• 제목/요약/키워드: Blade shape

검색결과 478건 처리시간 0.032초

Influence of guide vane shape on the performance and internal flow of a cross flow wind turbine

  • Son, Sung-Woo;Singh, Patrick Mark;Choi, Young-Do
    • Journal of Advanced Marine Engineering and Technology
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    • 제37권2호
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    • pp.163-169
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    • 2013
  • In order to make the vertical-axis cross flow wind turbine commercially feasible, a guide vane is adopted and the effect of the guide vane shape is examined in order to improve the wind turbine performance. CFD analysis on the performance and internal flow of the turbine is carried out for the wind turbine model. The result shows that when the guide nozzle is installed, almost over two times of power coefficient are achieved in comparison with the case of no guide nozzle installation. The guide nozzle acts as a role of suppressing the flow resistance at the blade passage, which is found when the guide nozzle is installed. Moreover, in this study, two kinds of the guide vane with a straight type and a curved type are adopted and compared. The curved guide vane nozzle produces higher power coefficient in comparison with that of straight guide vane nozzle.

Hydraulic performance and flow resistance tests of various hydraulic parts for optimal design of a reactor coolant pump for a small modular reactor

  • Byeonggeon Bae;Jaeho Jung;Je Yong Yu
    • Nuclear Engineering and Technology
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    • 제55권3호
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    • pp.1181-1190
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    • 2023
  • Hydraulic performance and flow resistance tests were performed to confirm the main parameters of the hydraulic instrumentation that can affect the pump performance of the reactor coolant pump. The flow resistance test offers important experimental data, which are necessary to predict the behavior of the primary coolant when the circulation of the reactor coolant pump is stopped. Moreover, the shape of the hydraulic section of the pump, which was considered in the test, was prepared to compare the mixed-flow- and axial-flow-type models, the difference in the number of blades of the impeller and diffuser, the difference in the shape of the impeller blade and its thickness, and the effect of coating at the suction bell. Additionally, five models of the hydraulic part were manufactured for the experiments. In this study, the differences in performance owing to the design factors were confirmed through the experimental results.

500W 급 다리우스형 풍력발전기의 최적설계를 위한 수치적 연구 (Numerical study to Determine Optimal Design of 500W Darrieus-type Vertical Axis Wind Turbine)

  • 이영태;임희창
    • 대한기계학회논문집B
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    • 제39권8호
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    • pp.693-702
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    • 2015
  • 본 논문은 NACA 익형의 블레이드를 가지는 다리우스 수직축 풍력발전기(VAWT)의 성능특성에 대한 연구이다. 다양한 설계변수를 이용한 다리우스 VAWT 의 최적 형상을 예측하기 위해서 블레이드 근처에서 나타나는 공력특성 및 박리유동, 유동과 블레이드 간의 상호작용, 이로 인해 유도되는 토크 및 출력특성 등을 분석하였다. 블레이드의 최적 형상 설계 및 주변 유동과의 상호작용 특성을 보기 위하여 다양한 인자들 (즉, 코드길이, 로터직경, 피치각, 블레이드의 두께비 및 비틀림각 등)을 고려하였다. 본 연구에서 연구결과로는 TSR 가 낮은 영역에서는 솔리디티가 큰 로터가 높은 출력계수를 가지는 반면, TSR 이 높은 영역에서는 솔리디티가 작은 로터가 높은 출력계수를 가진다. 블레이드의 익형이 안쪽으로 향하는 피치각은 $-2^{\circ}$와 비틀림각이 $0^{\circ}$ 일 때, 다리우스형 VAWT 가 최대 출력을 발생하였다.

