• Journal of Mechanical Science and Technology
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• 제19권7호
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• pp.1478-1487
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• 2005

A small mixed-type turbine with a diameter of 19.9 mm has been substituted for a rotational part of pencil-type air tool. Usually, a vane-type rotor is applied to the rotational part of the air tool. However, the vane-type rotor has some problems, such as friction, abrasion, and necessity of accurate assembly etc.,. These problems make the life time of the vane-type air tool short, but air tools operated by mixed-type turbines are free of friction and abrasion because the turbine rotor dose not contact with the casing. Moreover, it is assembled easily because of no axis offset. These characteristics are merits for using air tools, but loss of power is inevitable on a non-contacting type rotor due to flow loss, tip clearance loss, and profile loss etc.,. In this study, four different rotors are tested, and their characteristics are investigated by measuring the specific output power. Additionally, optimum nozzle location against the rotor is studied. Output powers are obtained through measured pressure, temperature, torque, rotational speed, and flow rate. The experimental results obtained with four different rotors show that the rotor blade shape greatly influences to the performance, and the optimum nozzle location exists near the mid span of the rotor.

• 대한기계학회논문집B
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• 제33권12호
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• pp.1007-1013
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• 2009

The purposes of this study are to evaluate the power performance through CFD analysis and structural integrity through uni-directional FSI analysis in aerodynamic design and structure design of wind turbine blade. The blade was designed to generate the power of 2MW under the rated wind speed of 11 m/s, consisting of NACA 6 series, DU series and FFA series airfoil. The inside section of the blade was designed into D-spar structure and circular stiffener was placed to reinforce the structural strength in the part of hub. CFD analysis with the application of transitional turbulence model was performed to evaluate the power performance of blade according to the change of TSR and 2.024MW resulted under the condition of rated wind speed. TSR of 9 produced the maximum power coefficient and in this case, Cp was 0.494. This study applied uni-directional FSI analysis for more precise evaluation of structural integrity of blade, and the results of fiber failure, inter fiber failure and eigenvalue buckling analysis were evaluated, respectively. For the evaluation, Puck's failure criteria was applied and the result showed that fiber failure and inter fiber failure did not occur under every possible condition of the analysis. As a result, power performance and structural integrity of 2 MW blade designed in this study turned out to satisfy the initial design goals.

• 대한기계학회논문집A
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• 제35권5호
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• pp.575-582
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• 2011

클리닝 블레이드는 레이저 프린터 토너 카트리지에 장착된 감광드럼 표면의 잔류 토너를 제거하는 우레탄 재질의 고무부품이다. 기존에는 고무 블레이드의 클리닝 성능과 수명에 대한 다양한 연구들이 수행되었으나, 본 연구에서는 클리닝 성능과 부품간의 간섭에 대한 구속조건들을 모두 만족하면서 클리닝 블레이드에 발생하는 최대응력을 최소화 하는 클리닝 블레이드의 형상최적설계를 수행하였다. 상용 PIDO 툴인 PIAnO 를 이용하여 클리닝 블레이드의 구조해석절차를 통합하고 자동화하였으며, 최적설계를 위해 PIAnO 에서 제공하는 실험계획법과 근사화기법, 최적화 알고리즘을 사용하였다. 최적설계 결과, 초기 모델 대비 최대응력을 32.6% 감소 시킬 수 있는 최적의 설계안을 도출하였으며, 이를 통해 본 연구에서 수행한 최적설계 방법의 유효성을 확인할 수 있었다.

• 한국터널지하공간학회 논문집
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• 제23권6호
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• pp.423-438
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• 2021

모터 그레이더의 블레이드는 도로공사시 골재를 산포하고 평탄화하는 역할을 수행한다. 본 연구는 그레이더의 작업효율을 향상시키기 위하여 블레이드 부품의 설계개선 연구를 진행하였다. 블레이드와 골재 입자의 접촉, 절삭, 산포 과정을 모사하기 위하여 동해석 코드에 개별요소법을 도입하여 전산해석 모델을 수립하였다. 블레이드 설계인자를 4가지 선별한 후 작업 시나리오를 수립하였다. 실험계획의 직교배열을 통해 각 인자의 수준조합별 9개 모델에 대해 평탄화 작업에 대한 동해석을 수행하고, 각 설계인자의 영향도를 분석하였다. 이후 유의한 인자를 분산분석을 통해 선별하여 최적화기법으로 점진적 반응표면법을 적용하였다. 최종적으로 블레이드의 작업 효율성을 향상시킬 수 있도록 설계인자의 최적값을 제안하였다.

• 한국정밀공학회지
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• 제20권7호
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• pp.70-77
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• 2003

The centerless through-feed grinding is performed by passing the workpiece between the grinding wheel and the regulating wheel. So, the amount of removed material around the leading end, of the workpiece is always more than that around the trailing end until the leading end leaves the grinding wheel. Because of this, there are differences in diameters along the workpiece axis during grinding, and workpiece axis is not parallel to the grinding wheel axis and the contact lines between the workpiece and wheels. Thus the ground workpiece shows tapering error inherently. To eliminate this error, the workpiece axis must be kept to be parallel to the grinding wheel axis. And, the direction of the workpiece axis can be controlled by the work-rest blade. Therefore, the effects of work-rest blade inclination angle on the through-feed centerless ground part are investigated in this study. As a result, it is found that there is a positive inclination angle of the work-rest blade for minimizing the tapering error of a ground workpiece.

