• Title/Summary/Keyword: Back Pressure Chamber

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A Study on the Design of Back Pressure for Automotive Scroll Compressor

  • Koo, In-Hwe;Lee, Geon-Ho
    • International Journal of Air-Conditioning and Refrigeration
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    • v.17 no.1
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    • pp.1-6
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    • 2009
  • The optimum design of back pressure chamber is one of the most important factors in designing scroll compressors because it has a great influence on the efficiency and other design parameters. The design process can be divided into 2 parts. One is obtaining the optimum pressure of the chamber and keeping it in constant value. The other is finding out the minimum inflow rate of medium with which back pressure chamber is filled. In this study we are focused on the first step. At first we added a simple structure that can change back pressure without reassembling compressor. It makes possible to obtaining optimum back pressure. Then we designed an equipment that the back pressure control valve assembly could be independently tested with. Spring was redesigned to decrease stiffness variation. Also sealing mechanism of back pressure control valve was improved to more effective way. As a result, it was verified that in a real mode test back pressure variation could be retained in 2.3% with discharge pressure and operating frequency varied. In addition the integrated structure of back pressure control valve is expected to contribute to effective manufacturing process.

Design of Back Pressure Control Valve for Automotive Scroll Compressor (차량용 전동식 스크롤 압축기의 배압제어밸브 설계)

  • Nam, Bo-Young;Koo, In-Hwe;Han, Young-Chang;Lee, Geon-Ho
    • Proceedings of the SAREK Conference
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    • 2007.11a
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    • pp.410-415
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    • 2007
  • The optimization of back pressure chamber is one of the most important factors in designing scroll compressors, because it has a great influence on the efficiencies and other design parameters. The design process can be divided into 2 parts. One is obtaining the optimum pressure of the chamber and keeping it in constant value. And the other is finding out the minimum inflow rate of medium with which back pressure chamber is filled. In this study we are focused on the first step. At first we added a simple structure that could change back pressure without reassembling compressor. It makes the optimum back pressure be obtained. And then we devised an equipment that the back pressure control valve assembly could be independently tested with. A spring was redesigned to decrease stiffness variation. And sealing mechanism of back pressure control valve was improved to more effective way. As a result it was verified in a real mode test that back pressure variation could be stabilized within 2.3% when discharge pressure and operating frequency varied. And the integrated structure of back pressure control valve is expected to contribute to an effective manufacturing process.

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Numerical Analysis of Noise Reduction and Back-pressure for a Simple Expansion Chamber with a Partition (내부 파티션을 갖는 단순확장관의 소음저감 및 배압특성의 전산해석)

  • Kim, Yeon Woo;Jeong, Weuibong
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.24 no.11
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    • pp.883-889
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    • 2014
  • Mufflers have been widely used in the exhaust system to reduce the noise. However, installing muffler may deteriorate the efficiency due to the increase of back pressure. Mufflers usually consist of partition plates and perforated holes in a expansion chamber. In this paper, the influences of the location of the partition and hole on the acoustic TL and back pressure were examined. The acoustic TL was predicted using virtual lab commercial software, while the back pressure were predicted using CFX commercial software. The results were used to set up a database for finding their trends. The optimal muffler model in user-interested frequency range could be selected by analyzing this database.

Effects of a Flow Guide on the Arcing History in a Thermal Puffer Plasma Chamber (유동 가이드가 열파퍼 플라즈마 챔버의 아크현상 이력에 미치는 영향)

  • Lee, Jong-Chul;Kim, Youn-Jea
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.31 no.10
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    • pp.832-839
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    • 2007
  • The geometry and dimensions of an expansion chamber are decisive factors in thermal puffer plasma chamber designs. Because they together dominate the temperature and speed at which the cooling gas from the chamber flows back through a flow channel to the arcing zone for the successful interruption of fault currents. In this study, we calculated the flow and mass transfer driven by arc plasma, and investigated the effects of a flow guide installed inside a thermal puffer plasma chamber. It is found that the existing cold gas of the chamber mixes with hot gases entrained from the arcing zone and is subjected to compression due to pressure build-up in the chamber. The pressure build-up with the flow guide is larger than that without due to a vortex which rotates clockwise around the chamber center. By the reverse pressure gradient, the mixing gas of the chamber flows back out for cooling down the residual plasma near current zero. In the case with the flow guide, the temperature just before current zero is lower than that without, and the Cu concentration with high electrical conductivity is also less than that without the flow guide.

Minimization of Tilting Moment of Co-Rotating Scroll Compressor by Design of Back Pressure Chamber (배압실의 설계를 통한 상호회전 스크롤 압축기의 전복 모멘트 최소화)

  • Gu, In-Hoe;Park, Jin-Mu
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.24 no.5 s.176
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    • pp.1305-1313
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    • 2000
  • In a co-rotating scroll compressor, both scrolls rotate on their fixed axes contrary to the conventional orbiting type scroll machine. This implies fixed locations and directions of the gas pressure force and sealing force. Because the tilting moment is mainly caused by interplay between the resultant force of above forces and bearing reaction force, the variation during one cycle is relatively small. Under real operation, this moment is balanced by the restoring moment created by the reaction between the baseplate and thrust bearing or between the scroll tip and baseplate. If these reactions become too large, greater torque is required due to increased friction in addition to the wear of mating parts. Consequently, appropriate study and minimization of tilting moment is important in the design of scroll machines. In this study, taking into account of the small variation of tilting moment during one cycle, we minimize the moment and thrust bearing reaction force by a properly designed back pressure chamber. As a result, for both the driving and driven scrolls, the tilting moment and the reaction force of thrust bearing can be minimized. And the stability is improved for all cases.

