• 제목/요약/키워드: High Pressure Turbine Nozzle

검색결과 62건 처리시간 0.022초

급수가열기 추기노즐 충격판 주변의 동체감육 현상의 완화를 위한 실험 및 수치해석적 연구 (Experimental and Numerical Analysis in the Surroundings of Impingement Baffle Plate of the Extracting Nozzle for Disclosing Shell Wall Thinning of a Feedwater Heater)

  • 정선희;김경훈;황경모;송석윤
    • 설비공학논문집
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    • 제19권12호
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    • pp.821-830
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    • 2007
  • Feedwater heaters of many nuclear power plants have recently experienced severe wall thinning damage, which will increase as operating time progresses. Several nuclear power plants in Korea have experienced wall thinning damage in the area around the impingement baffle-installed downstream of the high pressure turbine extraction steam line- inside number 5A and 5B feedwater heaters. At that point, the extracted steam from the high pressure turbine is two phase fluid at high temperature, high pressure, and high speed. Since it flows in reverse direction after impinging the impingement baffle, the shell wall of the number 5 high pressure feedwater heater may be affected by flow-accelerated corrosion. This paper describes the comparisons between the numerical results using the FLUENT code and the down scale experimental data on effect of geometry of the impingement baffle plate on the shell wall thinning. Additionally, a new type impingement baffle plate was installed above the impingement baffle plate in the feedwater heater and then the numerical and experimental study were performed in the same progress.

APU용 구심터빈의 공력리그시험 (Aerodynamic Rig Test of Radial Turbine for APU)

  • 강정식;임병준;안이기
    • 대한기계학회논문집B
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    • 제37권1호
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    • pp.1-7
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    • 2013
  • 본 연구는 보조동력장치에 적용되는 구심터빈의 공력성능시험을 한국항공우주연구원의 고온 터빈 시험리그에서 수행한 결과이다. 리그시험을 위하여 터빈의 형상은 동일하되 팽창비, 마하수 및 유량계수는 실제 엔진과 동일한 값이 되도록 상사법칙을 적용하여 시험하였다. 설계 팽창비는 3.096이며, 상사된 설계회전수는 34909 rpm이고 상사된 터빈 입구온도는 $160^{\circ}C$이다. 터빈의 입구에는 익형 형상의 노즐이 설치되었으며 터빈 휠의 직경은 175.74mm이다. 시험을 통하여 터빈의 성능지도가 생성되었으며 터빈 입구에서의 상세 유동이 측정되었다. 노즐의 허브면에서 측정한 압력과 노즐의 쉬라우드 면과 터빈 휠 케이싱에서 측정한 압력 분포를 볼 때 터빈 내부에서의 팽창과정이 적절함을 확인할 수 있었다.

超音速 노즐흐름에 있어서 凝縮이 傾斜衝擊波에 미치는 影響 (Effects of supersonic condensing nozzle flow on oblique shock wave)

  • 강창수;권순범
    • 대한기계학회논문집
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    • 제13권3호
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    • pp.547-553
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    • 1989
  • 본 연구에서는 작동유체로서 수증기와 거동이 유사한 습공기를 대기 흡입식 풍동을 사용하여 원호 노즐로서 팽창시키는 경우에 대하여 응축충격파가 발생하는 흐름이 측정부내에 쐐기를 설치하여 발생시킨 경사충격파에 미치는 영향에 대해 실험적으로 조사하였다.

증기-증기 이젝터를 적용한 OTEC 시스템 성능의 수치적 분석 (The numerical analysis of performance of OTEC system with vapor-vapor ejector)

  • 윤정인;손창효;예병효;하수정;최인수;이호생;김현주
    • 한국태양에너지학회 논문집
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    • 제34권4호
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    • pp.45-50
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    • 2014
  • In this paper, the Ocean Thermal Energy Conversion(OTEC) with vapor-vapor ejector is proposed newly. At this OTEC system, a vapor-vapor ejector is installed at inlet of condenser. The vapor-vapor ejector plays a very important role in increasing of the production work of low-stage turbine throughout the decrement of outlet pressure of ejector. The performance analysis is conducted for optimizing the system with HYSYS program. The procedure of performance analysis consists of outlet pressure of high turbine, the mass ratio of working fluid at separator, total working fluid rate, and nozzle diameters of vapor-vapor ejector. The main results is summarized as follows. The nozzle diameter is most important thing in this study. When each nozzle diameter of vapor-vapor ejector is 10 mm, the efficiency of OTEC system with vapor-vapor ejector shows the highest value. So it is necessary to set the optimized nozzle diameters of vapor-vapor ejector for achieving the high efficiency OTEC power system.

