• 한국자기학회지
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• 제14권6호
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• pp.207-212
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• 2004

전자기학의 분야에서 와전류를 이용한 응용 분야는 매우 다양하다. 예를 들면, 핵을 이용한 원자력 발전소의 증기 발생 튜브 또는 비행기의 엔진이나 날개 부분의 결함 등을 자기적 특성을 이용하여 비파괴 검사를 하는 등의 일이다. 와전류의 특성을 결정짓는 가장 중요한 인자 중 하나가 바로 센서 측정 거리 (lift-off)인데 이것은 와전류를 측정한 센서와 피검사 물체간의 물리적인 공간거리를 뜻한다. 이 인자는 와전류 신호의 특성을 정확하게 분석해내는데 매우 중요함에도 불구하고 실제 필드에서는 모든 경우마다 그 정확한 값을 측정해내기가 힘들 뿐더러 일정한 거리를 상시 유지 하기도 어렵다. 따라서 자기적 신호의 하나인 와전류로 하여금 다양한 상황에서의 lift-off로 변화에도 영향을 받지 않고 일정한 특성을 유지하게끔 해주는 기술이 필요하다. 이 논문은 다양한 lift-off로부터 얻어진 와전류를 보상하여 일정한 성질을 유지하도록 하는 기법을 설명하고 있다. 다양한 lift-off로 부터 얻어진 와전류들은 신호 획득 거리가 0인 이상적 상태의 신호들로 보상 변환 되어 다음 단계인 피검사 시료상의 결함 또는 흠집의 물성이나 특성 파악에 계속해서 쓰이게 된다.

• 한국전산유체공학회지
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• 제16권4호
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• pp.47-54
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• 2011

A rotating propeller of turboprop aircraft gives much effect on the aerodynamic characteristics of wing such as lift, moment and stall. Specially propeller effect on the wing surface is much more dominant when aircrafts are in landing or take-off conditions. In the present paper, three dimensional Navier-Stokes simulations for the interaction of propeller and wing were carried out for medium sized turboprop aircraft. For rotating propeller, unsteady sliding mesh method was used to simulate a relative motion between moving and static bodies. For the power effect analysis in landing and take off configurations, double slotted flap was also considered and the aerodynamic characteristics were investigated. It was shown that the propeller slipstream enhanced the lift slope including maximum lift by eliminating local flow separation region and this enhancement was more dominant with high lift device.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2011년 춘계학술대회논문집
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• pp.202-205
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• 2011

A rotating propeller of turboprop aircraft gives much effect on the aerodynamic characteristics of wing such as lift, moment and stall. Specially, a rotating propeller changes the lift and moment characteristics when aircrafts are in landing or take-off condition. In the present paper, 3-dimensional Navier-Stokes simulations for the interaction of propeller and wing were carried out. For rotating propeller, unsteady sliding mesh method was used to simulate a relative motion. For the power effect analysis in landing and take off configurations, double slotted flap was also considered and the aerodynamic characteristics were investigated. It was shown that the propeller slipstream enhanced the lift slope including maximum lift and this enhancement was more dominant with high lift device.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2001년도 추계학술대회 논문집 전기기기 및 에너지변환시스템부문
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• pp.51-53
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• 2001

Permanent Magnet DC Motors are widely used in Automotive parts because they have cheap price, simple structure and high torque-speed ratio. But the motor in automotive parts is required high quality, complex function and lower price than before. This paper deals with design of controller for safety function that body trap on the automotive window. The algorithm of controller can adapt variety conditions with temperature, electrical, driving, etc.

• Journal of Biosystems Engineering
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• 제8권2호
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• pp.1-10
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• 1983

The resulting characteristics of vibrations show different patterns for the various oscillating mechanisms. These vibrations causes troublesome operation problems for the operators and sometimes for the machines. Furthermore, in some cases the practical usage of this oscillating mechanism is constrained by its mechanical conditions. In this study, a balanced oscillating tillage tool with triple blades having different acting area was designed. The horizontal and vertical oscillating accelerations and draft power requirement due to the various travel speeds, lift angles, amplitudes and oscillating frequencies were investigated in a laboratory soil bin with a soil having invariable properties. The results obtained are summarized as follows: 1. Overall, the horizontal acceleration decreased as the oscillating frequency and amplitude decreased. But the increase in travel speed caused the decrease horizontal acceleration. The blade with the lift angle of $30^{\circ}$ exhibited the lowest value of horizontal acceleration among the blades tested. 2. For the vertical acceleration, the fluctuating trend of oscillating acceleration was similar to the trend of the horizontal acceleration. 3. The draft power requirement decreased as the amplitude and oscillating frequency increased. But the increase in travel speed caused the increase in draft power requirement. The blade with the lift angle of $10^{\circ}$ showed the lowest value of draft power requirement among the blades tested.

