• Title/Summary/Keyword: 디퓨저 유동

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Evaluation of Noise Reduction Performance of HVAC System for Ships (선박용 HVAC 시스템의 소음저감성능 평가)

  • Kim, Sang-Ryul;kim, Hyun-Sil;Kim, Jae-Seung;Kim, Bong-Ki;Lee, Sung-Hyun
    • The Journal of the Acoustical Society of Korea
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    • v.29 no.8
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    • pp.497-503
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    • 2010
  • In this paper, evaluation of noise reduction performance of HVAC system for ships by means of HVAC mock-up system is presented. Test is done for six different types of HVAC elements including room unit, silencer, etc. It is found that when diameter of silencer is small and air flow is large, flow noise degrades insertion loss. However, as diameter of silencer becomes larger, the effect of flow noise becomes smaller, and insertion loss up to 25 dB is measured. It is observed that insertion loss of diffuser type room unit is usually between zero and 10 dB, whereas that of the nozzle type room unit can be down to - 15 dB. In addition, it is shown that changing duct arrangement can reduce cabin noise by up to 2 dB, and providing same air flow to each room unit is crucial for generating less noise.

Aerodynamic Design and Numerical Study of a Propane-Refrigerant Centrifugal Compressor for LNG Plant (LNG 플랜트용 프로판 냉매 원심압축기의 공력설계 및 전산해석적 연구)

  • Park, Joo-Hoon;Lee, Won-Suk;Shin, You-Hwan;Kim, Kwang-Ho;Lee, Yoon-Pyo;Chung, Jin-Taek
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.8
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    • pp.781-787
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    • 2011
  • We design a four-stage propane-refrigerant centrifugal compressor for an LNG plant. Using a commercial code, we aerodynamically designed the compressor at each design point of the corresponding stages. We estimated the one-dimensional aerodynamic design output and the three-dimensional shape of the impeller flow passage via three-dimensional flow analysis. In particular, we discuss in detail the flow characteristics of the impeller and the vaneless diffuser passages of the fourth-stage compressor in terms of the velocity fields, the pressure, and the entropy distributions of the flow passages. We include the flow effects of the tip clearance flow, because at this stage the rotating speed and total inlet pressure are higher than those at the other compressor stages are. We carried out performance tests of the designed compressor stages using propane as a refrigerant in the LNG cycle. The practical evaluation could lead to design enhancements in the future.

A Numerical Study on the Impeller Meridional Curvature of High Pressure Multistage Pump (고압 다단 펌프의 임펠러 자오면 곡선에 대한 수치 해석적 연구)

  • Kim, Deok Su;Jean, Sang Gyu;Mamatov, Sanjar;Park, Warn Gyu
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.41 no.7
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    • pp.445-453
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    • 2017
  • This paper presents the hydraulic design an impeller and radial diffuser of a high-pressure multistage pump for reverse osmosis. The flow distribution and hydraulic performance for the meridional design of the impeller were analyzed numerically. Optimization was conducted based on the response surface method by varying the hub and shroud meridional curvatures, while maintaining the impeller outlet diameter, outlet width, and eye diameter constant. The analysis results of the head and efficiency with the variation in the impeller meridional profile showed that angle of the front shroud near the impeller outlet (${\varepsilon}Ds$) had the highest effect on head increase, while the hub inlet length ($d_{1i}$) and shroud curvature (Rds) had the highest effect on efficiency. From the meridional profile variation, an approximately 0.5% increase in efficiency was observed compared with the base model (case 25).

Mixed-Flow Pump Impeller-Diffuser Optimization Method by Using CFX and HEEDS (CFX 와 HEEDS 를 이용한 사류펌프 임펠러-디퓨저 최적화방법)

  • Lee, Yong Kab;Park, In Hyung;Shin, Jae Hyok;Kim, Sung;Lee, Kyoung Yong;Choi, Young Seok
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.39 no.10
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    • pp.831-842
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    • 2015
  • An optimization process was developed to improve mixed-flow pump performance. The optimization process was combined with CFX (a computational fluid dynamics (CFD) code) and HEEDS (an optimization code). CFX is a widely used CFD software for turbo machinery, whereas HEEDS, which uses the SHERPA algorithm, is a newly introduced optimization code. HEEDS can use a large number of optimization variables; thus, it is possible to effectively consider interaction effects. In this paper, an impeller model, which is already optimized with design of experiments (DOE), is used as the base model. The optimization process developed in this paper shows an improved design within an acceptable timeframe.

Numerical Analysis of Flow Rate Distribution of Diffusers with Various Shapes (다양한 디퓨저 형상의 유량 분배 특성에 관한 수치해석 연구)

  • Kim, Myoung Soo;Kim, Hoo Bae;Choi, Hyoung Gwon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.38 no.9
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    • pp.789-795
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    • 2014
  • In this study, the distribution characteristics of diffusers with various shapes that are installed in an open-type thermal storage system are numerically investigated. Four diffusers are designed to distribute a working fluid evenly through the holes on bifurcated pipes. Three-dimensional steady simulations of incompressible laminar flow are conducted using commercial software (ANSYS-FLUENT). The simulation results show that both the bidirectional header-type diffuser and the H-type diffuser distribute the working fluid evenly whereas both the unidirectional and the bidirectional diffusers distribute the working fluid unevenly. The results also show that the H-type diffuser requires a higher head of pump than the bidirectional header-type diffuser. Therefore, the bidirectional header-type diffuser is recommended for use because it enables even distribution of the working fluid and requires a low head of pump.

A Numerical Study on Performance Characteristics of STED with various Pressure Ratios and Cone Shapes using Burnt Gas Properties (연소가스 물성을 이용한 이차목 디퓨저의 압력비와 램 구조물 형상에 따른 성능 특성에 대한 수치적 연구)

  • Yu, Seongha;Jo, Seonghwi;Kim, Hongjip;Ko, Youngsung;Na, Jaejeong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.66-72
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    • 2018
  • A numerical study was conducted to investigate the performance characteristics of a STED with various pressure ratios (PRs) and cone shapes. Due to momentum loss, the pressure in vacuum chamber increased with cone angle for a PR of 75. Also, the STED is started between PRs of 36 and 37 in the case of a cone angle of $15^{\circ}$ and a blockage ratio (BR) of 15%. The results for various PRs and cone shapes are presented, and the optimal cone shape is found to have a cone angle of between $5{\sim}20^{\circ}$ and a BR of between 15~40%.