• 제목/요약/키워드: Turbo-compressor

검색결과 147건 처리시간 0.022초

저압방식을 적용한 대형과급기관의 배기가스에 관한 EGR효과 (EGR Effects on Exhaust Gas of Heavy-Duty Turbo Charge Engine with Low Pressure Route System)

  • 오용석
    • 한국산학기술학회논문지
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    • 제3권1호
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    • pp.58-62
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    • 2002
  • 본 연구는 기관의 성능과 배출가스의 ECR 효과을 대한 것으로 기관은 6실린더 11리터의 대형터보디젤기관이며 ECR 방식은 저압루트시스템을 적용하였다. EGR 작동방식은 기계시이며 터빈 출구로부터 압축기 입구로 재순환시키는 방식이다. 또한 실험은 기관회전수와 부하별로 변경시켰으며 ECR율은 4%와 8%로 고정하여 실험하였고 그 결과를 기존 기관의 성능 및 배출가스결과와 비교 분석하였다. 따라서 본 연구의 목적은 대형터보디젤기관에 폭넓은 작동범위에서 ECR에 의한 기관 및 배출가스 성능에 미치는 영향을 고찰하고자 한다.

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하이브리드 타입 초소형 가스터빈엔진 개발 및 초도 시운전 (Preliminary Study of Hybrid Micro Gas Turbine Engine)

  • 서준혁;최주찬;권길성;백제현
    • 한국유체기계학회 논문집
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    • 제19권1호
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    • pp.24-30
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    • 2016
  • In this study, a 2W micro-gas turbine engine was designed using micro-electro-mechanical systems (MEMS) technology, and experimental investigations of its potential under actual combustion conditions were performed. A micro-gas turbine (MGT) contains a turbo-charger, combustor, and generator. Compressor and turbine blades, and generator coil were manufactured using MEMS technology. The shaft was supported by a precision computer numerical control (CNC) machined static air bearing, and a permanent magnet was attached to the end of the shaft for generation. A heat transfer analysis found that the cooling effect of the air bearing and compressor was sufficient to cover the combustor's high temperature, which was verified in an actual experiment. The generator performance test showed that it can generate 2W at design rotational speed. Prototype micro-gas turbine generated maximum 1 mW electric power and lasted up to 15 minutes.

LabVIEW를 이용한 무인항공기용 소형 터보제트 엔진의 Fuzzy-PID 제어기 설계 (Design of Fuzzy-PID Controller for Turbojet Engine of UAV Using LabVIEW)

  • 신행철;지민석
    • 한국항행학회논문지
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    • 제20권3호
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    • pp.190-195
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    • 2016
  • 본 논문에서는 무인항공기용 소형 터보제트엔진에 대해 압축기 서지현상 및 화염소실을 방지하면서 과도응답 특성을 개선하는 제어기를 설계하였다. 터보제트 엔진의 가 감속 시 서지현상과 flame-out 현상을 방지하기 위해 연료 유량 제어 입력을 Fuzzy-PID 제어기로 생성하고 신속하고 안전하게 원하는 속도로 수렴할 수 있도록 제어기 설계한다. LabVIEW을 이용한 시뮬레이션을 통해 PID와의 응답특성 비교 분석 및 신속하고 안전하게 원하는 속도로 수렴하는 제어 성능을 확인하였다.

열회수를 고려한 소형 증기분사 가스터빈 시스템 해석 (Analysis of a small steam injected gas turbine system with heat recovery)

  • 김동섭;조문기;고상근;노승탁
    • 대한기계학회논문집B
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    • 제21권8호
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    • pp.996-1008
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    • 1997
  • This paper describes a methodology and results for the analysis of a small steam injected gas turbine cogeneration system. A performance analysis program for the gas turbine engine is utilized with modifications required for the model of steam injection and the heat recovery steam generator (HRSG). The object of simulation is a simple cycle gas turbine engine under development which adopts a centrifugal compressor. The analysis is based on the off-design operation of the gas turbine and the compressor performance map is utilized. Analyses are carried out with the injection ratio as the main parameter. The effect of steam injection on the power and efficiency of gas turbine and cogeneration capacity is investigated. Also presented is the variation in the main operating parameters inside the HRSG. Remarkable reduction in NOx generation by steam injection is confirmed. In addition, it is observed that for the 100% power operation the temperature of the cooled first nozzle blade decreases by 100.deg. C at full steam injection, which seems to have a favorable effect on the engine life time.

스마트 무인기용 가스터빈 엔진의 탈설계 영역 구성품 손상 진단에 관한 연구 (A Study on Fault Detection of Off-design Performance for Smart UAV Propulsion System)

  • 공창덕;고성희;최인수;이승현;이창호
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.245-249
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    • 2007
  • 본 연구에서는 모델 기반(Model-Based) 성능진단에 신경회로망을 적용하였고, SIMULINK를 이용하여 PW206C 터보축 엔진의 모델링을 수행하였다. 비행 고도, 비행 마하수, 가스발생기 회전수에 따른 다양한 운용영역의 성능데이터를 base로 하여 압축기, 압축기터빈, 동력터빈의 성능 저하에 대한 학습 데이터를 획득하고 역전파(Back Propagation Network)를 이용하여 훈련 하였다. 설계점 및 탈설계 영역에서 압축기, 압축기터빈, 동력터빈의 단일 손상 탐지를 수행한 결과 손상된 구성품을 잘 탐지함을 확인할 수 있었다.

