를 이용한 Tanker의 침로안정성 평가 (Evaluation of Course Stability Performance for Tanker using CFD)

  • 홍춘범;양희준
    • 대한조선학회논문집
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    • 제45권5호
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    • pp.523-529
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    • 2008
  • The course stability performance for tankers is evaluated by computational fluid dynamics. In the present work, a Reynolds averaged Navier-Stokes (RANS) code is applied to a maneuvering problem covering the pure drift and yaw motions. The purposes of this study are to evaluate the hydrodynamic force in the bare hull (AFRAMAX) in pure drift and yaw motion and to provide information about the trends in the forces and moments when the rudder angles are varied. The flow simulation is performed by FLUENT. The CFD code is examined to find the optimistic computational condition such as size of grid, turbulence model and initial condition. The hydrodynamic derivatives in drift and pure yaw motion are estimated by the numerical simulation, and then the stability levers are calculated. It is confirmed that the computations show the superiority and inferiority of course stability performance according to the hull forms. Finally, the CFD code is applied to the estimation of the rudder forces when the rudder angles are varied. The propeller effect expressed by the body force distribution is also included.

윤활유(潤滑油) 선미관(船尾管) 베어링 축계(軸系)의 준정적(準靜的) 평형상태(平衡狀態)에 관한 연구(硏究) (Quasi-Static Equilibrium of a Propeller Shaft in a Hydrodynamic Oil-Lubricated Stern Tube Bearing)

  • 안시영;김사수
    • 대한조선학회지
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    • 제26권3호
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    • pp.51-61
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    • 1989
  • 최근(最近)의 배는 에너지 절약(節約)을 도모하기 위하여 프로펠러 회전수(回轉數)의 저속화(低速化)와 더불어 대형화(大型化)되고 있다. 이와 같은 결과(結果)로 선미관(船尾管)의 후부(後部) 베어링에는 집중하중(集中荷重)이 작용(作用)하게 되어 선박(船舶)의 운항능력(運航能力)을 상실할 정도의 대형사고(大型事故)가 일어나고 있는 예(例)가 많다. 이와 관련하여 최근(最近) 유막(油膜)을 고려한 선미관(船尾管) 베어링 해석(解析)에 관(關)한 연구(硏究)가 활발하게 이루워지고 있다. 본(本) 연구(硏究)에서는 지금까지 연구발표(硏究發表)된 유막(油膜)을 고려한 선미관(船尾管) 베어링에 대한 축(軸)의 위치(位置)를 추정(推定)하는 방법(方法)을 수정보완(修正補完)한 새로운 방법(方法)을 제시(提示)하였다. 즉 축계(軸系)에 대해서는 유한요소법(有限要素法)에 의한 삼차원(三次元) 구조해석방법(構造解析方法), 베어링 유막(油膜)은 유한요소법(有限要素法)에 의한 이차원(二次元) 유체역학해석방법(流體力學解析方法), 그리고 축계(軸系)와 베어링 유막간(油膜間)의 준정적(準靜的) 평형점(平衡點)을 구하기 위해서는 최적화(最適化) 기법(技法)이 사용된다. 본(本) 해석방법(解析方法)의 타당성(妥當性) 여부(與否)를 확인(確認)하기 위하여 Vorus 등이 사용(使用)한 시산대상선(試算對象船)에 대한 일련의 수치계산(數値計算)을 수행하고 동(同) 결과(結果)를 Vorus등의 연구 결과와 비교검토(比較檢討)하여 본 결과(結果), 비교적(比較的) 잘 일치(一致)하고 있음을 미루어 보아 본(本) 해석방법(解析方法)의 타당성(妥當性)이 확인(確認)되었다.

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변화하는 단면의 문형구조물의 진동계산에 관한 연구 (A study on the vibration calculation method of portal frame structure with variable sections)

  • 조용수;전효중
    • Journal of Advanced Marine Engineering and Technology
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    • 제9권3호
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    • pp.214-224
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    • 1985
  • In this paper, some theoretical equations are derived to calculate natural frequencies and their modes of a portal type derrick system and developed a computer program to carry out their calculations. The ship's structures, such as funnels, upper decks, engine structures, shaft systems suffer local vibrations of the ship. The exciting forces of vibrations are induced by the bearing force and the surface force of propeller or by the main engine. For solving the vibration problem of riggings like the derrick system the natural frequency of its system must be exactly estimated as far as possible and its resonance condition must be kept out of the normal engine operating speed range. When some severe resonances are encountered after the ship's launching, it may be required a tremendous cost to amend their condition. An experimental model of the portal type derrick is made, which is composed of two posts and a truss. This experimental model is excited by an electrical-magnet, and its vibration responses are found out. The calculating results of the model by the developed computer program are compared with those of measured values of model experiment, and they show fairly good agreements.

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선내 탑재 장비용 마운팅 시스템의 진동특성 평가 프로그램 개발 (Development of evaluation program for vibration characteristics of onboard machinery with resilient mountings)

  • 김극수;최수현;백일국;조연;김병곤
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2001년도 춘계학술대회논문집
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    • pp.155-160
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    • 2001
  • This study is performed to evaluate and design the vibration characteristics of the onboard machinery with resilient mountings. To reduce the vibration level of onboard machinery with resilient mountings, it is important to evaluate and, if necessary, modify the vibration characteristics of the resilient mountings. In this study, we have developed a program to calculate natural frequencies of the machinery with resilient mountings, forced vibration levels due to internal excitation force of the machinery itself and external excitation forces. of the main engine and the propeller. and the force and motion transmissibility of the resilient mountings. The developed program is also able to be applied to optimal design of the resilient mountings for obtaining a target natural frequency and for achieving a minimum forced vibration level at the center of gravity of the machinery.

