• 대한조선학회논문집
• /
• 제60권6호
• /
• pp.416-423
• /
• 2023

Recently, the design point of the propeller is gradually changing due to the demand for energy saving and environmental protection. Until recently, self-propulsion model tests were conducted using stock propellers and geometry information was provided to propeller designers, but the range of existing stock propellers did not keep up with the changing design points, and the range of series propellers required in the initial design was also insufficient. Future propeller performance requires high performance and eco-friendliness, and the need for expansion of series propellers has increased. In order to respond to future needs and provide a wide range of advantages in propeller design, KRISO manufactures about 100 series propellers and builds series data through a model tests. In this paper, the approach method for deriving the representative optimal shape to be applied to the 4-blade series propeller in the initial stage of series propeller development was summarized.

• 한국해양환경ㆍ에너지학회지
• /
• 제14권2호
• /
• pp.73-80
• /
• 2011

어선용 고효율 표준 프로펠러 개발에 대해 고찰해 보았다. 어선용 프로펠러의 경우 모형시험이나 이론해석을 통한 정도 높은 설계가 이루어지지 않고 시리즈 데이터(주로 MAU 시리즈)에 의존하여 초기설계 수준에 머무르고 있는 실정이다. 본 연구에서는 52톤 어선을 기준으로 개발되었으며 기존 MAU 형 프로펠러보다 성능이 우수한 프로펠러를 손쉽게 설계, 적용할 수 있는 NACA형 단면을 사용한 시리즈 프로펠러 자료를 제공하기위한 연구를 수행하였다. 또 한 기존의 복잡한 설계 방식 대신에, NACA형 프로펠러를 표준화하여 보다 편리하게 사용할 수 있도록 하였다. 향후 모형 시험을 통한 추진 성능 및 캐비테이션 성능 검증을 수행할 계획이다.

• Selected Papers of The Society of Naval Architects of Korea
• /
• 제1권1호
• /
• pp.76-90
• /
• 1993

A new propeller series is developed using the newly developed blade section (KH 18 section) which has better cavitation characteristics and higher lift-drag ratio at wade angle-of-attack range than a conventional section. The radial patch distribution of the new series propellers is variable stance they were designed adaptively to a typical wake distribution. Basic geometric particulars of the series propellers. such as chord length, thickness, skew and rake distributions, are determined on the basis of recent full scale propeller geometric data. The series is developed for propellers having 4 blades, and blade area ratios of 0.3, 0.45, 0.6 and 0.75. Mean pitch ratios are varied as 0.5, 0.6, 0.7, 0.95 and 1.1 for each blade area ratio. The new propeller series consists of 20 propellers and is named as the KD(KRISO-DAEWOO)-propeller series. Propeller open-water tests are performed at the towing tank, and cavitation observation tests and fluctuating pressure tests are carried out at the cavitation tunnel of KRISO. $B_{p}-\delta$ curves, which can be used to select the optimum propeller diameter at the preliminary design stage, are derived from a regression analysis of the propeller open-water test results. The KD-cavitation chart is derived from the cavitation observation test results by choosing the local maximum lift coefficient and the local cavitation number as parameters. The cavity extent predicted by the KD-cavitation chart would be more accurate compared to that by an existing cavitation charts, such as the Burrll's cavitation chart, since the former is derived from the cavitation observation test results in a typical ship's wake, while the lather is derived from the test results in a uniform flow.

• 대한조선학회논문집
• /
• 제49권5호
• /
• pp.416-424
• /
• 2012

The MAU series has been usually used for the fishing vessel's propeller, which has been improved in consideration of the efficiency as well as the cavitation point of view in Pusan National University. The high efficiency standard series propeller(KF series) has been applied to the design of 52ton class fishing vessel's propeller in the previous study. The experimental study for the performance of the design propellers called KF series for 52 ton class fishing vessel has been conducted with five cases in Korea Ocean Research & Development Institute towing tank. The model tests have been carried out at different pitch ratio and expanded area ratio in comparison with the standard propeller to make the series chart. The KF series chart and the formula for performance expression have been completed on the basis of the experiment result.

