• 제목/요약/키워드: Blade-rates

검색결과 97건 처리시간 0.022초

유량에 따른 축류홴의 익단누설와류 특성 (Flow Characteristics of a Tip Leakage Vortex at Different Flow Rates in an Axial Flow Fan)

  • 장춘만;김광용
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.1383-1388
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    • 2004
  • The flow characteristics in the blade passage of a low speed axial flow fan have been investigated by experimental analysis using a rotating hot-wire sensor for design and off-design operating conditions. The results show that the tip leakage vortex is moved upstream when flow rate is decreased, thus disturbing the formation of wake flow near the rotor tip. The tip leakage vortex interfaces with blade pressure surface, and results in high velocity fluctuation near the pressure surface. From the relative velocity distributions near the rotor tip, large axial velocity decay is observed at near stall condition, which results in large blockage compared to that at the design condition. Througout the flow measurements using a quasi-orthogonal measuring points to the tip leakage vortex, it is noted that the radial position of the tip leakage vortex is distributed between 94 and 96 percent span for all flow conditions. High spectrum density due to the large fluctuation of the tip leakage vortex is observed near the blade suction surface below the frequency of 1000 Hz at near stall condition.

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축류 회전차 익말단 틈새유동에 대한 수치해석 (III) - 회전차 익말단의 누설손실과 효율저하에 대한 평가 - (Numerical Analysis on the Blade Tip Clearance Flow in the Axial Rotor (III) - Evaluation of Tip Leakage Loss and Reduction of Efficiency near Blade Tip Clearance Region of a Rotor -)

  • 노수혁;조강래
    • 대한기계학회논문집B
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    • 제23권9호
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    • pp.1113-1120
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    • 1999
  • Leakage vortices fonned near the blade tip cause an increase of total pressure loss near the casing endwall region and as a result, the efficiency of rotor decreases. The reduction of rotor efficiency is related to the size of tip clearance. In this study, the three-dimensional flow fields in an axial flow rotor were calculated with varying tip clearance under various flow rates, and the numerical results were compared with experimental ones. The effects of tip clearance and the of attack on the leakage vortex and overall performance, and the los9 distributions were investigated through numerical calculations. In this study, tip leakage flow rate and total pressure loss due to the tip clearance were evaluated using numerical results and approximate equations were presented to evaluate the reduction of rotor efficiency due to the tip leakage flow.

초음속 터빈의 로터 블레이드 스윕 효과에 대한 수치적 연구 (A Numerical Study of Blade Sweep Effect in Supersonic Turbine Rotor)

  • 정수인;정은환;김귀순
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.830-834
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    • 2011
  • 본 연구에서는 액체로켓엔진의 터보펌프용 초음속 터빈 로터 블레이드에 스윕 각도 ${\pm}15^{\circ}$를 적용하여 전방스윕(FSW), 후방스윕(BSW)모델의 유동형태 및 성능을 기준모델(NSW)과 비교하여 스윕 적용의 효과를 살펴보았다. 3차원 Navier-Stokes 유동해석에는 상용 코드인 FLUENT 6.3 Parallel을 사용하였다. BSW 모델은 기준 모델(NSW)에 비해 팁 간극으로 빠져나가는 누설 손실량을 줄이는데 효과가 있었고 정효율 증가에도 영향을 미쳤다.

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유량에 따른 축류홴의 익단누설와류 및 후류 특성 (Flow Characteristics of Wake Flow with Relation to a Tip Leakage Vortex at Different Flow Rates in an Axial Flow Fan)

  • 김광용;장춘만
    • 대한기계학회논문집B
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    • 제29권3호
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    • pp.322-329
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    • 2005
  • The flow characteristics in the blade passage and in the wake region of a low speed axial flow fan have been investigated by experimental analysis using a rotating hot-wire sensor for design and off-design operating conditions. The results show that the tip leakage vortex is moved upstream when flow rate is decreased, thus disturbing the formation of wake flow near the rotor tip. The tip leakage vortex interfaces with blade pressure surface, and results in high velocity fluctuation near the pressure surface. From axial velocity distributions downstream of the fan rotor, large axial velocity decay near the rotor tip is observed at near stall condition, which results in large blockage compared to that at the design condition. Although the wake flow downstream of the rotor blade is clearly measured at all operating conditions, the trough of the high velocity fluctuation due to Karmann vortex street in the wake flow is mainly observed at a higher flow condition than the design flow rate.

