• 제목/요약/키워드: Turbine Impeller

검색결과 91건 처리시간 0.024초

연료전지 BOP용 구심터빈 공력설계에 관한 연구 (A Study of Aerodynamic Design of a Radial Turbine for BOP of MCFC Fuel Cell System)

  • 최범석;안국영;박무룡
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
    • /
    • pp.531-534
    • /
    • 2006
  • 250kw급 MFFC용 연료전지 발전시스템에 적용 가능한 BOP 중에서 터보제너레이터 사이클을 구성하는 구심터빈의 공력설계에 관한 연구를 수행하였다. 기본적인 치수는 평균반경에서의 해석 뿐만 아니라 구심터빈에서 반경 반향으로 변화가 크게 발생하므로 출구측에서 반경반향의 변화를 고려하여 결정하였다. 기본공력설계 과정에서 결정된 구심터빈 임펠러의 자오면 기본형상과 입출구 날개각 등의 기본설계 자료를 바탕으로 임펠러의 기하학적 3차원 형상을 결정하였다. 구심터빈 임펠러의 3차원 블레이드 형상이 결정되면 일련의 CFD를 통한 원심펌프 임펠러 내부의 유동현상을 고찰함으로써 기하학적 형상의 타당성을 검토하는 반복 설계 과정을 수행하였다. 또한, 여러 회전수에 대하여 정익에서와 동익에서의 유량이 일치할 수 있도록 동익 출구의 압력을 조절하여 작동유체의 각 위치에서의 값들을 구하고 각각의 위치에 따라 적절한 손실모델을 적용하여 탈설계점에서의 성능곡선을 구하였다. CFD 해석결과, MCFC 발전시스템에 마이크로 터보제너레이터를 적용시킬 경우에 폐열을 이용하여 16kW 정도의 전력을 추가로 생산할 수 있는 것으로 나타났다.

  • PDF

레이저 형광여기법(LIF)를 이용한 러쉬톤 터빈 교반기의 혼합특성에 관한 연구 (A Study on the Mixing Characteristics in a Rushton Turbine Reactor by a Laser Induced Fluorescence Method)

  • 정은호;김경천
    • 대한기계학회논문집B
    • /
    • 제26권8호
    • /
    • pp.1145-1152
    • /
    • 2002
  • A non-intrusive Planar Laser-Induced Fluorescence(PLIF) technique was applied to study the turbulent mixing process in a Rushton turbine reactor. Instantaneous and ensemble averaged concentration fields was obtained by measuring the fluorescence intensity of Rhodamine B tracer excited by a thin Nd:Yag laser sheet illuminating the whole center plane of the stirred tank. The gray level images captured by a 14-bit cooled CCD camera could be transformed to the local concentration values using a calibration matrix. The dye injection point was selected at the tank wall with three quarter. height (3/4H) from the tank bottom to observe the mixing characteristics in upper bulk flow region. There exist distinct two time scales: the rapid decay of mean concentration after the dye infusion reflects the large scale turbulent mixing while the fellowed slow decay reveals the small scale molecular mixing. The temporal change of concentration variance field conjectures the two sequential processes for the batch type mixing. An inactive column of water is existed above the impeller disk, in which the fluid rotates with the shaft but is isolated from the mean bulk flow.

수차용 봉수장치의 마찰.마모특성에 관한 실험적 연구 (Experimental Study on the Friction and Wear Characteristics of Contact Sealing Unit for a Water Turbine)

  • 김청균;신인철;임광현
    • 한국신재생에너지학회:학술대회논문집
    • /
    • 한국신재생에너지학회 2006년도 추계학술대회
    • /
    • pp.515-518
    • /
    • 2006
  • This paper presents the friction and wear characteristics of contact type sealing unit for a water turbine of a small hydro-power generation, which Is to stop a leakage of a circulating water from a outside of an impeller to an inside of a rolling bearing. The surface wear strongly affect to the seal life of a mechanical face seal. In this study, the hardness of a stainless steel in which is a heat-treated is 892.8 in Vickers hardness and the hardness of silicone carbide of SiC is 714.1 in Vickers hardness. The surface hardness of a heat-treated stainless steel is 25% high compared with that of a ceramic material of SiC. The contact modes of rubbing surfaces aye a dry friction a water film friction and a mixed friction that is contaminated by a dust, silt and moistures, etc. These two factors of a contact rubbing modes and a material property are very important parameters on the tribological performance such as a friction and wear between a seal ring and a seal seat. The experimental result shows that the surface hardness of a seal material is very important on the friction coefficient and a wear volume. Thus, the results recommend higher hardness of a seal material, which may reduce a friction loss and increase a wear life of primary seal components

  • PDF

대기 중 모래 먼지 유입이 소형 가스터빈엔진에 미치는 영향에 대한 연구 (Effect of Sand and Dust Ingestion on Small Gas Turbine Engines)