1.2MW급 산업용 가스터빈 원심압축기 개발(1)- 공력설계해석 - (Development of Centrifugal Compressors in an 1.2MW Industrial Gas Turbine(I)-Aerodynamic Design and Analysis-)

  • 조규식;이헌석;손정락
    • 대한기계학회논문집B
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    • 제20권8호
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    • pp.2707-2720
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    • 1996
  • The aerodynamic design of the two-stages of centrifugal compressors in an 1.2MW industrial gas turbine is completed with the application of numerical analyses. The final shape of an intake, the axial guide vanes and a return channel is determined using several interactions between design and two-dimensional turbulent flow analysis, focused on the minimum loss of internal flows. The one-dimensional turbulent flow analysis, focused on the minimum loss of internal flows. The one-dimensional design and prediction of aerodynamic performances for the compressors are performed by two different methods; one is a method with conventional loss models, and the other a method with the two-zone model. The combination methods of the Betzier curves generate three-dimensional geometric shapes of impeller blades which are to be checked with a careful change of aerodynamic blade loadings. The impeller design is finally completed by the applications of three-dimensional compressible turbulent flow solvers, and the effect of minor change of design of the second-stage channel diffuser is also studied. All the aerodynamic design results are soon to the verified by component performance tests of prototype centrifugal compressors.

Analysis of Aerodynamic Performance in an Annular Compressor Bowed Cascade with Large Camber Angles

  • Chen, Shaowen;Chen, Fu
    • International Journal of Fluid Machinery and Systems
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    • 제2권1호
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    • pp.13-20
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    • 2009
  • The effects of positively bowed blade on the aerodynamic performance of annular compressor cascades with large camber angle were experimentally investigated under different incidences. The distributions of the exit total pressure loss and secondary flow vectors of compressor cascades were analyzed. The static pressure was measured by tapping on the cascade surfaces, and the ink-trace flow visualizations were conducted. The results show that the value of the optimum bowed angle and optimum bowed height decrease because of the increased losses at the mid-span with the increase of the caber angle. The C-shape static pressure distribution along the radial direction exists on the suction surface of the straight cascade with large r camber angles. When bowed blade is applied, the larger bowed angle and larger bowed height will further enhance the accumulation of the low-energy fluid at the mid-span, thus deteriorate the flow behavior. Under $60^{\circ}$ camber angle, flow behavior near the end-wall region of some bowed cascades even deteriorates instead of improving because the blockage of the separated flow near the mid-span keeps the low-energy fluid near the end-walls from moving towards the mid-span region, and as a result, a rapid augmentation of the total loss is easy to take place under large bowed angle. With the increase of camber angle, the choice range of bowed angle corresponding to the best performance in different incidences become narrower.

치수효과를 고려한 횡류홴의 작동특성연구 (A Study on the Operational Characteristic with the Scale Effect of the Cross-Flow Fan)

  • 김형섭;김윤제
    • 한국유체기계학회 논문집
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    • 제8권3호
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    • pp.26-32
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    • 2005
  • One of noticeable features in the cross flow fan is that a working fluid passes through impeller blade twice without distinction between the inlet and exit angles. Also, it does produce higher circumferential velocity than other types of blade at the same flow rate in accordance with the application of the forward curved shape. However, a design theory for the cross-flow fall has not yet been formed owing to an eccentric vortex, which is the remarkable characteristics, occurred in a cross-flow fan. Furthermore, the eccentric vortex, which is difficult to control the size and position, is the important cause of performance decrease. In this study, experiments we carried out to estimate the similarity of the cross-flow fan with various scales and rotational velocity changes. Pressure coefficients to flow coefficients with various scales of the cross-flow fan are plotted to the application of the general similarity law of the turbomachinery in the cross-flow fan with Archimedes spiral, which is the important factor having an effect on it.

곡관부 열전달 성능 강화를 위한 에어포일형 가이드 베인의 형상 최적설계 (SHAPE OPTIMIZATION OF THE AIRFOIL-GUIDE VANES IN THE TURNING REGION FOR A ROTATING TWO-PASS CHANNEL)

  • 문미애;김광용
    • 한국전산유체공학회지
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    • 제17권2호
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    • pp.1-10
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    • 2012
  • This paper presents the numerical simulation results of heat transfer and friction loss for a rotating two-pass duct with the airfoil-guide vanes in the turning region. The Kriging model is used as an optimization technique with Reynolds-averaged Navier-Stokes analysis of flow field and heat transfer with shear stress transport turbulent model. To improve the heat transfer performance, angle and location of the airfoil-guide vanes have been selected as design variables. The optimization problem has been defined as a minimization of the objective function, which is defined as a linear combination of heat transfer related term and friction loss related term with a weight factor. The airfoil-guide vanes in the turning region keep the high level of heat transfer while the friction loss has a low value. By comparing the presence or absence of airfoil-guide vanes, it is shown that the airfoil-guide vanes exhibited the best heat transfer performance to improve the blade cooling except the first passage.

