• Title/Summary/Keyword: 압축시험기

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An Experimental Study on the Performance of Swash Plate Compressor with variations of Oil Charging Conditions (오일 충전량 변화에 따른 사판식 압축기 성능의 실험적 고찰)

  • Kim, Min-Jun;Park, Ik-Seo;Lee, Geon-Ho
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.704-709
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    • 2003
  • The automobile air conditioning system generally consists of laminated type evaporator, swash plate type compressor, condenser, expansion valve and receiver drier. A swash plate type compressor has been used widely in automobile air conditioning system since 1955, because of wider operation range and better durability than other type compressors. In this study, the performance of an swash plate type compressor with variations of oil charging conditions has been investigated experimentally using the hot gas system. Further, the effects of varying compressor speed on the performance of the compressor has been discussed.

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Dynamic Stability Analysis of Axial Compressor Baldes end Vanes (축류 압축기 블레이드와 베인의 동적 안정성 평가에 관한 연구)

  • 정규강;박희용;김명섭;김용련;김유일
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2000.11a
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    • pp.39-39
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    • 2000
  • 축류 압축기 블레이드(blade)와 베인(vane)이 정하중(static load)에서 충분한 강도를 지니고 있더라도 반복하중이나 교번하중을 받게되면, 그 하중이 작더라도 파괴가 일어날 수 있다. 축류 압축기 블레이드와 베인의 피로파괴(fatigue failure) 현상은 개발 중인 가스터빈엔진 뿐만 아니라 현재 운용중인 엔진에서도 발생할 수 있는 엔진손상의 주요 원인이다. 블레이드나 베인의 동적 안정성 평가는 에어포일(airfoil)의 피로특성과 엔진운용조건에 따라서 발생하는 복잡한 공력가진과의 연관성을 고려하여 수행되어야 하기 때문에, 해석과 구성품 시험을 통하여 우선적으로 강도 평가를 실시하여야 한다.(중략)

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Performance Test for a Centrifugal Air Compressor (원심형 공기압축기 성능시험)

  • 신유환;안이기;김광호;손병진
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.8
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    • pp.1964-1971
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    • 1995
  • In the present study, the performance characteristics of a centrifugal air compressor were investigated experimentally. The PC controlled performance test facility for a centrifugal air compressor driven by an electric motor with a gear box to achieve higher compressor rotating speed was set up in the present study. The performance test for a turbocharger compressor of a diesel engine was conducted, and in a case of 34,800 rpm, pressure ratio 1.18, flow rate 0.09kg/s, compressor efficiency 61% were investigated. Adiabatic power for a tested compressor showed maximum value at mass flow ratio 0.8. The value of mass flow ratio of maximum efficiency was about 0.37, it was independent of compressor rotating speed.

System design of an air-cooled 3-stage reciprocating air compressor and performance testing (공랭식 3단 왕복동 공기압축기의 시스템 설계 및 성능시험)

  • Lee, An-Seong;Kim, Yeong-Cheol;Jeong, Yeong-Sik
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.21 no.10
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    • pp.1380-1391
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    • 1997
  • A 150 m$^{3}$/hr, 30 kg/cm$^{2}$, air-cooled 3-stage reciprocating air compressor is designed to be used in starting large diesel engines. A basic design procedure is presented to meet the targeted pressure and flow rate, and especially the volumetric efficiency. Temperature and stress analyses of the cylinder are performed using FEM modelings. The dynamics of valve system is analyzed and stress at the valve seat due to valve impact is evaluated. To reduce friction loss and wear at the compressor engine system, tribological design practices are suggested. Fin-type coolers are designed to dissipate generated compression heat at each stage. Finally, a prototype is manufactured and performance test is carried out utilizing an air tank. Performance results are compared to the design targets, other foreign specifications, and some quality standards.

A Steady-State Simulation and Experimental Study of Turboshaft Engine with Free Power Turbine (분리축방식 터보축 엔진의 정상상태 모사 및 실험연구)

  • 공창덕;기자영;고광웅
    • Journal of the Korean Society of Propulsion Engineers
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    • v.1 no.2
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    • pp.84-90
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    • 1997
  • The turboshaft engine with the free power turbine has been used for various purposes, for instance electric power generator, emergency power source, helicopter powerplant and so on. Steady-state simulation program was developed and experimental tests was carried out for comparing with computer simulation results. The test unit was composed of 1-stage centrifugal compressor, the can type combustor chamber, 1-stage radial type compressor turbine, and radial type free power turbine, and its output power is obtained from 3-phase AC generator. Main component characteristics which was used for the steady state simulation program, were obtained from the manufacturer of the test unit, and modified from experimental results of test unit. In comparison between computer simulation and experimental test results even though the test unit has the operational limit, deviation of component performance characteristics in simulation were within 6% range of experimental results.

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국내 플랜트기자재 성능인증센터 현황

  • Hong, Yong-Ju;Choe, Byeong-Il;Park, Seong-Je
    • Journal of the KSME
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    • v.52 no.10
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    • pp.49-52
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    • 2012
  • 이 글에서는 압축기, 펌프, 밸브 등의 플랜트기자재에 대한 국내 성능인증시험센터의 설비 현황에 대해 소개하고자 한다.

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Magnetization Fault Diagnosis of Concentrated Winding BLDC Motors for Compressor (압축기용 집중권 BLDC 전동기의 착자 불량 진단)

  • Lee, Kwang-Woon
    • The Transactions of the Korean Institute of Power Electronics
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    • v.14 no.3
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    • pp.197-203
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    • 2009
  • This paper presents a novel method to diagnose magnetization faults produced during magnetization process using stator coils of a brushless dc motor with concentrated windings. It is demonstrated that the stator coil magnetization faults can cause a drop of energy efficiency of the brushless dc motor through computer simulations using a magnetization fault model and efficiency test using compressors. The proposed method diagnoses the stator coil magnetization faults by using an inverter during the brushless dc motor driving test after the magnetization process is completed. An experimental study on the brushless dc motor for compressor shows that the stator coil magnetization faults can be detected with high sensitivity.

Development of 1/60th Scale Moving Model Rig Using the Compressed Air Launcher and One-Wire Guidance System of Train Model (압축공기 발사기에 단선 와이어 유도방식을 적용한 1/60축척 터널주행 열차모형 시험기 개발에 대한 연구)

  • Kim, Dong-Hyeon;O, Il-Geun
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.25 no.5
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    • pp.634-644
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    • 2001
  • The test facility of a 1/60-scale model for train-tunnel systems has been recently developed to investigate the effects of tunnel portal shapes, hood shapes and air-shafts for reducing the micro-pressure waves radiating towards the surroundings from the tunnel exit. The present test rig has been advanced from a 1/70-scale facility at NLR in Netherlands. The NLR test rig has the two-wise guidance system that needs two ears attached on the external surface of a model train nose. Therefore, their train models have irregular nose shapes. The main characteristics of the present facility are that the train model is guided by only one wire from the compressed air launcher to the absorber parts of test facility and the wire guidance hole is located at the axial center of a train model. In the present test rig, after a train model is launched, the air jet from the launcher does not enter the tunnel model. Experimental results were compared with numerical predictions to prove the performance of the test facility.