  • 이동호;임병준;안이기;구현철;김지희
    • 대한기계학회논문집B
    • /
    • 제36권8호
    • /
    • pp.791-796
    • /
    • 2012
  • 항공기용 소형 가스터빈엔진은 항공기의 주엔진 시동을 위한 압축공기 공급, 비상 전원 등을 위한 보조동력장치로 사용된다. 항공기가 모래와 먼지가 함유된 대기 조건에서 운용되는 경우, 보조동력장치와 엔진에 대기 중 모래와 먼지가 유입되며, 이러한 모래 먼지 유입은 가스터빈엔진의 마모, 성능 저하 등을 야기시킨다. 본 연구에서는 모래와 먼지가 소형 가스터빈엔진에 유입되는 경우에 대하여 그 영향성을 고찰하였다. 시험에서의 모래와 먼지 농도는 공기 단위 질량당 $4.4{\times}10^{-5}kg$ 이며, 이는 미 군사규격인 MIL-E-8593 에 제시된 조건과 동일하다. 모래 먼지 유입시험은 총 10 시간 동안 수행되었으며, 시험 전 후의 성능시험을 통해 성능 영향성을 고찰하였다. 또한, 임펠러, 터빈휠 등 주요 구성품에 대하여 분해검사를 수행하여 마모 특성에 대하여 고찰하였다.

Impeller Types and Feeding Modes Influence the Morphology and Protein Expression in the Submerged Culture of Aspergillus oryzae

  • Heo, Joo-Hyung;Vladimir Ananin;Park, Jeong-Seok;Lee, Chung-Ryul;Moon, Jun-Ok;Ohsuk Kwon;Kang, Hyun-Ah;Kim, Chul-Ho;Rhee, Sang-Ki
    • Biotechnology and Bioprocess Engineering:BBE
    • /
    • 제9권3호
    • /
    • pp.184-190
    • /
    • 2004
  • The influences of impeller types on morphology and protein expression were investigated in a submerged culture of Aspergillus oryzae. The impeller types strongly affected mycelial morphology and protein production in batch and fed-batch fermentations. Cells that were cultured by propeller agitation grew in the form of a pellet, whereas cells that were cultured by turbine agitation grew in a freely dispersed-hyphal manner and in a clumped form. Pellet-grown cells showed high levels of protein production for both the intracellularly heterologous protein (${\beta}$-glucuronidase) and the extracellularly homologous protein (${\alpha}$-amylase). The feeding mode of the carbon source also influenced the morphological distribution and protein expression in fed-batch fermentation of A. oryzae. Pulsed-feeding mainly showed high protein expression and homogeneous distribution of pellet whereas continuous feeding resulted in less protein expression and heterogeneous distribution with pellet and dispersed-hyphae. The pellet growth with propeller agitation paralleling with the pulsed-feeding of carbon source showed a high level of protein production in the submerged fed-batch fermentation of recombinant A. oryzae.

전이영역에서의 2단 날개가 있는 접시형 바닥 교반조의 유동 상태 변화 (Flow Pattern Change of Dished Bottom Vessel with Dual Impeller in Transition Region)

  • 고승태
    • Korean Chemical Engineering Research
    • /
    • 제59권1호
    • /
    • pp.94-99
    • /
    • 2021
  • 2단 Rushton turbine 날개를 장착한 접시바닥형 교반조 내의 유동 상태가 어떤 회전수에서 변화하는 현상을 찾아냈다. 층류 영역에서는 회전수를 변화시켜도 안정적인 도넛 링이 형성되어 혼합 패턴에 특이한 변동은 관찰되지 않았다. 전이영역에서의 평바닥형 교반조에서는 회전수에 변화를 주어도 두꺼운 2개의 미혼합 도넛 링에 변화가 없는 반면, 접시바닥형 교반조에서는 회전수가 450 rpm이 되면 두꺼운 2개의 미혼합 도넛 링이 아주 얇은 3개의 도넛 링으로 바뀌어 혼합이 개선되었다. 접시바닷형 교반조에서는 Re=138~178의 영역에서 링 모양의 미혼합 영역이 3곳에서 나타났고 그 크기도 컸지만, 평바닥형 교반조에서는 Re=116~176에서 링모양의 미혼합 영역은 2곳에서 나타났으며 그 크기도 작았다. 이러한 현상이 관찰되는 조건은 전이영역으로, 방해판을 부착하였을 때가 방해판이 없을 때와 비교하여 동력수가 커지기 시작하는 영역임을 알 수 있었다. 또한 교반 레이놀즈수가 300을 넘어 유동 상태에 약간의 난류가 섞이게 되면, 이 같은 흐름 양상의 단절이 해소되어 완전히 혼합되었다.