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삽입관이 있는 확장형 소음기에서의 기류음 감소 (Reduction of Flow-Induced Noise in an Expansion Muffler with Lids)

  • 강웅;김형진;성형진
    • 대한기계학회논문집B
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    • 제33권2호
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    • pp.79-84
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    • 2009
  • Turbocharger has been widely used in many passenger cars in application with diesel engines because of high power and fuel efficiency. However, flow-induced noise (whoosh or hissing noise) which is generated within a compressor during its operation at marginal surge line can deteriorate noise characteristics. Hissing noise excitation is associated with the generation of turbulence within the turbocharger compressor and radiated through the transmission path in a turbocharger system. In this study, a expansion muffler with lids is devised and installed in the transmission path to reduce the hissing noise. Acoustic and fluid dynamic characteristics for the muffler are investigated which are related to the unsteadiness of turbulence and pressure in the turbocharger system. A transfer matrix method is used to analyze the transmission loss of the muffler. A simple expansion muffler with lids is proposed for the reduction of high frequency component noise. Turbulence simulation is carried out by a standard k - ${\varepsilon}$ model. An optimal design condition of the muffler is obtained by extensive acoustic and fluid dynamic analysis on the engine dynamometer with anechoic chamber. A significant reduction of the hissing noise is achieved at the optimal design of the muffler as compared with the conventional muffler.

스마트 무인기용 가스터빈 엔진의 탈설계 영역 구성품 손상 진단에 관한 연구 (A Study on fault Detection of Off-design Performance for Smart UAV Propulsion System)

  • 공창덕;고성희;기자영;이창호
    • 한국추진공학회지
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    • 제11권3호
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    • pp.29-34
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    • 2007
  • 본 연구에서는 모델 기반(Model-Based) 성능진단에 신경회로망을 적용하였고, SIMULINK를 이용하여 PW206C 터보축 엔진의 모델링을 수행하였다. 비행 고도, 비행 마하수, 가스발생기 회전수에 따른 다양한 운용영역의 성능데이터를 base로 하여 압축기, 압축기터빈, 동력터빈의 성능 저하에 대한 학습데이터를 획득하고 역전파(Back Propagation Network)를 이용하여 훈련하였다. 설계점 및 탈설계 영역에서 압축기, 압축기터빈, 동력터빈의 단일 손상 탐지를 수행한 결과 손상된 구성품을 비교적 잘 탐지함을 확인할 수 있었다.

Application of a Turbojet Engine for Fire Extinguishing

  • Slitenko, A.F.;Kim, SooYong
    • International Journal of Aeronautical and Space Sciences
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    • 제1권1호
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    • pp.62-69
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    • 2000
  • Present study deals with performance analysis of an inert gas generator (IGG) which can be used as effective means to suppress fire. The IGG uses a turbo-jet engine to generate inert gas for fire extinguishing. It is generally known that a less degree of oxygen content in the product of combustion will increase the effectiveness of fire extinguishing. An inert gas generator system with water injection has advantages of suffocating and cooling effects that are very important factors for fire extinguishing. Some aspects of influencing parameters, such as, air excess coefficient, compressor pressure ratio, air temperature before combustion chamber, gas temperature after combustion chamber, mass flow rate of water injection etc. on the performance of IGG system are investigated.

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연료전지 차량용 공기 블로워의 공력 설계 (Aerodynamic Design of Cathode Air Blower for Fuel Cell Electric Vehicle)

  • 김우준;박창호;지용준;조경석;김영대;박세영;오창훈
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2007년도 추계학술대회 논문집
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    • pp.197-200
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    • 2007
  • FCEV uses electric energy generated from fuel cell stack, thus all consisting parts must be re-designed to be suitable for electricity based system. Cathode air blower which supplies compressed air into fuel cell stack has similar shape of turbocharger, but a radial turbine of traditional turbocharger is removed and high speed BLDC motor is installed . Generally, maximum 10% of electric power of fuel cell stack is consumed in air blower, therefore an effective design of air blower can improve the performance of FCEV directly. This study will present an aerodynamic design process of an air blower and compare computational results with experimental data.

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과급디젤기관의 성능시뮤레이션 프로그램개발 (Development of a Simulation Program for the Performance of Turbo-Charged Diesel Engines)

  • 최재성;박태인
    • Journal of Advanced Marine Engineering and Technology
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    • 제18권2호
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    • pp.97-103
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    • 1994
  • This paper describes briefly the simulation program for predicting the performance of a high speed turbocharged four cycle diesel engine. The wave phenomena in the intake and exhaust systems are calculated by the characteristic method. The combustion process in the power cycle is represented by the heat release pattern which is given by the Wiebe's function or the pattern based on measured values. Turbocharger matching for the engine is described by utilizing the characteristic maps of both the compressor and turbine, which are obtained from quasi-steady states. A comparison of experimental and calculated results shows a good agreement. Then the influences of the intake system, the period of valve overlap and the characteristics of the turbine are numerically investigated by the simulation.

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