가스터빈 입구에서의 유동 및 스칼라 분포 특성 (Measurement of Flow and Scalar Distribution at Gas Turbine Inlet Section)

  • 홍성국
    • 한국유체기계학회 논문집
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    • 제13권4호
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    • pp.45-50
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    • 2010
  • The goal of paper is to investigate the flow and scalar distribution through the HP Nozzle Guide Vane (NGV) passage. Flow and scalar distribution measurement are conducted by using 5-hole pressure probe and $CO_2$ tracing technique, respectively. Three different experimental cases are considered depending on cooling flow condition. The result shows that the vortical secondary flow patterns are observed clearly and these flow characteristics maintain through the NGV passage regardless of cooling flow injection. Compared to center region, the high axial velocity flow is observed near wall region due to cooling flow injection. Without cooling flow, the $CO_2$ (scalar) distribution becomes to be uniform quickly due to the strong flow mixing phenomenon. However, in cases of cooling flow, scalar distribution is significantly non-uniform.

소형 가스터빈 연소기 고공환경 점화 시험 설비 구축 및 검증 실험 (Construction of a High-Altitude Ignition Test Facility for a Small Gas-turbine Combustor)

  • 김태완;이양석;김기우;김보연;고영성;김선진;김형모;정용운
    • 한국추진공학회지
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    • 제14권3호
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    • pp.61-68
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    • 2010
  • 본 연구에서는 가스터빈 연소기의 고공환경 모사 점화 성능 시험을 목적으로 소형 고공환경 모사 시험 설비를 구축하였고 이에 대한 성능 실험을 수행하였다. 고공환경 조건인 저압 환경 구현을 위해서는 초음속 디퓨저를 사용하였고, 저온 환경 구현을 위해서는 드라이아이스를 냉각제로 사용한 열교환기를 사용하였다. 저압 환경 구현 성능 실험 결과 연소기로 20g/s의 공기 공급 상태에서도 연소기 내부에 고도 약 6,100m에 해당하는 저압 환경 구현이 가능한 것을 확인하였다. 또한 저온 환경 구현 성능 실험 결과 연소실 내부에 고도 6,100m 이상의 저온 환경 구현이 가능한 것을 알 수 있었으며, 상온공기와 냉각공기의 혼합율 조절로 다양한 고도의 저온 환경 구현이 가능한 것을 확인하였다.

가스터빈 냉각 베인에서 감온액정을 이용한 과도적 열전달 특성에 관한 실험적 연구 (An Experimental Study on Transient Heat Transfer Characteristics of Gas Turbine Cooled Vane by Using Liquid Crystal Thermography)

  • 서남규;장태현
    • Journal of Advanced Marine Engineering and Technology
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    • 제30권1호
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    • pp.22-29
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    • 2006
  • Gas turbine engine among Principal internal combustion engines has been mainly applied as an aero and industrial Power plant. In order to increase its thermal efficiency. it has been raised their pressure ratio of compressor and the turbine inlet temperature. To operate above the limit temperature of turbine material, turbine nozzle vanes should be cooled. For this the cooling air is bled from the compressor section of 9as turbine. Meanwhile, to keep high thermal efficiency of 9as turbine, turbine vanes are to be cooled by using small cooling air Therefore, the complex cooling passages are requested to be designed and evaluated the effectiveness of vane cooling by measuring turbine vane temperature. But it is very difficult or impossible for us to measure local turbine temperatures at actual temperature When local heat transfer coefficients are known these can be calculated, therefore this study has been investigated on obtaining these coefficients of turbine vane at room temperature using TLC.