레이저 형광여기법(LIF)를 이용한 복잡 난류유동장의 혼합특성에 관한 연구 (A Study on the Mixing Characteristics in Complex Turbulent Flow by a Laser Induced Fluorescence Method)

  • 김경천;정은호
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2001년도 춘계학술대회논문집E
    • /
    • pp.542-547
    • /
    • 2001
  • A non-intrusive Planar Laser-Induced Fluorescence(PLIF) technique was applied to study the turbulent mixing process in a Rushton turbine reactor. Instantaneous and ensemble averaged concentration fields are obtained by measuring the fluorescence intensity of Rhodamine B tracer excited by a thin Nd:Yag laser sheet illuminating the whole center plane of the stirred tank. The gray level images captured by a 14-bit cooled CCD camera can be transformed to the local concentration values using a calibration matrix. The dye injection point was selected at the tank wall with three quarter height (3/4H) from the tank bottom to observe the mixing characteristics in upper bulk flow region. There exist distinct two time scales: the rapid decay of mean concentration in each region after the dye infusion reflects the large scale mixing while the followed slow decay reveals the small scale mixing. The temporal change of concentration probability functions conjectures the two sequential processes in the batch type mixing. An inactive column of water existed above the impeller disk, in which the fluid rotates with the shaft but is isolated from the mean bulk flow.

  • PDF

마찰접촉조건에 따른 소수력 수차용 밀봉장치의 마찰.마멸특성 연구 (A Study on the Friction and Wear Characteristics of Contact Sealing Units for a Small Hydro-power Turbine Under Various Rubbing Conditions)

  • 김청균
    • Tribology and Lubricants
    • /
    • 제22권6호
    • /
    • pp.314-319
    • /
    • 2006
  • In this paper, the friction and wear characteristics of contact type sealing unit far a water turbine have been presented. The sealing unit for a small hydropower generation is to stop a leakage of circulating water from an outside of an impeller to an inside of a rolling bearing. The friction heating between a seal ring and a seal seat may radically increase a surface temperature in which increase a power loss and wear on the rubbing surface. The surface wear strongly affect to the seal life of a mechanical face seal. In this study, the hardness of a stainless steel in which is a heat-treated is 892.8 in Victors hardness and the hardness of silicone carbide of SiC is 714.1 in Victors hardness. The surface hardness of a heat-treated stainless steel is 25% high compared with that of a ceramic material of SiC. The contact modes of rubbing surfaces are a dry friction, a water film friction and a mixed friction that is contaminated by a dust, silt, and moistures, etc. These two factors of a contact rubbing modes and a material property are very important parameters on the tribological performance such as a friction and wear between a seal ring and a seal seat in primary sealing unit. The experimental result shows that the surface hardness of a seal material is very important on the friction coefficient and a wear volume. Thus, the results recommend higher hardness of a seal material, which may reduce a friction loss and increase a wear life of primary seal components.

Thermodynamic and Aerodynamic Meanline Analysis of Wet Compression in a Centrifugal Compressor

  • Kang, Jeong-Seek;Cha, Bong-Jun;Yang, Soo-Seok
    • Journal of Mechanical Science and Technology
    • /
    • 제20권9호
    • /
    • pp.1475-1482
    • /
    • 2006
  • Wet compression means the injection of water droplets into the compressor of gas turbines. This method decreases the compression work and increases the turbine output by decreasing the compressor exit temperature through the evaporation of water droplets inside the compressor. Researches on wet compression, up to now, have been focused on the thermodynamic analysis of wet compression where the decrease in exit flow temperature and compression work is demonstrated. This paper provides thermodynamic and aerodynamic analysis on wet compression in a centrifugal compressor for a microturbine. The meanline dry compression performance analysis of centrifugal compressor is coupled with the thermodynamic equation of wet compression to get the meanline performance of wet compression. The most influencing parameter in the analysis is the evaporative rate of water droplets. It is found that the impeller exit flow temperature and compression work decreases as the evaporative rate increases. And the exit flow angle decreases as the evaporative rate increases.

대추력 액체로켓엔진 예비설계 프로그램 : 정상성능 설계를 위한 구성품 모델링 (Preliminary Design Program for a High Thrust Liquid Rocket-Engine : Components Design for Static Performance Design)

  • 고태호;김상민;김형민;윤웅섭
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2009년도 춘계학술대회 논문집
    • /
    • pp.414-416
    • /
    • 2009
  • In order to build a transient simulation program for a high thrust liquid rocket engine(LRE), a static performance simulation program for components were made. The components were the thrust chamber (combustion chamber and supersonic nozzle), centrifugal pump (impeller and volute casing), impulse turbine, and flow control devices (control valve and orifice). Simplified mathematical models based on classical thermodynamic and inviscid theories were used to remove complexity and enhance the utility of the program. We examined the results of each program qualitatively for validate each component modeling.

  • PDF