• 제목/요약/키워드: Vane test

검색결과 178건 처리시간 0.033초

Comparative analysis of internal flow characteristics of LBE-cooled fast reactor main coolant pump with different structures under reverse rotation accident conditions

  • Lu, Yonggang;Wang, Xiuli;Fu, Qiang;Zhao, Yuanyuan;Zhu, Rongsheng
    • Nuclear Engineering and Technology
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    • 제53권7호
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    • pp.2207-2220
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    • 2021
  • Lead alloy is used as coolant in Lead-based cooled Fast Reactor (LFR). The natural characteristics of lead alloy are combined with the simple structural design of LFR. This constitutes the inherent safety characteristics of LFR. The main work of this paper is to take the main coolant pump (MCP) in the lead-cooled fast reactor (LFR) as the research object, and to study the flow pattern distribution of the internal flow field under the reverse rotation pump condition, the reverse rotation positive-flow braking condition and the reverse rotation negative-flow braking condition. In this paper, the double-outlet volute type and the space guide vane are selected as the potential designs of the CLEAR-I MCP. In this paper, the CFD method is used to study the potential reverse accident of the MCP. It is found that the highest flow velocity in the impeller appears at the impeller outlet, and the Q-H curves of the two design programs basically coincide. The space guide vane type MCP has better hydraulic performance under the reverse rotation positive-flow condition, the Q-H curves of the two designs gradually separate with increasing flow rate, and the maximum flow velocity inside the space guide vane type MCP is obviously lower than that of the double-outlet volute type. For the reverse rotation test of MCP, only the condition of the forward rotating pump of the main coolant pump is tested and verified. For the simulation of the MCP in LBE medium, it proved that the turbulence model and basic settings selected in the simulation are reliable.

현장시험에 의한 소수력발전용 튜블러수차시스템 성능계측 (Performance Measurement of a Tubular Type Turbine System for Small Hydropower by Field Test)

  • 황영호;이영호;최영도
    • 한국유체기계학회 논문집
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    • 제14권6호
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    • pp.5-10
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    • 2011
  • Recently, small hydropower attracts attention because of its renewable, clean and abundant energy resources to develop. Therefore, a tubular type hydro turbine is proposed for small hydropower in this study because the turbine has relatively simple structure and high possibility of applying to small hydropower. The purpose of this study is to investigate the performance characteristics of the turbine by field test. Field test iss conducted using one tubular turbine system as well as serial arrangement system by two tubular turbines taking into consideration of actual operation conditions. The results show that efficiency of test turbine changes considerably by the runner vane angle. Best efficiency of one turbine arrangement is higher than that of two turbine serial arrangement.

Plant Minimum Stable Load (Pmin) Test for Ilijan CCPP

  • Kim, Si Moon;Yun, Wan No;Jang, Cheol Ho;Park, Se Ik
    • KEPCO Journal on Electric Power and Energy
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    • 제2권1호
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    • pp.83-88
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    • 2016
  • This paper describes the test results of plant minimum stable load (Pmin) for Ilijan Power Plant. The test was conducted on May 13 through 14, 2015 to investigate the plant operating and equipment condition in accordance with "Ilijan Plant Performance Test Procedure on Plant Minimum Stable Load" [1]. This paper also contains the assessment of the impact of Pmin to plant operating parameters and possible technical operating issues when operating at lower loads and to recommend the safe minimum load operation of Ilijan per block. In addition, this paper describes the performance calculation results of efficiency and heat rate depending on the load level.

제트 베인형 추력편향장치의 성능시험 (Performance Test of a Jet vane type Thrust Vector Control System)