Development of Automatic Chicken Cutting Machine

  • Woo, Duk Gam;Kim, Yeong Jin;Lim, Hack kyu;Kim, Tae Han
    • Journal of Biosystems Engineering
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    • 제43권4호
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    • pp.386-393
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    • 2018
  • Purpose: Chicken cutting is done manually, which is inefficient, unhygienic, and carries a high accident risk during processing. This study develops and evaluates an automatic chicken cutting machine that suits small-scale workplaces. Methods: This study developed an automatic chicken cutting machine equipped with four traverse blades and two longitudinal blades. An experiment was conducted with various blade rotating speeds and tray feed rates to evaluate the machine's performance. The chicken loss rate and chicken piece weights were measured to calculate the coefficient of variation (CV), thereby determining processing uniformity. Results: The optimal cutting conditions with the smallest chicken loss rate were 0.05 m/s tray feed speed and 18.8 m/s and 16.4 m/s for the traverse and longitudinal blades, respectively. The processing ran at 55.3 chickens per hour and the chicken pieces were more uniform when using the device than for hand-work processed pieces. Conclusions: The loss rate increased in proportion to the cutting-blade rotation speed due to the high cutting rate in meat. The loss rate also increased as the tray feed speed slowed because the cutting blade pushed the chicken meat. The tray feed speed should be increased to improve the amount processed per hour.

A comparison of the performance characteristics of large 2 MW and 3 MW wind turbines on existing onshore wind farms

  • Bilgili, Mehmet;Ekinci, Firat;Demirdelen, Tugce
    • Wind and Structures
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    • 제32권2호
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    • pp.81-87
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    • 2021
  • The aim of the current study is to compare the performance of large 2 MW and 3 MW wind turbines operating on existing onshore wind farms using Blade Element Momentum (BEM) theory and Angular Momentum (AM) theory and illustrate the performance characteristic curves of the turbines as a function of wind speed (U∞). To achieve this, the measurement data obtained from two different Wind Energy Power Plants (WEPPs) located in the Hatay region of Turkey was used. Two different horizontal-axis wind turbines with capacities of 2 MW and 3 MW were selected for evaluation and comparison. The hub-height wind speed (UD), turbine power output (P), atmospheric air temperature (Tatm) and turbine rotational speed (Ω) data were used in the evaluation of the turbine performance characteristics. Curves of turbine power output (P), axial flow induction factor (a), turbine rotational speed (Ω), turbine power coefficient (CP), blade tip speed ratio (λ), thrust force coefficient (CT) and thrust force (T) as a function of U∞ were obtained for the 2 MW and 3 MW wind turbines and these characteristic curves were compared. Results revealed that, for the same wind speed conditions, the higher-capacity wind turbine (3 MW) was operating at higher turbine power coefficient rates, while rotating at lower rotational speed ratios than the lower-capacity wind turbine (2 MW).

냉각홀 형상 변화에 바른 원형봉 선단의 막냉각 특성 연구 (A Study of Film Cooling of a Cylindrical Leading Edge with Shaped Injection Holes)

  • 김성민;김윤제;조형희
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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    • pp.298-303
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    • 2002
  • Dispersion of coolant jets in a film cooling flow field is the result of a highly complex interaction between the film cooling jets and the mainstream. In order to investigate the effect of blowing ratios on the film cooling of turbine blade, cylindrical body model was used. Mainstream Reynolds number based on the cylinder diameter was $7.1{\times}10^4$. The effect of coolant flow rates was studied for blowing ratios of 0.7, 0.9, 1.2 and 1.5, respectively. The temperature distribution of the cylindrical model surface is visualized by infrared thermography (IRT). Results show that the film-cooling performance could be significantly improved by the shaped injection holes. For higher blowing ratio, the spanwise-diffused injection holes are better due to the lower momentum flux away from the wall plane at the hole exit.

