• 제목/요약/키워드: Cooled turbine

검색결과 58건 처리시간 0.029초

고정자 권선용 F종 주절연 테이프의 전기적 특성 (Electrical characteristics of class-F groundwall insulation tapes for stator windings)

  • 김태희;강명국;이재권;손삼용
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 하계학술대회 논문집 C
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    • pp.1679-1681
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    • 2004
  • Class-F and B resin-rich type insulating tapes are generally used for the ground wall insulations of respective air-cooled and water-cooled stator windings in larger turbine generators. In this paper, their electrical properties coupled with aging times in higher temperature than designed one in normal condition were experimentally investigated and the results of two comparative tests were presented on the existing class-F resin-rich type tape and a developed one after curing. The resin-rich tapes currently used arc composed of six and a half 3-layer sheets that arc structured with mica paper, the top and bottom supports of it respectively, and the epoxy resin to bind them tightly. The results for breakdown voltage and strength on the cured specimens were presented, which were composed of the unaged, the aged accelerated for one, two, and three thousand hours at 180 $^{\circ}C$. The surface and volume resistivities on them were measured and the results are also presented to make a comparative test for the initial electrical characteristics.

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고정자 권선용 F종 주절연테이프의 기계적 특성 (Mechanical characteristics of class-F groundwall insulation tapes for stator windings)

  • 김태희;강명국;이재권;손삼용
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2004년도 하계학술대회 논문집 C
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    • pp.1676-1678
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    • 2004
  • Class-F resin-rich type insulating tapes are generally used for the groundwall insulations of the large turbine generators with air-cooled and hydrogen-cooled stator windings. In this paper, mechanical strength properties degraded over aging time in higher temperature than designed one in normal condition were experimentally investigated and the results of comparative tests were presented on the existing class-F resin-rich type tape and a developed one after curing. The resin-rich insulating tapes with composite material of Mica/Epoxy/support currently were used in this test. The tests for tensile and flexural strength properties were conducted with the specimens which were composed of unaged and the aged specimens accelerated for one, two, and three thousand hours at 180 $^{\circ}C$. The tensional strength was only measured for the unaged specimens and the results are also presented to make a comparative test for their initial mechanical characteristics.

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대기온도 변화에 따른 150 MW 화력발전소용 공랭식 복수기 송풍기수 선정 (Selection of Number of Fans in an Air-Cooled Condenser of a 150 MW Thermal Power Plant according to Ambient Air Temperature)

  • 황용훈;허기무;윤성훈;문윤재;이재헌;문승재
    • 플랜트 저널
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    • 제10권4호
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    • pp.24-28
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    • 2014
  • 본 연구에서는 150 MW 화력발전소를 기준하여 발전소 건설지역의 최저 대기온도 $-17.1^{\circ}C$부터 최대 대기온도 $36.7^{\circ}C$까지를 $3^{\circ}C$의 일정한 간격으로 구분하여 복수기 압력이 증기터빈의 배압조건을 만족하는 대기온도별 송풍기 수량을 검토하였다. 공랭식 복수기는 대기온도 및 송풍기 운전수량 변화에 따른 냉각공기 순환량에 영향을 받아 운전조건이 변경이 되므로, 대기온도가 복수기 설계기준온도 이상의 경우에는 공랭식 복수기 송풍기의 운전수량을 최대로 해야 하고, 대기온도가 복수기 설계기준온도 미만의 경우에는 증기터빈 배압 운전조건을 만족하는 범위 내에서 송풍기 운전수량을 변화시켜 공랭식 복수기에 가해지는 공기 순환량을 감소시키는 것이 안정적인 발전소 운영을 하는 것임을 확인하였다.

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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.

나프탈렌 포화공기가 분사되는 막냉각 홀을 가진 터빈 블레이드 표면의 열/물질전달 계수 측정 (Heat/Mass Transfer Measurements on a Film Cooled Blade with Naphthalene Saturated Coolant)

  • 이동현;이동호;김경민;조형희;김범수
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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    • pp.433-436
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    • 2010
  • 본 논문에서는 막냉각홀이 설치된 동익 표면에서의 열/물질전달 특성을 나프탈렌 승화법들 이용해 고찰하였다. 실험에는 저속 환형풍동이 이용되었으며, 풍동 내에는 16개의 동익으로 구성된 터빈단이 설치되어 있다. 동익의 선단부에는 막냉각을 위한 홀이 3열로 배치되어 있으며, 막냉각유체의 분사비를 1.0에서 2.0으로 조절하며 국소 열/물질전달계수를 측정하였다. 전반적인 열/물질전달 계수는 분사비가 높아짐에 따라 증가하며, 박리기포에 의해 압력면에 형성된 낮은 열/물질전달 계수를 갖는 영역은 분사비의 증가와 함께 사라진다.