• International Journal of Naval Architecture and Ocean Engineering
• /
• 제9권3호
• /
• pp.246-255
• /
• 2017

The proposed design methodology represents a new approach to optimize the propeller-hull system simultaneously. In this paper, two objective functions are considered, the first objective function is Lifetime Fuel Consumption (LFC) and the other one is cost function including thrust, torque, open water and skew efficiencies. The variables of the propeller geometries (Z, EAR, P/D and D) and ship hull parameters (L/B, B/T, T and $C_B$) are considered to be optimized with cavitation, blades stress of propeller. The well-known evolutionary algorithm based on NSGA-II is employed to optimize a multi-objective problem, where the main propeller and hull dimensions are considered as design variables. The results are presented for a series 60 ship with B-series propeller. The results showed that the proposed method is an appropriate and effective approach for simultaneously propeller-hull system design and is able to minimize both of the objective functions significantly.

• International Journal of Aeronautical and Space Sciences
• /
• 제15권4호
• /
• pp.356-365
• /
• 2014

This paper is the second in a series and aims to build a high-fidelity mathematical model for a propeller-driven airplane using the propeller's aerodynamics and inertial models, as developed in the first paper. It focuses on aerodynamic models for the fuselage, the main wing, and the stabilizers under the influence of the wake trailed from the propeller. For this, application of the vortex lattice method is proposed to reflect the propeller's wake effect on those aerodynamic surfaces. By considering the maneuvering flight states and the flow field generated by the propeller wake, the induced velocity at any point on the aerodynamic surfaces can be computed for general flight conditions. Thus, strip theory is well suited to predict the distribution of air loads over wing components and the viscous flow effect can be duly considered using the 2D aerodynamic coefficients for the airfoils used in each wing. These approaches are implemented in building a high-fidelity mathematical model for a propeller-driven airplane. Flight dynamic analysis modules for the trim, linearization, and simulation analyses were developed using the proposed techniques. The flight test results for a series of maneuvering flights with a scaled model were used for comparison with those obtained using the flight dynamics analysis modules to validate the usefulness of the present approaches. The resulting good correlations between the two data sets demonstrate that the flight characteristics of the propeller-driven airplane can be analyzed effectively through the integrated framework with the propeller and airframe aerodynamic models proposed in this study.

• 대한조선학회논문집
• /
• 제28권2호
• /
• pp.52-68
• /
• 1991

캐비테이션 특성이 우수하고 넓은 받음각에서 양력-향력비가 큰 새로운 날개단면(KH18 단면)을 사용하여 체계적인 방법으로 기하학적 형상을 변화시켜 설계된 새로운 계열 프로펠러의 개발을 시도하였다. 새로운 계열 프로펠러의 형상을 설계함에 있어 기존의 계열 프로펠러와는 달리 선택된 반류분포의 회전방향 평균 반류분포를 입력자료로 하여 반경방향 부하분포와 코오드 방향 부하분포를 동일하게 유지하면서 피치 및 캠버의 형상을 결정하였다. 또한 코오드 길이, 두께, 스큐 및 레이크 분포와 같은 형상은 최근 실적선 프로펠러의 형상 특성을 정형화하여 선택되었기 때문에 초기설계시 설계된 형상이 최종 설계 프로펠러의 형상과 크게 다르지 않을 것으로 생각되어 초기성능을 보다 정확하게 추정할 수 있게 하였다. 설계된 계열 프로펠러는 날개수 4개인 프로펠러를 대상으로 날개 전개면적비 4개($A_{E}/A_{O}$=0.3, 0.45, 0.6, 0.75)에 대하여 각 전개면적비에서 평균피치비를 5개(P/D=0.5, 0.65, 0.8, 0.95, 1.1)로 변화시켜 총 20개의 프로펠러로 구성되었으며 KD-프로펠러 씨리즈(KRISO-DAEWOO Propeller Series)라 명명하였다. 설계된 계열 프로펠러들에 대하여 단독특성시험, 캐비테이션 관찰시험, 변동압력 계측시험을 수행하였다. 프로펠러 단독특성 시험결과의 회귀해석결과로 부터 $B_{P}-\delta$ 곡선을 도출하여 초기설계 단계에서 최적 프로펠러 직경등을 쉽게 결정할 수 있게 하였다. 기준으로 선택된 반류분포(2700TEU 콘테이너선의 반류) 후류에서 프로펠러 추력계수 및 캐비테이션 수를 체계적으로 변화시킨 상태에서 캐비테이션 관찰시험 및 변동압력계측시험을 수행하였다. 양력면이론에 의한 비정상 프로펠러 성능해석에 의해 계산된 최대 국부양력계수 ($C^{max}_{l,0.8R}$)와 국부캐비테이션 수(${\sigma}_0=\frac{p-p_v}{\frac{1}{2}{\rho}V^2_{0.8R}}$)를 기준으로 캐비테이션 관찰시험 결과를 정리하여 KD-캐비테이션 챠트를 도출하였다. 기존의 캐비테이션 챠트는 균일류중의 시험 결과를 정리하여 작성되었으나 KD-캐비테이션 챠트는 반류분포중에서 시험된 프로펠러 관찰시험 결과로 부터 도출되었으므로 초기설계 단계에서 보다 정확한 캐비테이션 발생량 추정이 가능하리라 예상된다.