• 한국유체기계학회 논문집
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• 제14권2호
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• pp.5-10
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• 2011

The purpose of this study is to develop a software for the performance evaluation and blade design of a pitch-controlled HAWT using BEMT(Blade Element Momentum Theory) with Prandtl's tip loss. The HERACLES V2.0 software consist of three major part ; basic blade design, aerodynamic coefficient mapping and performance calculation including stall or pitch control option. A 1MW wind turbine blade was designed at the rated wind speed(12m/s) composing five different airfoils such as FFA-W-301, DU91-W250, DU93-W-210, NACA 63418 and NACA 63415 from hub to tip. The mechanical power predicted by BEMT at the rated wind speed is about 1.27MW. Also, CFD analysis was performed to confirm the validity of the BEMT results. The comparison results show good agreement about the error of 6.5% in rated mechanical power.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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• pp.464-468
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• 2003

A general program of three dimensional profile design of impellers for centrifugal/fixed-flow compressors is successfully commercialized using Bezier curves and quasi-3D flow analysis methods. Control points for meridional hub and shroud contours and blade camberline angles are arbitrarily changed to give smooth Bezier curves. With specified blade normal thicknesses, contructed geometry is instantly analyzed using flow analysis methods to be checked.

• 한국산림과학회지
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• 제71권1호
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• pp.82-89
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• 1985

수종간(樹種間), 집단간(集團間), 집단내개체간(集團內個體間)의 변이(變異)를 밝히기 위(爲)해 신갈나무 10개(個) 천연집단(天然集團)과 졸참나무 9개(個) 천연집단(天然集團)의 엽형질변이(葉形質變異)를 조사(調査)하였다. 엽신장(葉身長)/최대엽폭(最大葉幅), 엽신장(葉身長)/엽병장(葉柄長), 엽신장(葉身長)/엽맥수(葉脈數), 상(上)1/3엽폭(葉幅)/최대엽폭(最大葉幅), 상(上)1/3엽폭(葉幅)/하(下)1/3엽폭(葉幅)의 5개(個) 엽형지수(葉型指數)와 엽병장(葉柄長), 엽맥수(葉脈數)가 본(本) 연구(硏究)에 포함(包含)되었다. 졸참나무의 엽신장(葉身長)/엽병장(葉柄長)을 제외(除外)한 조사(調査)된 모든 엽형질변이(葉形質變異)는 집단간(集團間), 집단내개체간(集團內個體間)에 고도(高度)의 유의적(有意的)인 차이(差異)를 보였다. 신갈나무와 졸참나무 다같이 엽신장(葉身長)/최대엽폭(最大葉幅), 엽신장(葉身長)/엽병장(葉柄長), 엽신장(葉身長)/엽맥수(葉脈數)의 지수(指數)에서 남부집단(南部集團)과 북부집단간(北部集團間)에 다른 엽형(葉型)을 나타냈다. 그리고 북부집단(北部集團)의 엽형(葉型)은 신갈나무의 독특(獨特)한 특성(特性)들과 더 유사(類似)하고 남부집단(南部集團)은 졸참나무의 독특(獨特)한 특성(特性)을 더 많이 지니고 있었다. 집단내개체목간(集團內個體木間)에 변이(變異)는 엽신장(葉身長)/엽병장(葉柄長), 엽병장(葉柄長)에서 더욱 두드러지게 나타났고 우리나라 중부(中部)에 하는 속(屬)하는 계룡산집단내(鷄龍山集團內)에서 더욱 현저(顯著)했다.

• 한국유체기계학회 논문집
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• 제15권3호
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• pp.51-56
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• 2012

This study analyzed the influence of firing biogas on the performance and operation of a gas/steam turbine combined system. A reference gas/steam turbine combined system, designed with biogas fuel(57% volumetric methane) was set up and off-design simulation was made to investigate operating characteristics when a couple of operating schemes to mitigate turbine blade overheating were applied. Performance at base-load operation using each scheme was compared and part load operation using the variable inlet guide vane was analysed. Also, differences in operating characteristics and performance caused by changes in the methane content of biogas and ambient temperature were examined.

• 대한조선학회논문집
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• 제41권2호
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• pp.33-46
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• 2004

The cavitating noise of underwater propeller is considered numerically in this study. The main purpose of this research is to analyze these noise sources from marine propeller. The approach for investigation is a potential based panel method coupled with acoustic analogy. To predict propeller sheet cavitation noise, the blade surface cavity is considered as a single valued pulsating volume of vapor attached to the blade surface. The time dependent cavity volume data are used for noise prediction. Furthermore, we analyze hydrofoil cavitation bubble behavior and noise using Eulerian/Lagrangian approach. Through this study, we can analyze dominant noise source of marine propeller and provide a basis for proper noise control strategies.