• 제목/요약/키워드: 프로펠러 단독 시험

검색결과 23건 처리시간 0.023초

초고속선을 위한 공기유입 물제트 추진기 개발 (Development of a Ventilating Waterjet Propulsor for Super-High Speed Ships)

  • 이진태;문일성;박영하;김경열;김기섭
    • 대한조선학회논문집
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    • 제36권3호
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    • pp.41-49
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    • 1999
  • 초고속선의 추진기로 새로이 주목받고 있는 공기유입 물제트 추진기에 대한 타당성을 검토하였다. 본 추진기는 벤틸레이션 상태에서 작동되므로 완전캐비테이션 단면을 사용하여 로터를 설계하였다. 즉 쐐기형(wedge type) 단면과 캐비테이터형(cavitator type) 단면을 갖는 로터 2종류를 설계 제작하여 모형시험을 수행하였다. 로터는 일반적으로 덕트-프로펠러에서 채택하고 있는 Kaplan형 프로펠러 형상을 선택하였다. 캐비테이션 터널 시험부를 개조하여 공기유입 물제트 추진기의 단독특성시험을 수행하였으며, 레이져 유속계를 이용하여 노즐 내부 속도를 엄밀하게 계측하였다. 단독특성 시험은 개조된 캐비테이션 터널의 시험부에서 수행되었으며 완전침수(fully-submerged)상태와 자유분출(free-jet)상태에서 수행되었다. 자유분출상태에서는 후류공기가 유입되어 벤틸레이션 현상이 발생하였으며, 특히 캐비테이터형 단면을 갖는 KP447 로터의 경우 낮은 전진계수에서 작동시킬 경우 완전캐비테이션이 발생하여 성능특성이 크게 변화하였다. 날개 압력면의 뒷날 부근에 높이가 다른 띠를 각각 부착시켜 양력 증가장치로 사용하였으며 이에 의한 추력과 토오크 변화를 계측하였다.

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소형 프로펠러 단독시험기 설계 (A Design Experience of Propeller Open Water Testing Dynamometer)

  • 김재성;송무석;김효철
    • 대한조선학회논문집
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    • 제32권4호
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    • pp.48-54
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    • 1995
  • 선박용 추진기의 단독시험을 위한 소형시험기를 설계제작하고 모형선 예인수조에서 검증시험을 실시하였다. 제작된 시험기는 전동기의 반동력을 스트레인 게이지를 이용하여 직접 계측함으로써 재래의 시험기에서 사용하고 있는 마모성 슬립링을(Slip Ring) 제거하였다. 또한 기기의 구조 부재를 검력계의 검출부로 사용함으로써 소형의 모형선에 탑재될 수 있도록 경량화 및 소형화를 이룩하였다. 개발된 이 제품은 회류수조 등에서 효과적으로 사용될 수 있을 뿐만 아니라 선형시험수조 및 캐비테이션 터널에서 사용될 각종 시험 기기 설계의 기초기술을 포괄하는 것으로 평가된다.

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KP505 프로펠러의 단독성능 시험을 위한 유동해석에 관한 연구 (A Study on the Flow Analysis for KP505 Propeller Open Water Test)

  • 이한섭;김민태;김원섭;이종훈;박상흡
    • 한국산학기술학회논문지
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    • 제20권9호
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    • pp.150-155
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    • 2019
  • 공동현상은 유체의 속도 변화에 의한 압력변화로 인해 유체 내에 빈 곳이 생기는 현상을 말한다. 고속의 액체유동에서 액체의 압력이 포화증기압 이하로 낮아져서 액체 내에 증기 기포가 발생하는 현상이다. 본 연구에서는 선박 및 해양플랜트 분야에서 사용되어지는 유체기기에 대해 CFD 유동해석을 이용하여 선박용 프로펠러의 단독성능 해석기법의 타당성 확보 및 공동에 따른 유동양상을 파악하기 위해 FLUENT를 이용하여 전진비를 증가시키며 3차원 해석을 수행하고 MOERI의 실험 데이터와 비교분석하였다. 대형 컨테이너선용 KP505프로펠러의 사양을 기준으로 전진비에 따른 해석의 결과 전진비 0.7~0.8 구간에서 효율은 60% 수준으로 가장 높게 확인되었다. 압력면과 흡입면의 차이로 추력이 발생되는 것을 확인하였고 프로펠러 표면보다는 이면부근에서 Bubble이 많이 생성될 것으로 추정되며 공동현상이 더 많이 발생할 것이라 추정되었다. 또한 전진비가 증가함에 따라 공동현상은 급격히 감소함을 알 수 있었다. 추력계수와 토크계수는 MOERI 실험값과 비교했을 때 비교적 유사한 결과를 나타내었으며 전진비 1을 제외하고 모두 5%이내의 차이를 나타내었다. 따라서, CFD로 프로펠러 단독 성능에 대한 평가가 가능함을 확인하였다.

