• 한국추진공학회지
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• 제3권1호
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• pp.24-33
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• 1999

가스터빈 엔진의 성능예측과 진단을 위해 선형 및 비선형 가스경로 해석방법이 적용되었다. 염, 부식, 침식과 같은 물리적 손상을 탐지하기 위한 최적 계측변수를 구하기 위해 비선형 가스경로 해석을 이용하였다. 물리적 손상이 엔진성능에 미치는 영향을 연구하는데 전형적 산업용 가스터빈 엔진인 TB5000에 적용하였다. 선형 가스경로 해석과 비선형 가스경로 해석의 끈 오차 비교를 통해 최적의 계측변수가 정의될 수 있었다. 결과적으로, 선형 가스경로 해석방법은 선형화 모델의 가정에 의해 유도된 오차정도가 손상의 크기와 같은 정도가 되는 반면에 비선형 가스경로 해석방법은 Newton-Raphson 반복기법을 사용하여 독립변수와 종속변수의 비선형 관계를 충분한 정확성과 함께 풀 수 있다는 점을 알 수 있었다.

• Wind and Structures
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• 제31권3호
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• pp.217-227
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• 2020

Based on translation models, both Gaussian and non-Gaussian wind fields are generated using spectral representation method for investigating the influence of non-Gaussian characteristics and directivity effect of wind load on fatigue damage of wind turbine. Using the blade aerodynamic model and multi-body dynamics, dynamic responses are calculated. Using linear damage accumulation theory and linear crack propagation theory, crack initiation life and crack propagation life are discussed with consideration of the joint probability density distribution of the wind direction and mean wind speed in detail. The result shows that non-Gaussian characteristics of wind load have less influence on fatigue life of wind turbine in the area with smaller annual mean wind speeds. Whereas, the influence becomes significant with the increase of the annual mean wind speed. When the annual mean wind speeds are 7 m/s and 9 m/s at hub height of 90 m, the crack initiation lives under softening non-Gaussian wind decrease by 10% compared with Gaussian wind fields or at higher hub height. The study indicates that the consideration of the influence of softening non-Gaussian characteristics of wind inflows can significantly decrease the fatigue life, and, if neglected, it can result in non-conservative fatigue life estimates for the areas with higher annual mean wind speeds.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2018년도 추계학술대회
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• pp.59-60
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• 2018

진동수주형 파력발전장치는 수주, 터빈, 발전기 그리고 전력변환 장치 등이 연계된 복잡한 물리적인 특성을 나타낸다. 본 연구는 1/4 스케일의 모형시험을 통해 진동수주와 터빈의 물리적인 관계의 도출에 중점을 두고 있다. 진동수주실과 연성된 터빈의 공력특성은 오리피스를 활용하여 모사하였다. 진동수주실 성능평가에 핵심요소인 터빈효과는 오리피스를 통과하는 유속과 압력강하로 대표할 수 있다. 진동수주형 파력발전장치의 터빈효과는 모형시험에서 계측된 유속과 압력강하로부터 비선형적인 관계를 갖는 것을 확인하였다.

• 한국추진공학회지
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• 제5권1호
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• pp.69-75
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• 2001

터보프롭 엔진의 성능진단을 위한 선형 GPA(Gas Path Analysis) 및 비선형 GPA 프로그램을 개발하고 최적 계측 변수 선정을 위한 해석을 수행하였다. 엔진의 손상은 압축기 오염과 압축기 터빈 및 동력터빈의 부식이 동시에 발생하는 경우를 가정하였다. 먼저 비선형 GPA에서 반복기법에 대한 영향을 알아보기 위해 독립변수의 저하량을 등간격으로 나누어 반복 해석한 경우와 Newton-Raphson법을 이용하여 해석한 경우를 선형 GPA 해석 결과와 비교하였다. 해석 결과 비선형 GPA의 성능은 반복기법에 의해 많은 영향을 받음을 알 수 있었다. 다음 계측변수 수에 대한 영향을 알아보기 위해 계측변수를 6개, 8개, 10개로 달리하여 각각 선형 GPA 기법과 비선형 GPA 기법을 이용하여 해석을 수행한 후 RMS 오차를 비교하였다. 해석 결과 계측변수가 많으면 보다 정확한 진단 결과를 얻을 수 있으나 계측변수를 잘 선정한다면 보다 적은 계측변수로도 신뢰성 있는 결과를 얻을 수 있음을 확인하였다. 또한 비선형 GPA 기법을 이용한 경우의 RMS 오차가 선형 GPA 기법을 이용한 경우보다 적어 비선형 GPA 기법의 유용성을 알 수 있었다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 추계학술대회논문집
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• pp.256-263
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• 2008