  • 신완순;이정민;이택상;박종호;김윤곤;이방업
    • 한국추진공학회지
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    • 제3권4호
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    • pp.75-82
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    • 1999
  • 초음속 유동장치를 사용하여 제트 베인형 추력편향장치의 이론적 해석과 성능평가를 수행하였다. 현재 개발되었거나, 개발중인 제트 베인형 추력편향장치는 전술미사일이나 로켓의 공중발사, 함대발사, 수중발사 미사일과 고 고도 자세제어에 사용되고 있다. 저속도, 고 앙각의 비행시나 공기가 희박한 고 고도에서는 공력제어의 부족한 제어력을 향상시키기 위해 추력편향장치를 이용하여 추력 방향을 변경하고 제어력을 얻음으로써 방향 제어에 보다 월등한 성능을 발휘하는 것으로 알려져 있다. 제트 베인 방식의 추력편향장치는 고도와 주위환경에 관계없이 작동되며, 제트 베인 편향각 $30^{\circ}$ 까지 효과적인 성능을 발휘하여 발사 초기시 그 성능을 이상적으로 나타낸다. 따라서 본 연구에서는 자체 제작한 초음속유동장치의 성능시험 수행 및 노즐에서 발생되는 초음속 제트를 가시화하고, 2종의 제트 베인의 형상과 편향각에 따른 유동특성에 대해 조사하였다.

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The thickness of the soft soil layer and canal-side road failure: A case study in Phra Nakhon Si Ayutthaya province, Thailand

  • Salisa Chaiyaput;Taweephong Suksawat;Lindung Zalbuin Mase;Motohiro Sugiyama;Jiratchaya Ayawanna
    • Geomechanics and Engineering
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    • 제35권5호
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    • pp.511-523
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    • 2023
  • Canal-side roads frequently collapse due to an unexpectedly greater soft-clay thickness with a rapid drawdown situation. This causes annually increased repair and reconstruction costs. This paper aims to explore the effect of soft-clay thickness on the failure in the canal-side road in the case study of Phra Nakhon Si Ayutthaya rural road no. 1043 (AY. 1043). Before the actual construction, a field vane shear test was performed to determine the undrained shear strength and identify the thickness of the soft clay at the AY. 1043 area. After establishing the usability of AY. 1043, the resistivity survey method was used to evaluate the thickness of the soft clay layer at the failure zone. The screw driving sounding test was used to evaluate the undrained shear strength for the road structure with a medium-stiff clay layer at the failure zone for applying to the numerical model. This model was simulated to confirm the effect of soft-clay thickness on the failure of the canal-side road. The monitoring and testing results showed the tendency of rapid drawdown failure when the canal-side road was located on > 9 m thick of soft clay with a sensitivity > 4.5. The result indicates that the combination of resistivity survey and field vane shear test can be successfully used to inspect the soft-clay thickness and sensitivity before construction. The preliminary design for preventing failure or improving the stability of the canal-side road should be considered before construction under the critical thickness and sensitivity values of the soft clay.

공력과 추력방향 동시 제어가 가능한 전기식 구동장치 설계 (Design of Electromechanical Actuator Capable of Simultaneous Control of Aerodynamic and Thrust Vector)

  • 이하준;윤기원;송인성;박창규;이영철
    • 한국항공우주학회지
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    • 제48권1호
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    • pp.35-42
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    • 2020
  • 비행체용 전기식 구동장치는 일반적으로 공력비행 조종날개의 편향각 또는 추력방향을 제어하는 장치로 본 논문은 공력제어와 추력방향 제어가 모두 가능한 전기식 구동장치의 설계 및 개발을 다루고 있다. 본 논문에서는 하나의 작동기로 미익과 제트 베인을 동시에 제어할 수 있고, 비행체의 표적까지 비행동안 효율을 증가시키기 위하여 수직 발사 및 고속 선회 후 제트 베인을 분리할 수 있는 새로운 소형 전기식 구동장치를 제안하였다. 이를 위하여, 푸시-푸시 링크 구조를 사용한 전기식 구동장치를 설계하였고 수학적 모델을 유도하였다. 수학적 모델은 시뮬레이션 결과와 실험 결과를 비교하여 모델의 타당성을 검증하였다. 개발된 구동장치의 성능 및 신뢰성은 성능시험, 환경시험, 지상연소시험을 통하여 검증하였다. 제안된 구동장치는 성능 및 신뢰성 뿐만 아니라 단순하고 콤팩트한 구조로 인해 비행체용 전기식 구동장치로 유용할 것으로 기대된다.

