• 제목/요약/키워드: Annular region

검색결과 79건 처리시간 0.045초

베인과 블레이드 사이의 상대위치 변화에 따른 터빈 블레이드 표면에서의 열/물질전달 특성 (Effect of Relative Position of Vane and Blade on Heat/Mass Transfer Characteristics on Stationary Turbine Blade Surface)

  • 이동호;조형희
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
    • /
    • pp.140-150
    • /
    • 2004
  • In this study, the effect of relative position of the blade for the fixed vane has been investigated on blade surface heat transfer. The experiments were conducted in a low speed stationary annular cascade, and heat transfer of blade was examined for six positions within a pitch. Turbine test section has one stage composed of sixteen guide vanes and blades. The chord length of the tested blade is 150 mm and the mean tip clearance of the blade having flat tip is about $2.5\%$ of the blade chord. For the detailed mass transfer measurements on the blade surfaces, a naphthalene sublimation technique was used. The inlet flow Reynolds number is fixed to $1.5{\times}10^5$. Complex heat transfer characteristics are observed on the blade surface due to various flow characteristics, such as separation bubble, relaminarization, transition to turbulence and leakage vortices. The distributions of velocity and turbulence intensity change significantly with the relative position due to the blockage effect of the blade. This causes the variation of heat transfer patterns on the blade surface. The results show that the flow near the leading edge get highly disturbed and deflected toward the either side of the blade when the blade leading edge is positioned close to the trailing edge of the vane. Therefore, separation bubble disappears on the pressure side and overall heat transfer on the relaminarization region is increased. But, due to reduced tip gap flow at the upstream region, the effect of leakage flow on the upstream region of the blade surface is weakened. Thus, the heat transfer characteristics significantly change with the blade positions.

  • PDF

모형가스터빈 연소기에서 분무각 변화에 따른 연료농도 및 화염온도 분포 (Fuel Concentration and Flame Temperature Distribution in Model Gas Turbine Combustor with Various Spray Angles)

  • 황진석;변용우;성홍계;구자예;강정식
    • 한국항공우주학회지
    • /
    • 제36권10호
    • /
    • pp.1011-1016
    • /
    • 2008
  • KIVA3V를 이용하여 모형 가스터빈 연소기에서 Jet-A의 분무와 연소에 관한 수치해석을 하였다. 연소기 형상은 6개의 희석홀을 가지며, 스월효과를 고려하였다. 연소 특성을 해석하기 위해 열적 NO 발생을 고려하였다. 다양한 분무각에 대해서 Jet-A 증기, 화염온도 분포와 NO 발생량에 대하여 비교하였다. 분무각이 커질수록 1차 영역에서 연료 증기가 비교적 고르게 나타나게 되며 증발이 더욱 빠르게 되고, 주변 기체와 연료 증기 사이의 혼합이 증가한다. 그 결과 고온부가 넓게 나타나게 되고, 이에 의해 열적 NO 발생이 증가한다.

형상변화 에 의한 열교환기 의 열전달 성능 향상 (II) (The Improvement of the Heat Exchanger Performance by Shape Modifieation(II))

  • 노승탁;이택식;강신형;이은현;송명호
    • 대한기계학회논문집
    • /
    • 제9권2호
    • /
    • pp.202-212
    • /
    • 1985
  • 본 논문에서는 이러한 연구의 첫단계로 Gosman과 Ideriah가 다룬 TEACH-2E전 산프로그램을 모체로 하여 본 논문의 문제에 적합하도록 수정하여 사용하였다. 그러 나 기본적인 k-.epsilon.난류모델은 수정하지 않았다. 한편, 본 논문에서는 열선풍속계를 이용하여 평균 속도분포 및 난류특성을 계측하고 계산결과와 비교하였다. 이를 통하 여 표준형 k-.epsilon.모델을 이용한 TEACH-2E코드의 특성을 파악하고 이를 위한 실험 데이터 를 확보하는데 중점을 두었다.