10 kW급 수평축 풍력 터빈 로터 블레이드의 공력 설계 (Aerodynamic Design of 10 kW-level HAWT Rotor Blades)

  • 장세명;이장호
    • 한국항공우주학회지
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    • 제35권10호
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    • pp.884-890
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    • 2007
  • 10 kW급 수평축 풍력 터빈의 로터를 개발하기 위해 블레이드의 공력 설계 절차를 체계적으로 연구하고 실행하였다. 운동량 이론과 깃 요소법에 근거한 역 설계 방법을 확립하고, 이를 이용하여 주어진 공력 분포에 따른 근사 최적 형상을 설계하였다. 설계된 형상은 공군사관학교의 풍동에서 검증되었고, 본 설계를 통하여 실제로 제작된 로터로부터 실측 데이터를 취득하여 비교하였다. 본 연구를 통하여 저자들은 풍력 터빈 블레이드의 설계 방법에 대한 체계적 기술을 축적하고, 나아가 같은 방법을 중대형 시스템으로 확장하기 위한 기술적 노하우를 취득하였다.

층류화염 유동속도 측정을 위한 modulated LII 기법 (Modulated LII technique for the Measurement of Flow Velocity in Laminar Flames)

  • 이원남;이정수;남연우
    • 한국연소학회지
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    • 제11권3호
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    • pp.36-43
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    • 2006
  • The modulated LII technique has been suggested for the measurement of axial velocity profiles of laminar diffusion flames. The theoretical background is explained based on the blackbody radiation and LII signal. Experimentally, soot particles in ethylene diffusion flames are heated by a modulated Ar-ion laser beam. LII signals and their phase angles are measured using a lock-in amplifier at the different flame heights and the axial flow velocities are obtained from the measured phase angle delay informations. The measured velocities are similar to those from LDV measurements under the same operating conditions. The effects of laser power, LII signal wavelength, and modulation frequencies are not sensitive to the velocity measurement. However, the choice of an optical chopper blade type could affect the measurement result. The use of a 6/5 chopper blade showed the better result that is. possibly due to the square shape of modulated laser beam. This study successfully demonstrated that axial flow velocities of laminar diffusion flames can be measured by a new technique utilizing LII signal, which does not need particle seeding unlikely to LDV or PIV techniques.

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부여군 고란초의 생육지 환경조건과 분포 (Distribution and Habitat Condition of Crypsinus hastatus in Buyeogun)

  • 송홍선;김성민
    • 한국약용작물학회지
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    • 제24권1호
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    • pp.27-30
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    • 2016
  • Background : This text was conducted to evaluate the distribution, shape characteristics and habitat condition of Crypsinus hastatus in Buyeo Korea. Methods and Results : In Buyeo, Crypsinus hastatus was distributed at an altitude of 31.2 m, a slope of 82.5% and a distance from river water of 27.2 m. The leaf blade was oblong, 2.7 cm long, 1.2 cm wide with a petiole length of 2.3 cm. The total population comprised 2,100 individuals, with the highest proportion being individuals with a leaf blade of length 0.5 - 1 cm. The temperature and light intensity of the growth point were lower, but the humidity higher, than that of growth around. The chemical properties of the soil were as follows: pH 4.42, organic matter 77.99 g/kg, electrical conductivity 0.50 dS/m, nitrate nitrogen 20.50 mg/kg and available phosphate 165.7 mg/kg. Exchangeable cation content of potassium, magnesium, sodium and calcium was 0.35, 0.70, 0.09 and $2.04cmol^+/kg$, respectively. Conclusions : In Buyeo, Crypsinus hastatus was distributed in $5.3m^2$ area of Nakhwaam, Naeseongri and Jeongamri. However, the population of the medicinal resources seemed to decrease owing to the poor environmental conditions of the habitat.