The assumed modes method is developed to derive a set of linear differential equations describing the motion of a flexible wind turbine blade and to propose an approach to investigate the forced responses result from various wind excitations. In this work, we have adopted Euler beam theory and considered that the root of the blade is clamped at the rigid hub. And the aerodynamic parameters and forces are determined based on Blade Element Momentum (BEM) theory and quasi-steady airfoil aerodynamics. Numerical calculations show that this method gives good results and it can be used fur modeling and the forced vibration analysis including the coupling effect of wind-turbine blades, as well as turbo-machinery blades, aircraft propellers or helicopter rotor blades which may be considered as straight non-uniform beams with built-in pre-twist.

• Advances in aircraft and spacecraft science
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• 제4권1호
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• pp.37-52
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• 2017

Gas turbines operating in dusty or sandy environment polluted with micron-sized solid particles are highly prone to blade surface erosion damage in compressor stages and molten sand attack in the hot-sections of turbine stages. Commercial/Military fixed-wing aircraft engines and helicopter engines often have to operate over sandy terrains in the middle eastern countries or in volcanic zones; on the other hand gas turbines in marine applications are subjected to salt spray, while the coal-burning industrial power generation turbines are subjected to fly-ash. The presence of solid particles in the working fluid medium has an adverse effect on the durability of these engines as well as performance. Typical turbine blade damages include blade coating wear, sand glazing, Calcia-Magnesia-Alumina-Silicate (CMAS) attack, oxidation, plugged cooling holes, all of which can cause rapid performance deterioration including loss of aircraft. The focus of this research work is to simulate particle-surface kinetic interaction on typical turbomachinery material targets using non-linear dynamic impact analysis. The objective of this research is to understand the interfacial kinetic behaviors that can provide insights into the physics of particle interactions and to enable leap ahead technologies in material choices and to develop sand-phobic thermal barrier coatings for turbine blades. This paper outlines the research efforts at the U.S Army Research Laboratory to come up with novel turbine blade multifunctional protective coatings that are sand-phobic, sand impact wear resistant, as well as have very low thermal conductivity for improved performance of future gas turbine engines. The research scope includes development of protective coatings for both nickel-based super alloys and ceramic matrix composites.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 추계학술대회논문집
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• pp.270-275
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• 2008

In this study, computer applied engineering (CAE) techniques are full? used to conduct structural and dynamic analyses of a huge composite rotor blade. Computational fluid dynamics is used to predict aerodynamic load of the rotating wind-turbine blade model. Static and dynamic structural analyses are conducted based on the non-linear finite element method for composite laminates and multi-body dynamic simulation tools. Various numerical results for aerodynamic load, dynamic analyses are presented and characteristics of structural behaviors are investigated herein.

• 전기학회논문지
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• 제62권10호
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• pp.1383-1389
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• 2013

There were telecommunication noise and malfunctions of the electronic devices occurred over a wide area due to the high harmonic voltage and/or current levels of the Back-to-back converter in the DFIG wind power system even though the magnitude of all harmonics is within the international standards. The triangular carrier signals of the PWM used in the power converter system is related to the telecommunication noise because they are in the range of audible frequencies and amplified by a variety of the standing waves that were excited by harmonic voltage sources in the weak grid system such as a long distance distribution transmission lines. This paper describes the characteristics of the harmonics in the wind turbine-generator, numerical analysis and simulation of the harmonics resonance phenomena in the distribution lines as well as measuring induced voltage of the telecommunication lines in parallel with power lines in order to verify the root cause of the telecommunication noise. These noise problems can occur in a wind turbine power system with a non-linear converter at any time, as well as photovoltaic power system. So, the preliminary review of suitable filter devices and switching frequencies of the PWM have to be required by considering the stability of the controller at the design stage but as part of the measures the effect of the telecommunication cable shields was analyzed by comparing the measured data between multi-conductor with/without shields so as to attenuate the sources of the harmonics voltage induced into the telecommunication lines and to apply the most cost-effective measures in the field.