• Title/Summary/Keyword: propeller shaft

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Development of New Cavitation Erosion Test Method for Analyzing the Durability of Erosion Resistance Paint (내침식페인트 성능 판별에 적합한 새로운 캐비테이션 침식시험기법 개발)

  • Paik, Bu-Geun;Kim, Kyung-Youl;Kim, Ki-Sup;Kim, Tae-Gyu;Kim, Kyung-Rae;Jang, Young-Hun;Lee, Sang-Uk
    • Journal of the Society of Naval Architects of Korea
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    • v.47 no.2
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    • pp.132-140
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    • 2010
  • The very erosive cavitation is simulated by an inclined propeller dynamometer in the medium-size cavitation tunnel of MOERI. The inclined shaft for propeller makes strong cavitaion, which occurs around the root of a propeller blade. The cavitation begins at the leading edge of the propeller and contracted toward the trailing edge through the reentrant jet action. The cavity focused on the region near the trailing edge collapsed over the blade surface. As the impact pressure by the cavitation collapsing is too strong, it can damage the blade surface in the form of pit. This cavitation impacts created by the collapsing process are similar to the full-scale ones and are different from those by other erosion test methods. The newly developed cavitation erosion test method can be applied to evaluate the materials such as metals, ceramics and coatings in terms of cavitation resistance.

A Study on the Analysis of Axial Vibration of Flexible Shafting System for Propulsion and Lift in Air Cushion Vehicle (공기부양선의 추진 및 부양축계 종진동 해석에 관한 연구)

  • Son, Seon-Tae;Kil, Byung-Lea;Kim, Jung-Ryul
    • Journal of Advanced Marine Engineering and Technology
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    • v.31 no.6
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    • pp.768-776
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    • 2007
  • In this study, axial vibration analysis has been conducted on a propulsion and lift shafting system for an air cushion vehicle using ANSYS code. The shafting system is totally flexible multi-elements system including wood composite material of air propeller. aluminum alloy of lift fan and thin walled shaft with flexible coupling. The analysis calculated the axial natural frequencies and mode shapes of the shafting system taking into account an equivalent mass-elastic model for shafting system as well as the three-dimensional models for propeller blade and fan impeller. Such a flexible shafting system has very intricate vibrating characteristics and especially, axial natural frequencies of flexible components such as propeller blade and impeller of lift fan can be lower to the extent that causes a resonance in the range of operating revolution. The results for axial vibration analysis are presented and compared with the results of axial vibration test for lift fan conducted during Sea Trial.

Performance Characteristics of an Axial Propeller Small-hydro Turbine with Various Cambers of Runner Blade (캠버각 변화에 따른 소수력 축류 프로펠러 수차의 유동 특성 연구)

  • Byeon, Sun-Seok;Kim, Tae-Youn;Han, Sang-Meok;Kim, Jeong-Hwan;Kim, Youn-Jea
    • New & Renewable Energy
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    • v.8 no.2
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    • pp.44-51
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    • 2012
  • The aim of this paper is to examine the hydraulically optimized camber of a blade. Prior studies have tried to determine the sound method of design on small-hydro turbines. These have appeared to realize a reasonably efficient small-hydro turbine. Nonetheless, specific and accurate design data have not as yet been established for the shape of the runner blade. Hence, this study examines the performance characteristic of an axial propeller turbine with 0~8% camber variations. The results of output power, efficiency, and pressure distribution of the turbine are graphically depicted. The definition of camber refers to the NACA airfoil. The commercial finite element analysis (FEA) packages, ANSYS, and CFX are used in this study. The results revealed the performance characteristics on small-hydro turbine and suggested a highly efficient section shape of the runner.

Operation limits analysis of PW206C turboshaft engine in manual mode (PW206C 터보축 엔진의 수동운용범위 분석)

  • Lee, Chang-Ho
    • Journal of the Korean Society of Propulsion Engineers
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    • v.12 no.4
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    • pp.42-47
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    • 2008
  • The power control system of Smart UAV is similar to the propeller pitch governing concept of turboprop aircraft. The pilot adjusts the engine power directly and the pitch governor controls the propeller pitch to maintain the propeller rotational speed. The electronic engine controller(EEC) of PW206C engine developed for helicopter is not fit for the power control concept of Smart UAV, and therefore the manual back-up system of PW206C engine is used for the engine power control of Smart UAV. Engine performance estimation program is used to predict the control range of power lever angle(PLA) according to the variation of engine output shaft speed, flight altitude and flight speed. These data provide a guide for the PLA control in manual mode operation.

Design of an Active Shaft Grounding System for the Elimination of Alternating Electromagnetic Field in Vessel (선체 교류 전자장 제거를 위한 능동 축 접지 시스템 설계)

  • Kim, Tae-kue;Ahn, Ho-kyun;Yoon, Tae-sung;Park, Seung-kyu;Kwak, Gun-pyong
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.19 no.6
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    • pp.1515-1524
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    • 2015
  • Recently, for the purpose of preventing the corrosion of a vessel, the electrical corrosion protection device that prevents the corrosions of the hull and the propeller is widely used. However, the electrical corrosion protection method artificially emits the current into the seawater around the hull using the power supply in order to make the hull and propeller be in the state of not being corrosion, so that electromagnetic field is generated outside the hull by the current emitted into the seawater. In this paper, the static and alternating constituents of the electromagnetic field generated in underwater outside the hull are analyzed and a countermeasure is investigated to reduce the strength of the electromagnetic field. In conventional shaft grounding system, the shaft potential is maintained above at least 100mV and the alternating current component constitutes more than 10% of the total current. However, in this paper, a control system was designed in order that the alternating current component and the shaft potential which generate electromagnetic field are maintained within 1% and 2mV respectively, and the performance was verified by simulation.