SVA Potsdam 프로펠러 단독 및 캐비테이션 성능 수치해석 (Numerical Analysis of Non-Cavitating and Cavitating Performance of a SVA Potsdam Propeller)

  • 김제인;박일룡;김기섭;안종우
    • 대한조선학회논문집
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    • 제54권3호
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    • pp.215-226
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    • 2017
  • This paper presents numerical results of the performance of a marin propeller in cavitating and non-cavitating flow conditions. The geometry and experimental validation data of the propeller are provided in Potsdam Propeller Test Case(PPTC) in the framework of the second International Symposium on Marine Propulsors 2011(SMP'11) workshop. The PPTC includes open water tests, velocity field measurements and cavitation tests. The present numerical analysis was carried out by using the Reynolds averaged Navier-Stokes(RANS) method on a wall-resolved grid ensuring a y+=1, where the SST k-${\omega}$ model was mainly used for turbulence closure. The influence of the turbulence model was investigated in the prediction of the wake field under a non-cavitating flow condition. The propeller tip vortex flows in both cavitating and non-cavitating conditions were captured through adaptation of additional grids. For the cavitation flows at three operation points, Schnerr-Sauer's cavitation model was used with a Volume-Of Fluid(VOF) approach to capture the two-phase flows. The present numerical results for the propeller wake and cavitation predictions including the open water performance showed a qualitatively reasonable agreement with the model test results.

고용량 경사류용 동력계를 이용한 프로펠러 단독시험 특성의 실험적 연구 (Experimental Study of the POW Characteristics using High-capacity Inclined-shaft Dynamometer)

  • 안종우;김기섭;박영하
    • 대한조선학회논문집
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    • 제56권2호
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    • pp.168-174
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    • 2019
  • In order to investigate Propeller Open Water (POW) characteristics for the high-speed propeller in Large Cavitation Tunnel (LCT), the high-capacity inclined-shaft dynamometer was designed and manufactured. Its measuring capacities of thrust and torque are ${\pm}2200N$ and ${\pm}120N-m$, respectively. The driving motor is directly connected to the propeller shaft. Inclined angle of the propeller shaft can be adjusted up to ${\pm}10^{\circ}$. As the pressure inside LCT can be adjusted in the range of 0.1~3.0bar, we can carry out the POW test at high Reynolds number (above $1.0{\times}10^6$) without propeller cavitation and the cavitation test in uniform flow. After the new dynamometer setup in LCT, the Reynolds number variation test and propeller open-water test were conducted at the inclined angle of $0^{\circ}$ and $6^{\circ}$. The present POW results of the new dynamometer are compared with those of the existing high-capacity dynamometer in LCT and of the dynamometer in the towing-tank. Through systematic model tests and comparison with their results, the performance of the new inclined-shaft dynamometer was verified. It is thought the POW test for the high-speed propeller should be better conducted at high Reynolds number.

비정렬 격자를 이용한 선체 주위의 유동 해석 (ANALYSIS OF FLOW AROUND SHIP USING UNSTRUCTURED GRID)

  • 전제형;이상의;권재웅;손재우
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.187-193
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    • 2011
  • In this report, We compared the actual test with the result of pow calculation and Resistance/Self-propulsion of the ship using STAR-CCM+ which is the commercial Reynolds Averaged Navier-Strokes(RANs) Solver. The calculation model was the KRISO Container Ship and 205K Bulk Carrier of Sungdong shipbuilding company. For this calculation, We used Realizable K-Epsilon model for flaw analysis, VOF method for the free surface creation, Moving Reference Frame method for reducing the POW calculation time, and Sliding Mesh method for Self-Propulsion analysis. Calculation of Resistance and Self-Propulsion includes the free-surface. And all calculations in this report were based on unstructured grids.

