• 제목/요약/키워드: Blade shape

검색결과 478건 처리시간 0.02초

수직축 소형 풍력터빈 성능 향상을 위한 로터 형상 개선에 대한 연구 (A Study on the Improvement of the Rotor Shape for Improving Performance of Small Wind Turbine with Vertical Axis)

  • 김찬종;김재운;백인수;김철진
    • 산업기술연구
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    • 제37권1호
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    • pp.37-40
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    • 2017
  • This study was carried out to improve the performance of a vertical-axis micro wind turbine. It is unique in that it has two identical generators on both sides of the main shaft. Also it has a C shape frame to fix the generators and the main shaft firmly and to provide a connection to a tower. Performance analysis of the wind turbine rotor was performed using Qblade, which is an analysis program for vertical axis wind turbines and freeware. Based on the analysis results, the blade airfoil, the chord length, and the rotor size were modified to improve the performance of the rotor. The modification was found to increase the performance of the wind turbine and to reach the targeted rated power.

전산유체역학을 활용한 가전 제품용 원심팬 블레이드의 단계별 형상 최적화 (MULTI STAGE SHAPE OPTIMIZATION OF CENTRIFUGAL FAN FOR HOME APPLIANCE USING CFD)

  • 김종수;강태곤
    • 한국전산유체공학회지
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    • 제21권3호
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    • pp.39-47
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    • 2016
  • We conducted a multi-stage optimization to secure the desired performance of a centrifugal fan for home appliance in an early stage of product development. In optimization, the static pressure at the outlet of the fan is chosen as an objective function that is to be maximized, providing the required flow rate at the operating point of the fan. The optimization procedure begins with parameters for an initial baseline fan design. The baseline design is optimized by using a commercial optimization package. Accordingly, the corresponding blade models with a set of geometrical parameters are generated. Flow through a fan is simulated by solving the Reynolds-averaged Navier-Stokes equations. A multi-stage optimization scheme is employed to determine the family of optimum values for the parameters, leading to the pressure increase at the outlet of the fan. To validate the numerically obtained optimal design parameters, we fabricated the three types of fans using rapid prototyping and assessed the performance using a fan tester. Experimental results show that the design parameters at each stage satisfy the goal of optimization. The multi-stage optimization process turned out to be a useful tool in the development of a centrifugal fan.

UV 임프린팅을 통한 프레넬 렌즈 제작 시 미세 복제 특성에 관한 연구 (Micro replication quality of Fresnel lens using UV imprinting process)

  • 임지석;김병욱;강신일
    • 정보저장시스템학회논문집
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    • 제6권1호
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    • pp.37-40
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    • 2010
  • Fresnel lens is a kind of refractive optical lens with various advantages. It has nearly flat shaped optical lens that has small mass. Fresnel lens has number of applications in the compact optical systems. Recently, demands of high quality Fresnel lens for small size optical systems such as illumination units, compact imaging systems, display units, information storage systems, optical detecting units had increased rapidly. Conventional manufacturing process of high quality Fresnel lens is direct machining. However, it is not suitable for mass production because of high cost and long cycle time. Replication method can provide cost effective mass production process. However, there are various issues about replication of Fresnel lens. Fresnel lens has number of sharp blade shape prism. In the replication process, this blade shape causes defects that can affect optical efficiency. In this study, replication processes; injection molding process and UV imprinting process, were developed and evaluated using Fresnel lens that has maximum pattern height of $250\;{\mu}m$ and aspect ratio of 1.5.

MDO 최적화 설계기법을 이용해 설계된 1단 축류형 압축기의 성능평가 (Performance Assessment of MDO Optimized 1-Stage Axial Compressor)

  • 강영석;박태춘;양수석;이세일;이동호
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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    • pp.397-400
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    • 2011
  • 소형 가스터빈 엔진에 장착 가능한 저압단 축류 압축기의 공력성능 및 구조적 안정성을 동시에 고려한 최적화 설계를 수행하였다. 근사모델을 구축하여 유전알고리즘을 이용하여 전역 최적화 해를 도출하였다. 최적 설계된 압축기의 동익단은 Hub쪽에서 날개의 부하가 커지되, Tip쪽에서 입사각이 0에 가깝게 설계되었다. 한편 동익의 형상은 허브쪽에서 사다리꼴 모양으로 수렴이 되어 구조적 안정성을 확보하도록 설계가 되었다. 최종적인 수치해석 결과 작동점에서 동익단의 효율은 87.6%이며 구조적 안정성을 나타내는 안전계수는 3이상을 확보하였다.

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Optimization of the Propeller Steady Performance Behind Wake Field

  • Lee, Wang-Soo;Choi, Young-Dal;Kim, Gun-Do;Moon, Il-Sung;Lee, Chang-Sup
    • Journal of Ship and Ocean Technology
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    • 제11권2호
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    • pp.10-25
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    • 2007
  • With the sharp increase of the oil price, the issue of the energy saving requires even higher propulsive efficiency of the propellers. Traditionally the propellers have been designed with the criteria such as that of Lerbs optimum based on the lifting line theory and the empirical formulae of Lerbs and van Manen giving relations of the wake pitch with the wake non-uniformity. With the aid of the high speed computer, it is now possible to apply the time-consuming iterative approaches for the solution of the lifting surface problems. In this paper we formulate the variational problem to optimize the efficiency of the propeller operating in the given ship wake using the lifting surface method. The variational formulation relating the spanwise circulation distribution with the propulsive efficiency to be maximized is however non-linear in circulation distribution functions, thus the iterative method is applied to the quasi-linearized equations. The blade shape design also requires the iterative procedures, because the shape of the blade which is represented by the lifting surface is unknown a priori. The numerical code was validated with the DTNSRDC propeller 4119 which is well-known to be optimum in uniform inflow condition. In addition existing (well-designed) commercial propellers were selected and compared with the results of the open water tests and the self-propulsion tests.