Modeling and Simulation of Small and Medium-sized Ships for Fuel Reduction Rate Verification (연료 감소율 검증을 위한 중소형 선박의 모델링 및 시뮬레이션)

  • Kim, Sung-Dong;Kim, Nam-Ho
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.26 no.6
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    • pp.914-921
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    • 2022
  • The International Maritime Organization (IMO) has set a goal of reducing ship's carbon dioxide emissions by 70% and greenhouse gas emissions by 50% by 2050 compared to 2008. Shipowners and shipyards are promoting various R&D activities such as LNG propulsion, ammonia propulsion, electric propulsion, CO2 capture, and shaft generators as a way to satisfy this problem. The dual shaft generator has the advantage that it can be directly applied to an existing ship through remodeling. In this paper, the total fuel reduction rate that can be obtained by applying the shaft generator to the existing ship was verified through simulation. For this purpose, the size of the medium-sized ship was defined, and the governor, diesel engine, propeller, torque switch, generator for shaft generator, propulsion motor for shaft generator, and ship model were modeled and simulated.

A Study on the Reduction of Differential Vibration of FR Passenger Car (후륜구동 승용차의 디퍼렌셜 진동저감에 관한 연구)

  • 최은오
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 1997.10a
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    • pp.316-321
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    • 1997
  • The purpose of this study is to reduce the vibration noise of differential gear by reducing torque fluctuation of drive pinion shaft which causes vibration noise of differential gear in rear wheel drive vehicles. For this we developed multi-degree of freedom analysis model in which mass moment of inertia and torsional spring combined, the validity of the simulation model was checked by the field test and we examined the influence of torsional vibration of driveline elements by performing forced vibration analysis of engine excitation torque. We studied the methods for reducing torsional vibration of driveline according to the design factor of propeller shaft and examined the effects reducing vibration differential gear by applying flexible coupling.

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Vibrational analysis of driveline for reducing differential gear vibration (차동 기어의 진동 저감을 위한 동력 전달계 진동 해석)

  • 최은호
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.6 no.3
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    • pp.96-102
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    • 1997
  • Eigenvalue analysis of vibration mode and an analysis by frequency response among the methods of predicting gear noise are related with transmitting sound of vibration. In this study we intended to reduce the vibration noise of differential gear by reducing torque fluctuation of drive pinion shaft which causes vibration noise of differential gear in rear wheel drive vehicles. For this we developed multi-degree of freedom analysis model in which mass moment of inertia and torsional spring combined and we examined the influence of torsional vibration of driveline elements by performing forced vibration analysis of engine excitation torque. We studied the methods for reducing torsional vibration of driveline according to the design factor of propeller shaft and examined the effects reducing vibration in differential gear by applying flexible coupling.

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Optimum Design of Diameters of Marine Propulsion Shafting by Binary-Coded Genetic Algorithm and Modal Analysis Method (이진코딩 유전알고리즘과 모드해석법을 이용한 선박 추진축계의 직경 최적설계)

  • Choi, Myung-Soo;Moon, Deok-Hong;Seol, Jong-Ku
    • Journal of Power System Engineering
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    • v.7 no.3
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    • pp.29-34
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    • 2003
  • Genetic algorithm is a optimization technique based on the mechanics of natural selection and natural genetics. Global optimum solution can be obtained efficiently by operations of reproduction, crossover and mutation in genetic algorithm. The authors developed a computer program which can optimize marine propulsion shafting by using binary-coded genetic algorithm and modal analysis method. In order to confirm the effectiveness of the developed computer program, we apply the program to a optimum design problem which is to obtain optimum diameters of intermediate shaft and propeller shaft in marine propulsion shafting. Objective function is to minimize total mass of shafts and constraints are that torsional vibration stresses of shafts in marine propulsion shafting can not exceed the permissible torsional vibration stresses of the ship classification society. The computational results by the program were compared with those of conventional design technique.

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A Study on Optimum Shaft Alignment Analysis for VLCC (VLCC의 최적 축계정렬해석 연구)

  • Kim Hyu Chang;Kim Jun Gi
    • Special Issue of the Society of Naval Architects of Korea
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    • 2005.06a
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    • pp.134-137
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    • 2005
  • Recently, in VLCC, shafting system is stiffer due to large engine power whereas hull structure is more flexible due to scantling optimization, which can be suffered from alignment damage by incompatibility between shafting and hull, In this study, shafting system without stern tube forward bush was adapted for less sensitive system against external factors. Also, shaft alignment analysis was considered with hull deflection at various ship loading conditions and stern tube after bush of long journal bearing was evaluated by static squeezing pressure and dynamic oil film pressure with sloping control. Whirling vibration was also reviewed to avoid resonance with propeller blade order. So, reliable shafting design for VLCC could be achieved through optimized alignment analysis for the system without stern tube forward bush.

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