• Journal of Ship and Ocean Technology
• /
• 제6권3호
• /
• pp.37-45
• /
• 2002

A series of detailed study was performed to identify the sources of the propeller blade failure and resolve the problem systematically, by use of the theoretical tools and by the direct measurement and observation in the full-scale sea trials. The selection of inexperienced propulsion control system with a reversible gear system is shown to cause the serious damage to the propeller blades in crash astern maneuver, when the rotational direction of the propeller is changed rapidly. Quasi-steady analysis for propeller blade strength using FEM code in bollard backing condition indicates that the safety factor should be order of 18∼20 to avoid the structural failure for the selected propeller geometry and reduction gear system.

• International Journal of Aeronautical and Space Sciences
• /
• 제15권4호
• /
• pp.345-355
• /
• 2014

This paper focuses on aerodynamic and inertial modeling of the propeller for its applications in flight dynamics analyses of a propeller-driven airplane. Unsteady aerodynamic and inertial loads generated by the propeller are formulated using the blade element method, where the local velocity and acceleration vectors for each blade element are obtained from exact kinematic relations for general maneuvering conditions. Vortex theory is applied to obtain the flow velocities induced by the propeller wake, which are used in the computation of the aerodynamic forces and moments generated by the propeller and other aerodynamic surfaces. The vortex lattice method is adopted to obtain the induced velocity over the wing and empennage components and the related influence coefficients are computed, taking into account the propeller induced velocities by tracing the wake trajectory trailing from each of the propeller blades. Aerodynamic forces and moments of the fuselage and other aerodynamic surfaces are computed by using the wind tunnel database and applying strip theory to incorporate viscous flow effects. The propeller models proposed in this paper are applied to predict isolated propeller performances under steady flight conditions. Trimmed level forward and turn flights are analyzed to investigate the effects of the propeller on the flight characteristics of a propeller-driven light-sports airplane. Flight test results for a series of maneuvering flights using a scaled model are employed to run the flight dynamic analysis program for the proposed propeller models. The simulations are compared with the flight test results to validate the usefulness of the approach. The resultant good correlations between the two data sets shows the propeller models proposed in this paper can predict flight characteristics with good accuracy.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2002년도 추계 학술대회논문집
• /
• pp.139-143
• /
• 2002

The purpose of this paper is to develop the CFD code to consider the viscous flow features of the marine propeller. The flow of the marine propeller has been numerically analyzed by using three dimensional viscous incompressible Navier-Stokes equation. The model used in this study is Screw B with 4 blades whose pitch ratio is 1 in Ka-4-55 screw series. The result of the analysis was compared with panel method.