• 제목/요약/키워드: Compressor Characteristics

검색결과 651건 처리시간 0.025초

축류 압축기 날개의 제작 공차가 공력 특성에 미치는 영향- 1. 날개 형상 곡률 변형 (Influence of Manufacturing Tolerance on the Aerodynamic Characteristics of Axial Compressor Blades - 1. Distortion of Blade Profile Curvatures)

  • 손정락;강동진;전현주;강신형
    • 한국유체기계학회 논문집
    • /
    • 제2권3호
    • /
    • pp.30-36
    • /
    • 1999
  • Blade shape profile in the axial compressor is one of the most important factors governing its aerodynamic characteristics. Manufacturing tolerance, which is inevitable in the blade manufacturing processes, may change blade profile and as a consequence, it will affect the compressor performance. In this paper, influence of manufacturing tolerance on the aerodynamic characteristics of axial compressor blades with distortion of blade profile curvatures is investigated by using a flow simulation technique. It is found that manufacturing tolerance can be an important factor affecting the source of both profile and wake losses of the axial compressor blades.

  • PDF

The Influence of the Vane on the Lubrication Characteristics Between the Vane and the Rolling Piston of a Rotary Compressor

  • Cho, Ihn-Sung;Jung, Jae-Youn
    • Journal of Mechanical Science and Technology
    • /
    • 제20권12호
    • /
    • pp.2242-2249
    • /
    • 2006
  • The rolling piston type rotary compressor has been widely used for refrigeration and air-conditioning systems due to its compactness and high-speed operation. The present analysis is part of a research program directed toward maximizing the advantages of refrigerant compressors. The study of lubrication characteristics in the critical sliding component is essential for the design of refrigerant compressors. Therefore, theoretical investigation of the lubrication characteristics of a rotary compressor being used for refrigeration and air-conditioning systems was investigated. The Newton-Raphson method was used for a partial elastohydrodynamic lubrication analysis between the vane and the rolling piston of a rotary compressor. The results demonstrated that the vane thickness and the center line position of the vane significantly influenced the friction force and the energy loss between the vane and the rolling piston.

Lubrication Characteristics Between the Vane and the Rolling Piston in a Rotary Compressor Used for Refrigeration and Air-Conditioning Systems

  • Jung, Jae-Youn;Oh, Seok-Hyung;Cho, Ihn-Sung
    • Journal of Mechanical Science and Technology
    • /
    • 제15권5호
    • /
    • pp.562-568
    • /
    • 2001
  • The rolling piston type-rotary compressor has been widely used for refrigeration and air-conditioning systems due to its compactness and high-speed operation. The present analysis is part of a research program directed toward maximizing the advantages of refrigerant compressors. The study of lubrication characteristics in critical sliding components is essential for the design of refrigerant compressors. Therefore, theoretical investigation of the lubrication characteristics of a rotary compressor used for refrigeration and air-conditioning systems was studied. The Newton-Raphson method was used for the partial elastohydrodynamic lubrication analysis between the vane and the rolling piston of a rotary compressor. The results showed that the rotational speed of a shaft and the discharge pressure significantly influence the friction force and the energy loss between the vane and the rolling piston.

  • PDF

The Lubrication Characteristics of a Rotary Compressor Used for Refrigeration and Air-conditioning Systems (Part III; Analysis of partial elastohydrodynamic lubrication on vane tip)

  • 조인성;오석형;정재연
    • Tribology and Lubricants
    • /
    • 제17권2호
    • /
    • pp.138-145
    • /
    • 2001
  • The rolling piston type rotary compressor has been widely used for refrigeration and air-conditioning systems due to its compactness and high-speed operation. The present analysis is a part of research program directed toward maximizing these advantages of refrigerant compressors. The study of lubrication characteristics in the critical sliding component is essential for the design of refrigerant compressors. Therefore, theoretical investigation of the lubrication characteristics of a rotary compressor used for refrigeration and air-conditioning systems is studied. Newton-Raphson method is used for the partial elastohydrodynamic lubrication analysis between vane and rolling piston in the rotary compressor. The results show that the rotational speed of a shaft and the discharge pressure influence significantly the friction force and the energy loss between vane and rolling piston.

냉동, 공조용 로터리 콤프레서의 윤활 특성 제1보;롤링 피스톤의 거동해석 (The Lubrication Characteristics of Rotary Compresssor for refrigeration & air-conditioning (Part I; The analysis of Rolling Piston behavior ))

  • 조인성;김진문;백일현;정재연
    • 한국윤활학회:학술대회논문집
    • /
    • 한국윤활학회 1996년도 제23회 학술대회
    • /
    • pp.7-16
    • /
    • 1996
  • Rapid increase of refrigeration & air-conditioning system( r & a system ) in modern industries brings attention to the urgency of development as a core technology in the area. And it required to the compatibility problem of r & a system to alternative refrigerant for the protection of environment. Then, it is requested to research about the lubrication characteristics of refrigerant compressor which is the core thechnology in the r & a system. The study of lubrication characteristics in the critical sliding component is essential for the design of refrigerant compressor. Therefore, theoetical investigation of the lubrication characteristics of rotary compressor for r & a system is studied. And the Runge-Kutta method is used for the analysis of the behavior of rolling piston in the rotary compressor. The results show that the rotating speed of shaft and the discharge pressure have an important effect upon the angular velocity of the rolling piston. This results give important basic data for the further lubrication analysis and design of the rotary compressor.