민수헬기 대상기종 로터 공력성능 및 소음 비교 (Comparisons of Rotor Performance and Noise between Candidate Light Civil Helicopters)

  • 정기훈;강희정;김도형;윤철용;김승호;박구환;이상기
    • 한국항공우주학회지
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    • 제41권9호
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    • pp.726-733
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    • 2013
  • 헬리콥터 로터 블레이드는 헬리콥터의 성능을 좌우하는 동시에 비행 시 주된 소음을 발생함에 따라 고성능, 저소음 특성이 요구되는 구상품이다. 국내 소형무장헬기 개발과 병행하여 개발될 민수헬기는 해외체계업체 보유 민수헬기를 기반으로한 국제공동 업그레이드 개발이 추진됨에 따라 해외체계업체 제시 대상기종의 로터 블레이드 성능파악이 매우 중요하다. 본 연구는 해외체계업체 제시 대상기종 블레이드의 성능분석을 통하여 최신 해외 블레이드 대비 성능파악 및 국내고유형상 블레이드 개발 가능성을 타진하는 것을 목적으로 수행되었다. 본 연구의 결과는 일차적으로 향후 민수헬기개발사업의 해외협상 및 국내 고유형상 블레이드 개발 시 목표 성능지표 등으로 활용될 수 있다.

잎이 강건하고 화색이 엷은 좀비비추 '청나래' 육성 (Cultivation of Hosta minor 'Cheongnarae' with Thick Leaves and Light-Colored Petals)

  • 오혜진;이종석;김진호;김상용;서강욱
    • 한국자원식물학회지
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    • 제34권1호
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    • pp.73-78
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    • 2021
  • '청나래'는 국립수목원(Korea National Arboretum)에서 2019년에 육성한 품종이다. 제주도에서 채집한 좀비비추(H. minor)를 모본으로, 외국에서 육성된 H. 'Krossa Regal'을 부본으로 인공 교배하여 종자를 채종하였다. 파종 후 얻은 개체 중 잎의 모양, 색깔 등의 형태적 특성에 차이를 보이는 계통을 우선 선발하였다. 이 중, 잎이 강건하고 화색이 연한 개체를 선발하여 영양번식과 재배를 반복하며 특성 고정 및 검정을 실시하였다. '청나래'는 대조품종인 H.'Black Hills'과 비교하여 잎이 두텁고 색이 진하며(RHS 137A) 잎자루(petiole)와 잎몸(leaf blade)이 만나는 부위에 날개가 있다. 잎몸 가장자리는 물결 모양이 뚜렷하고 화색은 흰색(White N155B)에 가깝다. 이와 같이 육성된 청나래는 분화 또는 정원용으로 활용이 가능하다.

제철소 소결냉각용 축류송풍기 출구 덕트 형상에 따른 내부유동특성 (Internal Flow Characteristics of a Steelworks Sintering Cooler by the Duct Shape of Cooler Fan Outlet)

  • 최영도;김경훈
    • 한국유체기계학회 논문집
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    • 제17권5호
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    • pp.72-77
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    • 2014
  • Because of overload working condition of sintering cooler, the cooler fan often suffers the break or damage of rotor blade and fixing shaft. Therefore, internal flow characteristics of a steelworks sintering cooler fan by the duct shape of the cooler fan outlet, such as duct outlet opening ratio, duct height and dividing wall shape on the duct outlet flow pattern are examined in detail. The results show that relatively short duct wall height and attachment of dividing wall shape improves flow patterns considerably.

역설계 방법을 적용한 사류펌프의 임펠러 및 디퓨저 설계 (Design of Impeller and Diffuser for Mixed Flow Pump with Inverse Design Method)

  • 이경용;최영석;김준호
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2009년도 하계학술발표대회 논문집
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    • pp.1322-1325
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    • 2009
  • The impeller and vane diffuser for the mixed flow pump(NS550) was designed by using meridional selection program and inverse design method. We decided the meridional shape of the impeller from the meridional design parameter, such as the specific speed and maximum diameter at the impeller exit. The meridional shape of vane diffuser was set from the impeller shape, distribution of cross sectional area and maximum diffuser diameter. The angle of impeller blade and diffuser vane was designed by using inverse design method. The predicted overall performance by using commercial CFD code(ANSYS CFX-11) shown good agreement with design goals.

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배관계 오리피스 하류에서 유동가속부식으로 인한 국소 유동 파라미터에 대한 조사 (Investigation of Local Flow Parameters Caused by Flow Acceleration Corrosion Downstream of an Orifice in a Piping System)

  • 김경훈;조연수;김형준
    • 설비공학논문집
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    • 제25권7호
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    • pp.377-385
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    • 2013
  • In this study, the performance of an impeller according to blade length and pitch angle was studied experimentally by building a variable pitch impeller while changing blade length to review the effect of blade length and pitch angle on a fan's performance. The pitch angle was changed in six steps from $20^{\circ}{\sim}45^{\circ}$ at intervals of $5^{\circ}$ while the blade lengths were changed to 90 mm, 100 mm, 110 mm and 120 mm with an identical airfoil shape while carrying out the experiment. The results are summarized as follows : The air flow per static pressure of axial fans increased linearly with increase of pitch angle, but the high static pressure showed a decrease at a pitch angle of $35^{\circ}$. The shaft power increased proportionally to the pitch angle at all blade lengths; the larger the pitch angle, the larger the measured increase of shaft power. This is because the drag at the fan's front increases with the pitch angle. In the axial fans considered in this research, the flow and incre.