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A Study of Performance and Internal Flow in a New Type of Sewage Pump

  • Nishi, Yasuyuki;Fukutomi, Junichiro
    • International Journal of Fluid Machinery and Systems
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    • 제2권3호
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    • pp.239-247
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    • 2009
  • Sewage pumps are designed with a wide flow channel by, for example, sacrificing some efficiency and reducing the number of blades, in order to prevent plugging with foreign bodies. However, the behavior of foreign bodies which actually flow into a pump is extremely complex, and there are questions about whether the presumed foreign bodies will actually pass through. This paper proposes a new type of sewage pump impeller designed to further improve pump efficiency and performance in passing foreign bodies. This sewage pump impeller has a structure in which the suction flow channel of a closed type non-clog pump is wound in a helical spiral. The focus of this research was to investigate pump performance and internal flow in this single blade sewage pump impeller. The results clearly indicated the following facts: The developed sewage pump impeller exhibits high efficiency over a wide range of flow rates; internal flow of the pump is very complicated; and the internal flow state varies greatly when the flow rate changes.

Experimental Study of Film Cooling Behaviors at a Cylindrical Leading Edge

  • Kim S. M.;Kim Youn-J.
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2002년도 추계학술대회 논문집
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    • pp.81-84
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    • 2002
  • Dispersion of coolant jets in a film cooling flow field is the result of a highly complex interaction between the film cooling jets and the mainstream. In order to investigate the effect of blowing ratios on the film cooling of turbine blade, cylindrical body model was used. Mainstream Reynolds number based on the cylinder diameter was $7.1\;\times\;10^4$. The free-stream turbulence intensity kept at $5.0\%$ by using turbulence grid. The effect of coolant flow rates was studied for blowing ratios of 0.9, 1.3 and 1.6, respectively. The temperature distribution of the cylindrical model surface is visualized by infrared thermography (IRT). Results show that the film-cooling performance may be significantly improved by controlling the blowing ratio. As blowing ratio increases, the adiabatic film cooling effectiveness is more broadly distributed and the area protected by coolant increases. The mass flow rate of the coolant through the first-row holes is less than that through the second-row holes due to the pressure variation around the cylinder surface.

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박피(剝皮)날 및 연마재(硏磨材)가 백하수오(白何首烏) 기계박피(機械剝皮)에 미치는 영향(影響) (Effect of Peeling Blades and Abrasives on Mechanical Peeling of Cynanchum wilfordii Hemsley)

  • 김주;김창수;송영은;이윤석;심진찬;한종현;곽준수
    • Korean Journal of Acupuncture
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    • 제18권1호
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    • pp.165-170
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    • 2001
  • 전북 진안지역에서 재배된 백하수오 2년생 생근을 공시재료로 이용하여 백하수오의 적정 기계박피 조건을 구명하고자 박피날은 돌기형 고무, 플라스틱 패드, 마름모형 철제날과 솔브러시를 공시하고 연마재로서 인조석, 모래, 잔자갈을 이용하여 박피시험을 수행한 결과를 요약하면 다음과 같다. 1. 손박피의 경우 철제칼을 이용하여 1kg을 박피하는 시간이 36분으로 가장 적게 걸렸고 기계박피는 통일 무게 처리에 2분이 소요되는 것으로 나타났으며 명도의 경우 손박피가 기계박피에 비해 다소 높게 나타나는 경향이었다. 2. 백하수오 기계박피시 박피날과 연마재 처리조건에서 수율은 마름모형 철제날에 모래을 처리한 조합에서 89.9%로 가장 낮게 나타났으며 박피율은 마름모형 철제날에 잔자갈을 처리 한 조합에서 71.3%로 가장 높게 나타났다. 3. 백하수오의 박피후 품질결정에 중요한 요소중의 하나인 명도의 경우 마름모형 철제날에 잔자갈을 연마재로 사용한 조합에서 61.90.으로 가장 높게 나타났다. 4. 백하수오 기계박피시 적정 회전속도를 구명하기 위한 조건에서는 박피 회전속도가 빨라 칠수록 수율은 낮은 경향을 나타냈으며 박피율의 경우 회전속도 30r.p.m.에서 66.8%로 가장 높게 나타났으며 명도 또한 57.16으로 나타나 백하수오 기계박피시 적정 회전속도는 30r.p.m.으로 처 리 하는 것이 타당하다고 분석 되었다.

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