  • PDF

저진동을 위한 터보형 공기압축기의 설계 (TURBO TYPE AIR COMPRESSOR DESIGN FOR LOW VIBRATION LEVEL)

  • 김명국;정용수;박노길
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 1998년도 유체기계 연구개발 발표회 논문집
    • /
    • pp.159-165
    • /
    • 1998
  • Bearing design of turbo type geared centrifugal air compressor for low vibration level has been studied. The Transfer Matrix Method was used in this paper to analyze the air-compressor consisting of impellers, multi-stage geared rotors, and oil-film hearings. We have to consider this air-compressor as multi-geared rotating system, because characteristics of rotor-bearing system are different from conventional characteristics of non-rotating system. From the view point of Rotordynamics, the stiffness and damping coefficient of oil-film bearing in case of compressor system are more sensitive than other design parameters such as shaft length, shaft diameter and the weight of impellers, etc. Therefore, the stiffness and damping coefficients on each bearing were considered as design parameters. As the result of this study, turbo type air compressor with low vibration level can be achieved.

  • PDF

압축기용 흡입머플러의 음향 및 유동해석 (Acoustic and Flow-filed Analysis of Suction Muffler in Compressor)

  • 주재만;이학준;오상경
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2001년도 춘계학술대회논문집
    • /
    • pp.1162-1167
    • /
    • 2001
  • Suction valve fluttering is generated by reciprocating motions of the piston inhaling and discharging process of gas in the hermetic compressor. A reactive type suction muffler, which produces high pressure-drop because of its complicated flow path, controls the impulsive noise radiated from the flutter of suction valve. The high-pressure drop in the muffler increases the transmission loss, but reduces the EER(Energy Efficiency Ratio) of the compressor. We consider how to design the high acoustic attenuation and low pressure-drop performance to take account of the acoustic and flow performances of the suction muffler. In this study, we identified the suction noise source of compressor from the measurement of the acoustic pulsation and flutter of suction valve. We analyzed the acoustic characteristics of muffler using the finite element method, and compared the experimental and analytical characteristics of flow path of suction muffler. Theoretical predictions and experimental results are compared from the viewpoint of the acoustic performance and energy efficiency of the compressor.

  • PDF

냉동.공조용 로터리 콤프레서의 축심궤적 해석 (The Analysis of Shaft Center Locus in the Refrigeration & Air-conditioning Rotary Compressor)

  • 조인성;장원수;김진문;김동우;오석형;정재연
    • Tribology and Lubricants
    • /
    • 제12권2호
    • /
    • pp.65-73
    • /
    • 1996
  • Rapid increase of Refrigeration and Air conditioning system in modem industries brings attention to the urgency of core technology development in the area. This paper presents theoretical investigation of the lubrication characteristics of rotary compressor for refrigeration and air conditioning. In order to analyze the lubrication characteristics of the main & sub bearing of rotary compressor, the bearing force and locus of shaft center are analyzed by the dynamic analysis of rotary compressor and numerical analysis of Reynolds equation as the operating condition is changed in various ways. In this paper, we used the Runge-Kutta method for the dynamic analysis of rotary compressor and the SOR (Successive OverRelaxation) method for the numerical analysis of Reynolds equation. The result shows that the operating condition of sub bearing is severer than that of main bearing, and eccentricity ratio grows as the bearing force increases. It is believed that the result can be applied to the design of alternative refrigerant rotary compressor.

연료전지용 터보 공기압축기의 설계 및 시험평가 (Design and Experimental Study on a Turbo Air Compressor for Fuel Cell Applications)

  • 최재호
    • 한국수소및신에너지학회논문집
    • /
    • 제19권1호
    • /
    • pp.26-34
    • /
    • 2008
  • This study presents an aerodynamic design and an experimental performance test of a turbo air compressor consisted of mixed-flow impeller and curved diffuser for the PEM fuel cell vehicle application. Many studies compare the efficiency, cost or noise level of high-pressure and low-pressure operation of PEM fuel cell systems. Pressure ratio 2.2:1 is considered as design target The goal of compressor design is to enlarge the flow margin of compressor from surge to choke mass flow rate to cover the operational envelope of FCV. Large-scale rig test is performed to evaluate the compressor performance and to compare the effects of compressor exit pipe volume to stall or surge characteristics. The results show that the mixed-flow compressor designed has large flow margin, and the flow margin of compressor configuration with small exit volume is larger than that with large exit volume.

원심압축기 임펠러의 형상 변화에 따른 저유량 영역에서 발생하는 불안정 유동 평가 (Flow Instability Assessment Occurring in Low Flow Rate Region According to the Change of a Centrifugal Compressor Impeller Shape)

  • 조성휘;김홍집;이명희
    • 한국유체기계학회 논문집
    • /
    • 제19권2호
    • /
    • pp.21-26
    • /
    • 2016
  • The objective of present study is to assess the performance of the first stage compressor in a total 3-stage 5000 HP-level turbo compressor. CFD commercial code, CFX has been used to predict three-dimensional flow characteristics inside of the impeller. Shear Stress Transport (SST) model has been used to simulate turbulent flows through Reynolds-averaged Navier-Stokes (RANS) equations. Grid dependency has been also checked to get optimal grid distribution. Numerical results have been compared with the experimental test results to elucidate performance characteristics of the present compressor. In addition, flow characteristics of the impeller only have been studied for various blade configurations. Angular offset in leading edge of the blade has been selected for the optimal blade design. Performance characteristics in region of low mass flow rate and high pressure ratio between the impeller entrance and exit have been investigated for the selection of optimal blade design. Also, flow instability such as stall phenomena has been studied and anti-stall characteristics have been checked for various blade configurations in the operational window.