• 제목/요약/키워드: Off-design Point

검색결과 259건 처리시간 0.034초

일체형원자로 SMART 냉각재 순환펌프의 전산성능예측 (Computational Performance Prediction of Main Coolant Pump for the Integral Reactor SMART)

  • 김민환;이재선;박진석;김종인;김긍구
    • 한국전산유체공학회지
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    • 제8권3호
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    • pp.32-40
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    • 2003
  • CFD analyses of the three-dimensional turbulent flow in the impeller and diffuser of an axial flow pump including suction and discharge parts are presented and compared with experimental data. The purpose of the current study is to validate the CFD method for the performance analysis of the main coolant pump for SMART and to investigate the effect of suction and discharge shapes on the pump performance. To generate a performance curve, not only the design point but also the off-design points were computed. The results were compared with available experimental data in terms of head generated. At the design point, the analysis accurately predicts the experimental head value. In the range of the higher flow rates, the results are also in very good agreement with the experimental data, in magnitude but also in terms of slope of variation. For lower flow rates, the results shows that the analysis considering the suction and discharge well describe the typical S-shape performance curve of the axial pump.

Investigation of touchdown point mismatch during installation for catenary risers

  • Huang, Chaojun;Hu, Guanyu;Yin, Fengjie
    • Ocean Systems Engineering
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    • 제8권3호
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    • pp.313-327
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    • 2018
  • Meeting the touchdown point (TDP) target box is one of the challenges during catenary riser installation, especially for deep water or ultra-deep water riser systems. TDP location mismatch compared to the design can result in variation of riser configuration, additional hang-off misalignment, and extra bending loads going into the hang-off porch. A good understanding of the key installation parameters can help to minimize this mismatch, and ensure that the riser global response meets the design criteria. This paper focuses on investigating the potential factors that may affect the touchdown point location, and addressing the challenges both in the design stage and during installation campaign. Conventionally, the vessel offset and current are the most critical factors which may affect the TDP movement during installation. With the offshore exploration going deeper and deeper in the sea (up to 10,000ft), other sources such as the seabed slope and seabed soil stiffness are playing an important role as well. The impacts of potential sources are quantified through case studies for steel catenary riser (SCR) and lazy wave steel catenary riser (LWSCR) in deep water application. Investigations through both theoretical study and numerical validation are carried out. Furthermore, design recommendations are provided during execution phase for the TDP mismatch condition to ensure the integrity of the riser system.

원심압축기의 디퓨져 각도조절과 회전수변경에 따른 성능예측에 관한 연구 (Study on performance prediction of centrifugal compressor with diffuser angle and rotational speed change)

  • 박영하;심영호;김재실;조수용
    • 동력기계공학회지
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    • 제16권5호
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    • pp.55-62
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    • 2012
  • Centrifugal compressors are widely used and each operating condition is different. However, it cannot be manufactured according to the every operating condition. In the this study, performance of compressor was evaluated with various rotational speeds of impeller and various stagger angles of diffuser in order to apply a typical model widely. A centrifugal compressor was designed and manufactured based on the design point. On this machines, an experiment was conducted and the performance was predicted at off-design point. The performance prediction was validated with the experimental result and the numerical result. Although the isentropic efficiency on the prediction was slightly lower than that on the experimental result due to the heat loss in the experiment, the pressure ratio was predicted well and also the predicted results were matched well with the numerical results. When the rotational speed of the impeller and the stagger angle of the diffuser were changed together, the compressor can be worked in the high efficiency region and avoided operating in the stall region.

IEEE 802.16e OFDMA-TDD 시스템 Digital Front End의 Fixed-point 설계 최적화 (Optimization of Fixed-point Design on the Digital Front End in IEEE 802.16e OFDMA-TDD System)

  • 강승원;선태형;장경희;임인기;어익수
    • 한국통신학회논문지
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    • 제31권7C호
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    • pp.735-742
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    • 2006
  • 본 논문에서는 IEEE 802.16e OFDMA(Orthogonal Frequency Division Multiplexing-FDMA) TDD(Time Division Duplexing) 시스템 단말 수신기의 입력 신호에 대하여 DC 오프셋 보상, 자동 주파수 조정, 자동 이득 조정을 수행하는 DFE(Digital Front End)의 동작 원리와 Fixed-point 설계 방법에 대하여 설명하고, DFE의 성능을 ITU-R M. 1225 Veh-A 60km/h 채널 환경에서 시뮬레이션 결과를 통해 분석한다. DFE의 Fixed-point 설계시, 시스템의 성능에 영향을 주지 않는 범위 내에서 연산을 통해 출력되는 bit의 크기를 줄임으로서때 H/W 동작의 복잡도를 줄이고, Acquisition time과 안정도 간의 Trade-off를 고려하여 Loop Filter를 설계함으로서 DFE 의 Fixed-point 설계를 최적화 한다.

고고도 장기체공무인기 경량 주익 스파 설계 (Light Wing Spar Design for High Altitude Long Endurance UAV)

  • 신정우;박상욱;이무형;김태욱
    • 한국항공운항학회지
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    • 제22권2호
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    • pp.27-33
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    • 2014
  • There are several methods to improve the flight efficiency of HALE(High Altitude Long Endurance) UAV(Unmaned Aerial Vehicle). Airframe structural point of view, weight reduction of the airframe structure is the most important method to improve the flight efficiency. In order to reduce the weight of airframe structures, new concepts which are different from traditional airframe structure design such as the mylar wing skin should be introduced. The spar is the most important component in a mylar skin wing structure, so the spar weight reduction is the key point for reduction of the wing structural weight. In this study, design trade-off study for the front spar of the HALE UAV wing is conducted in order to reduce the weight. Design and analysis procedure of high aspect ratio wing spar are introduced. Several front spar structures are designed and trade-off study regarding the weight and strength for the each spar are performed. Spar design configurations are verified by the static strength test. Finally, optimal front spar design is decided and applied to the HALE UAV wing design.