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RANS법을 이용한 선박 프로펠러 날개 끝 보오텍스 유동 해석 (RANS ANALYSES OF THE TIP VORTEX FLOW OF A MARINE PROPELLER)

  • 박일룡
    • 한국전산유체공학회지
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    • 제21권2호
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    • pp.62-69
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    • 2016
  • It has been highly demanded to improve the accuracy of CFD(Computational Fluid Dynamics) methods for the assessment of the hydrodynamic performance of marine propellers in cavitating and non-cavitating flows. This paper presents a validation study on the numerical simulation of the tip vortex flow of a non-cavitating marine propeller SVA VP1304. The calculations are carried out by using the Reynolds averaged Navier-Stokes(RANS) approach, where the Reynolds Stress Model(RSM) is used for turbulence closure. The present paper contains a grid dependence test for the propeller open water simulations and a special emphasis is placed on conducting a local grid adaptation on the blade tip and in the tip vortex to reasonably reproduce the velocity and the pressure in the tip vortex flow field. The numerical results are compared with the experimental validation data, which are published in the second International Symposium on Marine Propulsors 2011(SMP'11). The present numerical results show a reasonable agreement with the experiments.

비정렬격자를 이용한 프로펠러 성능 및 주위 유동해석 (Fully Unstructured Mesh based Computation of Viscous Flow around Marine Propellers)

  • 김민건;안형택;이진태;이홍기
    • 대한조선학회논문집
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    • 제51권2호
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    • pp.162-170
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    • 2014
  • A CFD(Computational Fluid Dynamics) analysis is presented to predict hydrodynamic characteristics of a marine propeller. A commercial RANS(Reynolds Averaged Navier-Stokes equation) solver, namely FLUENT, is utilized in conjunction with fully unstructured meshes around rotating propeller. Mesh generation process is greatly accelerated by using fully unstructured meshes composed of both isotropic and anisotropic tetrahedral elements. The anisotropic tetrahedral elements were used in the flow domain near the blade and shaft, where the viscous effect is important, having complex shape yet resolving the thin boundary layers. For other regions, isotropic tetrahedral elements are utilized. Two different approaches simulating rotational effect of the propeller are employed, namely Moving reference frame technique for steady simulation, and Sliding mesh technique for unsteady simulation. Both approaches are applied to the propeller open water (POW) test simulation. The current results, which are thrust and torque coefficients, are compared with available experimental data.

층류-난류 천이 모델을 적용한 프로펠러 단독 성능 해석에 관한 CFD 시뮬레이션 (CFD Simulation on Predicting POW Performance Adopting Laminar-Turbulent Transient Model)

  • 김동현;전규목;박종천;신명수
    • 대한조선학회논문집
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    • 제58권1호
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    • pp.1-9
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    • 2021
  • In the present study, the model-scale Propeller Open Water (POW) tests for the propeller of 176K bulk carrier and 8600TEU container ship were conducted through Computational Fluid Dynamics (CFD) simulation. In order to solve the incompressible viscous flow field, the Reynolds-averaged Navier-Stokes (RaNS) equations were employed as the governing equations. The γ-Reθ(gamma-Re-theta) transition model combined with the SST k-ωturbulence model was introduced to describe the laminar-turbulence transition considering the low Reynolds number of model-scale. Firstly, the flow simulation developing over a flat plate was performed to verify the transition modeling, in which the wall shear stresses were compared with experiments and other numerical results. Then, to investigate the effect of the model, the CFD simulation for the POW test was performed and the simulated propeller performance was validated through comparison with the experiment conducted at Korea Research Institute of Ships & Ocean Engineering (KRISO).

Hybrid mesh 및 sliding mesh를 이용한 선박 저항추진 성능 시험 (SHIP RESISTANCE AND PROPULSION PERFORMANCE TEST USING HYBRID MESH AND SLIDING MESH)

  • 이주현;박범진;이신형
    • 한국전산유체공학회지
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    • 제15권1호
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    • pp.81-87
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    • 2010
  • In this study, we conducted resistance and propulsion performance test of ship composed of the Resistance Test, Propeller Open Water Test and Self Propulsion Test using the CFD(Computational Fluid Dynamics). We used commercial RANS(Reynolds Averaged Navier Stokes equation) solver, as a calculating tool. The unstructured grids were used in a bow and stern of ship, having complex shape, for a convenience of generating grids, and the structured grids were adopted in a central hull and rest of hull having a relatively simple shape which is called hybrid grid method. In addition, The sliding mesh method was adopted to rotate a propeller directly in the Propeller Open Water and Self Propulsion Test. The Resistance Test and Self Propulsion Test were calculated using Volume of Fluid (VOF) model and considering a free surface. And all The three cases were applied realizable k-epsilon model as the turbulence model. The results of calculations were verified for the suitability of calculations by comparing MOERI's EFD results.