복합혼합날개를 장착한 5${\times}$5 봉다발에서 부수로 혼합 및 임계열유속 실험 연구 (Experimental Study on the Thermal Mixing and the Critical Heat Flux in the 5${\times}$5 Rod Bundle with the Hybrid Mixing Vane)

  • 강경호;신창환;추연준;윤영중;박종국;문상기;천세영
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.2303-2308
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    • 2007
  • Experiments were performed to determine the thermal (or turbulent) diffusion coefficient (TDC) and to investigate the critical heat flux (CHF) performance in the 5${\times}$5 rod bundle with 5 unheated rods which are supported by Hybrid Mixing Vane. In this study, HFC-134a fluid was used as working fluid and the fluid temperature were measured in the important subchannels. To determine the TDC value, the measured fluid temperatures were compared with the predicted values obtained from the MATRA code. The best optimized value of ${\beta}$ was found to be 0.02 by considering prediction statistics, i.e., average and standard deviations of the differences between the experimental results and code calculations. Using the best optimized value of ${\beta}$ as 0.02, the MATRA code predicts the test results of the fluid temperature within ${\pm}$1.0 % of error. According to the experimental results on CHF of 5 non-heating guide tubes, the case with non-heating guide tube showed a little good performance in terms of CHF.

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AE신호의 신경망 형상인식법에 의한 로터리 압축기의 결함 분류에 관한 연구 (Classification of Defects in Rotary Compressor by Neural Pattern Recognition of Acoustic Emission Signal)

  • 이강용;이종명;황인범;김윤원;홍정기
    • 비파괴검사학회지
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    • 제18권1호
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    • pp.17-26
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    • 1998
  • 음향방출법을 이용하여 룸 에어컨에 사용되고 있는 로터리 압축기의 로울러와 베인의 마모결함과 정상인 압축기, 축과 베어링의 scoring 결함과 정상인 압축기를 분류하기 위한 연구를 실사용 상태에서 수행하였다. 이를 위해 AE 신호 형상 인식법과 신경회로망 분류기를 사용하여 모두 완벽하게 분류하였다. 내부압력과 오일과 냉매는 로울러와 베인의 마모에 영향을 미친다.

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A Robotic Vision System for Turbine Blade Cooling Hole Detection

  • Wang, Jianjun;Tang, Qing;Gan, Zhongxue
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2003년도 ICCAS
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    • pp.237-240
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    • 2003
  • Gas turbines are extensively used in flight propulsion, electrical power generation, and other industrial applications. During its life span, a turbine blade is taken out periodically for repair and maintenance. This includes re-coating the blade surface and re-drilling the cooling holes/channels. A successful laser re-drilling requires the measurement of a hole within the accuracy of ${\pm}0.15mm$ in position and ${\pm}3^{\circ}$ in orientation. Detection of gas turbine blade/vane cooling hole position and orientation thus becomes a very important step for the vane/blade repair process. The industry is in urgent need of an automated system to fulfill the above task. This paper proposes approaches and algorithms to detect the cooling hole position and orientation by using a vision system mounted on a robot arm. The channel orientation is determined based on the alignment of the vision system with the channel axis. The opening position of the channel is the intersection between the channel axis and the surface around the channel opening. Experimental results have indicated that the concept of cooling hole identification is feasible. It has been shown that the reproducible detection of cooling channel position is with +/- 0.15mm accuracy and cooling channel orientation is with +/$-\;3^{\circ}$ with the current test conditions. Average processing time to search and identify channel position and orientation is less than 1 minute.

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선박용 송풍기의 날개 끝 간격과 정익이 성능에 미치는 영향에 대한 전산 유체 해석 (Computational and Experimental Study of Effects of Guide Vanes and Tip Clearances on Performances of Axial flow Fans)

  • 이승수;김학선;남광현;홍재익;천승현
    • 대한조선학회논문집
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    • 제41권6호
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    • pp.24-32
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    • 2004
  • The effects of guide vanes and tip clearances on the characteristics nf axial flow fans are investigated both computationally and experimentally. Performance test of fans carried out in full scale shows considerable effects of tip clearance between rotor tip and duct on the characteristics of fans. The tested results are compared with the computation based on the finite volume method to solve the Navier-Stoke equations with $textsc{k}$-$\varepsilon$ turbulence model. The comparison shows good agreements between experimental and computational results. In addition, the effects of shape of guide vanes are numerically studied. The results show that increased volume of separated region around the guide vane reduces the recovery of tangential component of kinetic energy in the wake, resulting in loss of efficiency