증기터빈 블레이드의 공진 방지를 위한 실험 연구 (An Experimental Study for Preventing the Resonance of Steam Turbine Blade)

  • 하현천;이동진;류석주
    • 소음진동
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    • 제11권3호
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    • pp.410-415
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    • 2001
  • This paper describes an experimental analysis for improving the stability of blade failure due to the vibration resonance, which happens in the low-pressure steam turbine. Some cracks due to high cycle fatigue were found in the blades of a low-pressure turbine after long time operation. Impact test showed that such failure was mainly caused by the resonance. In other words, since one of the natural frequencies of the grouped blade is very close to the excitation frequency of the nozzle, the resonant vibration leads to a large amplitude of displacement and results in a large amount of stress that may cause fatigue failures in the blades. It is interesting that the blade failures occur only at blades neighboring with the nodal points of the natural vibration mode whose natural frequency is close to the nozzle passing frequency. The effective methods for increasing the reliability against the blade vibration are a heightening the fatigue limit of the blade using an advanced material and a removing the resonance away from the operating speed. It is well known that the removal of theresonance could be obtained by the installation of different types of shrouds, wires, and links between the blades as well as by the chance of the number of nozzles. In the present work, two kinds of modification for avoiding the resonance haute been considered; 1) slot-type finger, 2) long span cover. Full-scale mockup tests have been performed in order to confirm the verification for modification in the shop. Test results show that the use of long span cover is very useful to change the natural frequencies of the grouped blade and to avoid the resonance effectively.

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유동가속부식으로 인한 급수가열기 동체 감육현상 규명과 완화 방안 및 충격판 설계개선에 관한 연구 (A Study on the Shell Wall Thinning by Flow Acceleration Corrosion and Mitigation Plan and Design Modification of a Feedwater Heater Impingement Baffle)

  • 김경훈;황경모;김인태
    • 한국분무공학회지
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    • 제15권2호
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    • pp.83-93
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    • 2010
  • Feedwater heaters of many nuclear power plants have recently experienced severe wall thinning damage, which will increase as operating time progresses. Several nuclear power plants in Korea have experienced wall thinning damage in the area around the impingement baffle inside feedwater heater installed downstream of the turbine extraction stream line. At that point, the extract steam from the turbine is two phase fluid at high temperature, high pressure, and high speed. Since it flows to reverse direction after impinging the impingement baffle, the shell wall of feedwater heaters may be affected by flow-accelerated corrosion. In this paper, to compare degree of shell wall thinning mitigation rate to squared type with mitigation rate of other type baffle plate, four different types of impingement baffle plate-squared, curved, mitigating type and multi-hole type-applied inside the shell. With these comparison data, this paper describes operation of experiments and numerical analysis which is composed similar condition with real feed water heater. And flow visualization is operated for verification of experiments and numerical analysis. In conclusion, this study shows that mitigating type and multi-hole type baffle plate are more effective than other baffle plate about prevention of pressure concentration and pressure value decrease.

급수가열기 동체 감육 현상과 완화 방안 및 충격판 설계개선 (Shell Wall Thinning and Mitigation Plan and Design Modification of a Feedwater Heater Impingement Baffle)

  • 김경훈;황경모;박상훈
    • 한국정밀공학회지
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    • 제27권6호
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    • pp.55-63
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    • 2010
  • Feedwater heaters of many nuclear power plants have recently experienced severe wall thinning damage, which will increase as operating time progresses. Several nuclear power plants in Korea have experienced wall thinning damage in the area around the impingement baffle inside feedwater heater installed downstream of the turbine extraction stream line. At that point, the extract steam from the turbine is two phase fluid at high temperature, high pressure, and high speed. Since it flows to reverse direction after impinging the impingement baffle, the shell wall of feedwater heaters may be affected by flow-accelerated corrosion. In this paper, to compare degree of shell wall thinning mitigation rate to squared type with mitigation rate of other type baffle plate, three different types of impingement baffle plate-squared, curved and mitigating type-applied inside the shell. With these comparison data, this paper describes operation of experiments and numerical analysis which is composed similar condition with real feed water heater. And flow visualization is operated for verification of experiments and numerical analysis. In conclusion, this study shows that mitigating type baffle plate is more effective than other baffle plate about prevention of pressure concentration and pressure value decrease.