탈설계 조건에서 원심압축기의 미끄럼 계수 모델들의 평가 (Assessment of Slip Factor Models for Centrifugal Compressor at Off-Design Condition)

  • 윤성호;백제현
    • 대한기계학회논문집B
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    • 제25권11호
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    • pp.1459-1466
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    • 2001
  • A slip factor is defined as an empirical factor, which should be multiplied to theoretical energy transfer to estimate real work input of a centrifugal compressor. During the last century, researchers have tried to develop simple empirical models to predict the slip factor. However most of these models have been developed based only on design point data. Furthermore flow is assumed inviscid. As a result, these models often fail to predict the correct slip factor at off-design condition. In this study, various models for the slip factor were analysed and compared with experimental and numerical data at off-design conditions. As a result of this study, Wiesner's and Paeng and Chung's models are shown to be applicable for radial impeller, but all the models are found to be inappropriate for backswept impellers.

A Passive Multiple Trailer System with Off-axle Hitching

  • Lee, Jae-Hyoung;Woojin Chung;Kim, Munsnng;Song, Jae-Bok
    • International Journal of Control, Automation, and Systems
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    • 제2권3호
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    • pp.289-297
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    • 2004
  • This paper deals with the design and control of passive multiple trailer systems for practical applications. Due to the cost and complexity of the trailer mechanism, passive systems are preferred to active systems in this research. The design and control objective is to minimize the trajectory tracking errors occurring in passive multiple trailers. Three sorts of passive trailer systems, off-hooked, direct-hooked, and three-point, are discussed in this paper. Trajectory tracking performance and stability issues under constant curvature reference trajectories are investigated for these three types. As well, various simulations and experiments have been performed for each type. It is shown that the proposed off-hooked trailer system produces a tracking performance that is superior to the others.

에어터보램제트 엔진의 아음속 성능 해석 (Subsonic Performance Analysis of Air Turbo-Ramjet Engine)

  • 이양지;양수석;양인영
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제23회 추계학술대회 논문집
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    • pp.62-67
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    • 2004
  • 이 논문에서는 메탄을 연료로 하는 에어터보램제트(ATR) 엔진의 아음속 영역에서의 탈설계점 성능 해석을 수행하였다 이를 위하여 ATR 엔진을 수치적으로 모델링하여 성능을 모사하였다. 각 구성품에 대해 탈설계점 성능을 계산할 수 있도록 모델을 작성하였다. 압축기 작동점은 노즐과의 유량매칭(matching)에 의하여, 터빈 작동점은 일 매칭에 의하여 결정하였다. 성능 해석 결과, ATR 엔진은 기존의 개스 터빈 엔진과 비교해 상당히 다른 탈설계점 특성을 가지고 있음을 보였다.

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장기모의를 통한 도시유역 비점오염원 처리장치 용량 산정 (Determination of Design Capacity for NPS Pollutant Treatment Facilities by Long-term Simulation in Urban Areas)

  • 주진걸;유도근;김중훈
    • 한국물환경학회지
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    • 제27권6호
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    • pp.841-847
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    • 2011
  • In this study, a method to determine the design capacities of nonpoint source (NPS) pollutant treatment facilities in urban areas was suggested. A facility capacity to treat 80 percent of total SS discharge was estimated by 2-year rainfall - runoff - build-up and wash-off simulation at Goonja drainage district in Seoul. For wash-off simulation, four wash-off models (EMC, RC, EXP, and Joo model) were used. As the results, 80 percent of total SS discharge could be treated with only 7.7~31.4% facility capacity of peak flow. The suggested method and results will provide a guideline to determine design capacities of NPS pollutant treatment facility in urban areas.

Design and Manufacture of an Off-axis Aluminum Mirror for Visible-light Imaging

  • Zhang, Jizhen;Zhang, Xin;Tan, Shuanglong;Xie, Xiaolin
    • Current Optics and Photonics
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    • 제1권4호
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    • pp.364-371
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    • 2017
  • Compared to one made of glass, an aluminum mirror features light weight, compact design, low cost, and quick manufacturing. Reflective mirrors and supporting structures can be made from the same material, to improve the athermal performance of the system. With the rapid development of ultraprecise machining technologies, the field of applications for aluminum mirrors has been developed rapidly. However, most of them are rotationally symmetric in shape, and are used for infrared applications. In this paper, the design and manufacture of an off-axis aluminum mirror used for a three-mirror-anastigmat (TMA) optical system at visible wavelengths is presented. An optimized, lightweight design provides a weight reduction of more than 40%, while the surface deformation caused by earth's gravity can meet the required tolerance. The two pieces of an off-axis mirror can be diamond-turned simultaneously in one setup. The centrifugal deformation of the off-axis mirror during single-point diamond turning (SPDT) is simulated through the finite-element method (FEM). The techniques used to overcome centrifugal deformation are thoroughly described in this paper, and the surface error is reduced to about 1% of the original value. After post-polishing, the form error is $1/30{\lambda}$ RMS and the surface roughness is better than 5 nm Ra, which can meet the requirements for visible-light imaging.