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An Experimental Evaluation of the Coanda Jet Applied High Efficient Rudder System for VLCC

  • Park, Bong-Joon;Kim, Hyo-Chul
    • Journal of Ship and Ocean Technology
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    • 제8권2호
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    • pp.1-12
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    • 2004
  • To keep the ocean environment from pollutions, strict international requirements on the controllability are arisen to the VLCC. Especially in low speed operations near the harbor, the VLCC is often supported by tug to replenish the insufficient rudder force. When water jet is blown to the flapped rudder, the Coanda effect induces a high-lift force by delaying stall and re-enforcing circulation in a large angle of attack (Lachmann 1961, Ahn 2003). Based on numerous research efforts, the rudder system supported by the Coanda effect was devised and its performances were evaluated in the towing tank for a large VLCC model. Hydrodynamic forces acting on the rudder system were measured with a water jet blowing on the rudder surface and compared with those acting on a conventional rudder. The effectiveness of the new rudder system was proven through an experimental evaluation.

특이점분포방식(特異點分布方式)에 의한 비정상수중익문제(非正常水中翼問題)에 대(對)한 해석(解析) (Solution of Unsteady Hydrofoil Problems by Discrete Vortex Method with Application to Fish Propulsion)

  • 김형태;이창섭
    • 대한조선학회지
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    • 제18권3호
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    • pp.11-27
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    • 1981
  • This paper is prepared to solve the problem of two-dimensional sinusoidal motion of hydrofoil, which can be related not only to the prediction of unsteady forces acting on the marine propeller blade but to the study of aquatic animal's undulatory mode of propulsion. For convenience's shake, this manuscript can be devided into two parts. In the first part, the lift and moment coefficients have been calculated by the method of conformal transformation. In the other part, the thrust and the hydromechanical efficiency have been evaluated, using Lagally's technique having extended to the unsteady case, they also have been compared with the results, which had been obtained by Lighthill[6] and Wu[7] using Prandtl's acceleration potential.

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비대선형의 조종 유체력 미계수 및 간섭 계수에 관한 실험적 연구 (Experimental Study on Manoeuvring Hydrodynamic Derivatives and Interaction Coefficients of Full Form Ship)

  • 최명식;윤점동;이경우
    • 한국항해학회지
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    • 제18권4호
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    • pp.49-57
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    • 1994
  • In marine transportation of bulk cargoes such as crude oil. ore, coal etc., a lot of full form ship which have poor manoeuvrability were presented in many countries. Since ship manoeuvrability depends upon many parameters namely hydrodynamic derivatives, interference factors etc., as external forces, it is of great importance that we investigate these values of parameters on analysis of manoeuvrability. In this paper, we investigated and analyzed interaction coefficients among hull-propeller-rudder for a full form ship by captive model test in circulating water channel, and then compared with experimental results by PMM test. A tanker model ship which has 0.83 as block coefficient and MMG mathematical models were used in this experiment. Almost same tendencies were found in qualitative analysis, even though more serial experiments were demanded in quantitative analysis.

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CFD estimation of HDCs for varying bodies of revolution of underwater gliders

  • R.V. Shashank Shankar;R. Vijayakumar
    • Ocean Systems Engineering
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    • 제13권3호
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    • pp.269-286
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    • 2023
  • Autonomous Underwater Gliders (AUGs) are a type of Underwater Vehicles that move without the help of a standard propeller. Gliders use buoyancy engines to vary their weight or buoyancy and traverse with the help of the Lift and Drag forces developed from the fuselage and the wings. The Lift and Drag Coefficients, also called Hydrodynamic coefficients (HDCs) play a major role in glider dynamics. This paper examines the effect of the different types of glider fuselages based on the bodies of revolution (BOR) of NACA sections. The HDCs of the glider fuselages are numerically estimated at a low-speed regime (105 Reynolds Number) using Computational Fluid Dynamics (CFD). The methodology is validated using published literature, and the results of CFD are discussed for possible application in the estimation of glider turning motion.

정상 및 비정상 유동중 덕트 프로펠러의 성능해석 (Steady/Unsteady Analysis of Ducted Propellers by Using a Surface Panel Method)

  • 김광;표상우;서정천
    • 대한조선학회논문집
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    • 제36권1호
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    • pp.30-36
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    • 1999
  • 본 논문에서는 교란 포텐셜을 기저로 하는 패널방법을 사용하여 정상 및 비정상 유동중의 덕트 프로펠러 성능해석을 수행하였다. 경계면은 쌍곡면패널로 이산화하였으며, 각 경계조건은 패널의 중심점에 적용하였고 Kutta조건의 수렴성 향상을 위해 Suh[1]의 방법을 사용하였다. 후류면의 위치계산을 위하여 덕트의 영향을 고려한 비선형 모델을 사용하였다. 비정상 유동중 해석은 시간영역에서 수행하였다. 수치적인 검증은 정상 및 비정상 유동중에 대해서 이루어졌으며 개발된 프로그램이 좋은 수렴성을 가지고 있음을 확인하였다. 날개와 덕트의 간격에 따른 날개의 순환분포 변화를 보였으며 No.19a 덕트를 갖는 Ka4-70 날개(피치비 1.2)에 대해 실험값과 개발된 프로그램의 수치결과를 비교하였다. 비교결과 실험값과 계산값은 좋은 일치를 보이고 있음을 확인하였다.

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