• Journal of Power Electronics
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• 제11권5호
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• pp.639-654
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• 2011

This paper presents a Current Distribution Control design for Paralleled Positive Output Elementary Super Lift Luo Converters (PPOESLLCs) operated in Continuous Conduction Mode using a Sliding Mode Controller (SMC). Manipulating the higher current requirement of the load through the paralleling of POESLLCs, results in a current inequality. This is mainly due to dissimilarities in the power semiconductor switches and circuit components used in POESLLCs, which may lead to converter failures. In order to balance the proper load current sharing and the load voltage regulation of PPOESLLCs, a SMC is developed. The SMC is designed for the inherently variable-structured of POESLLCs by using the state-space average based model. The static and dynamic performance of the developed controller with PPOESLLCs is validated for its robustness to perform over a wide range of operating conditions through both a laboratory prototype and MatLab/Simulink models, which are compared with a Proportional-Integral (PI) controller. Theoretical analysis, simulation and experimental results are presented to demonstrate the feasibility of the developed SMC along with the complete design procedure.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2009년도 추계학술대회 논문집
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• pp.615-616
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• 2009

• 한국산업융합학회 논문집
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• 제2권2호
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• pp.173-180
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• 1999

When Automobile runs high velocity, it causes sleepy velocity profile then that generates lift force and drag force. Lift force reduce tire friction force. Drag force increase consumed power. For improve automobile performance, reduction of Lift force and Drag force was seriously considered. It measured experimently using wind tunnel, numerically using numerical analysis. Finite difference method is using difference equation and simplifed mesh. This method require less calculation time and computer power than other method.

• 한국항공우주학회지
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• 제40권1호
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• pp.12-22
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• 2012

샤프트각이 감소하며 비행 속도가 증가하는 자동회전 상태의 로터에 대한 성능 변화를 해석하였다. BO-105 헬리콥터의 로터에 비틀림이 없는 NACA 0012 단면을 가지는 깃을 해석하였고 변수에 대한 자동회전의 영역을 구하기 위해 과도모사법(TSM)이 사용되었다. 고속 비행에서 압축성 효과를 모사하기 위해 압축성 Navier-Stokes 솔버로 해석된 2차원 공력 데이터가 사용되었으며 유도 속도장을 모사하기 위해 Pitt/Peters의 유도속도 이론이 사용되었다. TSM으로 구해진 정상 자동회전 상태에 대하여 추력계수와 양력계수, 양항비를 계산하였으며 로터의 양력과 동력을 구하여 BO-105 헬리콥터와 비교하였다. 복합 항공기의 개념을 도입할 때 자동회전하는 로터와 날개의 양력 및 동력 분담률을 고찰하였다.

• 한국군사과학기술학회지
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• 제23권4호
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• pp.311-318
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• 2020

This study investigates the performance and blade airloads for a rigid coaxial rotor of high-speed compound unmanned rotorcrafts. The present compound unmanned rotorcraft uses not only a rigid coaxial rotor, but also wings and propellers for high-speed flights. For the rigid coaxial rotor in this work, CAMRAD II, a rotorcraft comprehensive analysis code, is used to study the performance at a flight speed of up to 250 knots and blade section lift forces at 230 knots. As the flight speed increases, the rotor power decreases; however, the power of propellers increases to overcome the drag force of a rotorcraft in high-speed flight. The effective lift-to-drag ratio of a rotor has the maximum value of about 11.6 which is much higher than the value of the conventional helicopter. The blade section lift forces of the upper and lower rotors at 230 knots show the similar variation trends for one rotor revolution, and the impulses because of the aerodynamic interaction between both rotors are observed.