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가스터빈 발전기 고정자 권선의 절연상태 평가 (Assessment of Insulation Condition in Gas Turbine Generator Stator Windings)

  • 김희동;양규현;주영호
    • 전기학회논문지
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    • 제59권8호
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    • pp.1423-1428
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    • 2010
  • The results of off-line and on-line diagnostic tests performed on the stator winding of an air-cooled gas turbine(G/T) generator are reported in this paper. Off-line diagnostic tests included measurements of the ac current, dissipation factor(tan${\delta}$), and partial discharge(PD). Six epoxy-mica capacitors were installed in the three phases of G/T generator for performing on-line diagnostic testing with the turbine generator analyzer(TGA). The TGA showed that the normalized quantity number(NQN) and the PD magnitude($Q_m$) were high in phase A of the stator winding. Internal discharges were generated in phases B and C, and slot discharge occurred in phase A. According to the trend analyses of the NQN and $Q_m$ values available for insulation condition assessment for G/T generator stator windings, it was concluded that phases B and C were in good condition, whereas phase A has been significantly deteriorated.

원통형과 변형된 분사홀을 갖는 터빈 블레이드의 막냉각 특성에 관한 연구 (Studies on the Film Cooling Characteristics of Turbine Blade Cylindrical and Shaped Holes)

  • 김성민;김윤제;조형희
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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    • pp.334-338
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    • 2001
  • In order to investigate the effects of various injection hole shapes on the film cooling of turbine blade, three test models having cylindrical and shaped holes were used. A three-dimensional Navier-Stokes code with standard k-$\epsilon$ model was used to compute the film cooling coefficient on the film cooled turbine blade. Over 330,000 grids were used to compute the flow over the blade. Mainstream Reynolds number based on the cylinder diameter was $7.1{\times}10^4$. The turbulence intensity kept at $5.0\%$ for all inlets. The effect of coolant blowing ratio was studied for various blowing ratios. For each blowing ratios, wall temperatures around the surface of test model were calculated. Temperature was visualized using cartesian cut-cell method to obtain traces of the injected secondary air on the test surface, so we could interpret the film effectiveness as temperature distributions.

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대용량 터빈발전기 고정자 권선의 정지중 및 운전중 부분방전 특성 (Off-Line and On-Line Partial Discharge Properties of Large Turbine Generator)

  • 김희동;이영준
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2000년도 하계학술대회 논문집 C
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    • pp.1846-1849
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    • 2000
  • Off-line and on-line partial discharges were measured on a 828MVA, 22kV and direct hydrogen-cooled large turbine generator. Partial discharge tests were conducted using digital partial discharge detector(PDD) and turbine generator analyzer(TGA). PDD and TGA showed that off-line partial discharge pattern seems to be very, similar to that found with on-line. Most of the partial discharge is originating with the stator slot in the three phases. As the partial discharge activity is very low, the stator insulation condition of this generator is very good.

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1600K급 가스터빈 연소실에서의 열특성 해석 (Thermal Characteristics in a Gas Turbine Combustion Liner with Firing Temperature of 1600K)

  • 윤남건;김경민;전윤흥;이동현;조형희;김문영
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2008년도 추계학술대회B
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    • pp.2984-2988
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    • 2008
  • Numerical analyses are carried out in order to understand complex thermal characteristics of a gas turbine combustor liner such as combustion gas temperatures, wall temperatures and heat transfer distributions. As results, The maximum internal and external heat transfer is $2218W/m^2K$ and $2358W/m^2K$, respectively. The combustion gas temperatures range is 673K to 1760K. A range of temperature on TBC is 676K to 1382K. Lastly, temperature range on outer surface of combustion liner cooled by compressed air is 676K to 1188K.

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