Multi-layered neural network-based pressure curve estimation for hydroforming (다층 신경회로망 기법을 이용한 하이드로포밍 공정의 성형압력곡선추정)

  • 현봉섭;김재선;조형석
    • 제어로봇시스템학회:학술대회논문집
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    • 1992.10a
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    • pp.607-612
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    • 1992
  • For hydroforming process, determination of back-up fluid pressure in chamber is one of the most essential tasks. In this paper, we present a back-up pressure estimation system which estimates the back-up pressure of hydroforming process utilizing a multi-layered neural network. The neural network learns the nonlinear relation ship between the back-up pressure and the geometric state variables of hydroforming process. The proposed method does not necessitate sophisticated analysis on hydroforming process but some geometric intuition. The experimental results show that the neural network well approximates the nonlinear relationship between the back-up pressure and the geometric state variables of hydroforming process, thus giving the good estimation of back-up pressure vs punch stroke curve.

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Dynamic Characteristics of Pintle Nozzle about Changes of Chamber Boundary Condition (연소실 경계조건 변화에 따른 핀틀 노즐의 동특성 연구)

  • Jeong, Kiyeon;Kang, Dong-Gi;Lee, Daeyeon;Choi, Jaesung
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.22-31
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    • 2018
  • In this study, numerical simulations were performed to determine the dynamic characteristics of a pintle nozzle, with changes to the chamber boundary conditions. To apply movement, to the pintle, the nozzle and pintle were created separately by an auto-grid generation program using an overset grid method. The chamber boundary conditions were selected between a constant mass-flow rate condition and a propellant burn-back condition. The pressure and thrust characteristics of the constant mass-flow rate condition were determined by changing the ratio of the mass-flow rate in the inlet. The propellant burn-back condition was considered by formulation of the combustion rate. The burn-back conditions represented nonlinear phenomena, unlike the constant mass flow rate, and a small flow rate resulted in a large change in the chamber pressure.

Development of Large Calibration Chamber System (Large Calibration Chamber의 개발)

  • 정충열;김태준;김대규;이우진
    • Proceedings of the Korean Geotechical Society Conference
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    • 2002.03a
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    • pp.673-678
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    • 2002
  • Laboratory calibration chamber tests for cone penetrometers, pressuremeters and dilatometers in cohesionless soil specimens have been conducted by numerous researchers. However, there have been only few applications to compacted or preconsolidated cohesive soils. Therefore, for the first time, Calibration Chamber System was developed in Korea University. This can be attributed to the extremely time consuming and laborious process involved in the preparation of large cohesive soil specimens in addition to other complexities involving instrumentation for pore pressure monitoring and the need for maintaing saturation by back pressure. Chamber System with similar principle as LSU Chamber System was made of more strengthen and complementary form by increasing system diameter(1.2m), carrying out 1st and 2nd consolidation process in one system for smooth and safe work, accurate Data Aquisition.

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Computational and Experimental Simulations of the Flow Characteristics of an Aerospike Nozzle

  • Rajesh, G.;Kumar, Gyanesh;Kim, H.D.;George, Mathew
    • Journal of the Korean Society of Visualization
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    • v.10 no.1
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    • pp.47-54
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    • 2012
  • Single Stage To Orbit (SSTO) missions which require its engines to be operated at varying back pressure conditions, use engines operate at high combustion chamber pressures (more than 100bar) with moderate area ratios (AR 70~80). This ensures that the exhaust jet flows full during most part of the operational regimes by optimal expansion at each altitude. Aero-spike nozzle is a kind of altitude adaptation nozzle where requirement of high combustion chamber pressures can be avoided as the flow is adapted to the outside conditions by the virtue of the nozzle configuration. However, the thrust prediction using the conventional thrust equations remains to be a challenge as the nozzle plume shapes vary with the back pressure conditions. In the present work, the performance evaluation of a new aero-spike nozzle is being carried out. Computational studies are carried out to predict the thrust generated by the aero-spike nozzle in varying back pressure conditions which requires the unsteady pressure boundary conditions in the computational domain. Schlieren pictures are taken to validate the computational results. It is found that the flow in the aero-spike nozzle is mainly affected by the base wall pressure variation. The aerospike nozzle exhibits maximum performance in the properly expanded flow regime due to the open wake formation.

Behaviour of Ultra-High Pressure Diesel Spray on Electronic Hydraulic FuelInjection System (전자유압식 분사계에 의한 초고압 디젤분무의 거동에 관한 연구)

  • 장세호;김준효;안수길
    • Transactions of the Korean Society of Automotive Engineers
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    • v.4 no.2
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    • pp.137-146
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    • 1996
  • Behaviour of ultra-high pressure diesel spray and its structure in a constant-volume pressure chamber were studied with injection pressure ranging from 35 to 110MPa. Sprays were observed by using the back illumination scattering method and righ angle scattering method. The spray process mechanism were investigated with both photographs. As a result, the spray angle and air entrainment angle was larger as injection pressure and back pressure increase. It becomes clear that mean air-fuel ratio is increased by increasing the injection pressure.

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