입사각 변화에 따른 터빈 블레이드에서의 열전달 특성 변화 (I) - 블레이드 끝단면 - (Effect of Incidence Angle on Turbine Blade Heat Transfer Characteristics (I) - Blade Tip -)

  • 이동호;조형희
    • 대한기계학회논문집B
    • /
    • 제31권4호
    • /
    • pp.349-356
    • /
    • 2007
  • The present study investigated local heat/mass transfer characteristics on the tip of the rotating turbine blade with various incoming flow incidence angles. The experiments are conducted in a low speed annular cascade with a single stage turbine. The blade has a flat tip with a mean tip clearance of 2.5% of the blade chord. The incoming flow Reynolds number is $1.5{\times}10^5$ at design condition. To examine the effect of off-design condition, the experiments with various incidence angles ranging between $-15^{\circ}$ and $+7{\circ}$ were conducted. A naphthalene sublimation method is used to measure detailed mass transfer coefficient on the blade. The results indicated that the incidence angle strongly affects the behavior of tip leakage flow around the blade tip and consequently plays an important role in determining heat transfer characteristics on the tip. For negative incidence angles, the heat/mass transfer in the upstream region on the tip decreases by up to 20%. On the contrary, for positive incidence angles, much higher heat transfer coefficients are observed even with small increase of incidence angle.

소형펀치 크리프 시험중 측정하는 변수에 대한 연구 (A Study on Parameters Measured during Small Punch Creep Testing)

  • 박태규;심상훈;윤기봉;장창희
    • 대한기계학회논문집A
    • /
    • 제26권1호
    • /
    • pp.171-178
    • /
    • 2002
  • An effect is made in this study to deepen understanding of small punch(SP) creep testing which has been a round for about 10 years as a substitute for the conventional uniaxial creep testing. Even though considerable numbers of SP creep test program have been performed, most of the tests were aimed at measuring creep rupture lives only. Very flew studies showed interest on the meaning of what we were really measuring during the SP creep tests. In this paper meanings of the parameters measured during the SP creep testing, such as punch load and punch displacement rate are investigated using finite element analysis. It was shown that the measured parameters must represent the stress and strain rates of the material at the annular region located at about 0.65 mm from the center of the SP specimen. The material in this location would go through constant maximum stress and strain rate during the testing. Experimental verification is also discussed.

접선형 산화제 주입기의 운동량비에 따른 End-Burning 하이브리드 연소기의 연소유동장 해석 (Reactive Fields Analysis of End-Burning Hybrid Combustor Using Tangential Oxidizer Injectors with Various Momentum Ratio)

  • 민문기;김수종;김진곤;문희장
    • 한국추진공학회지
    • /
    • 제11권2호
    • /
    • pp.37-46
    • /
    • 2007
  • 본 연구에서는 접선형 산화제 주입기를 갖는 end-burning 하이브리드 연소기에서 산화제 운동량비에 따른 연소 유동장을 해석하였다. 산화제의 운동량비가 감소할수록 연소효율은 연소기 전 영역에 걸쳐 증대되는 경향이 포착되었으며 이론 혼합분율과 온도장을 통해 연소실 전 영역에서 최적의 연소가 저 운동량비에서 발생됨을 확인하였다. 강한 선회류가 연소실 내부 유동장을 지배하지만 압력장은 비교적 균일한 분포를 보였다. 접선형 산화제 주입기를 가진 연소기는 운동량비에 관계없이 공통적으로 연료와 산화제가 만나는 연소실 상부에서 환형의 고온부가 발생했으며 향후 주요 개선 사항으로 판단되었다.

개에서 발생한 결장직장 선암종 1례 (Colorectal Adenocarcinoma in a Dog)

  • 최호정;안지영;오이세;정성목;박성준;조성환;이영원
    • 한국임상수의학회지
    • /
    • 제25권5호
    • /
    • pp.429-433
    • /
    • 2008
  • An 8-year-old, female Pointer dog was presented with weight loss, hematochezia, and dyschezia. For the diagnosis, physical examination, complete blood counts, serum chemistry, radiography, ultrasonography, computed tomography, colonoscopy, cytology and histopathological examination were performed. The complete blood counts and serum biochemistry results were within the reference range. Ultrasonographic findings were presented with the thickened wall of the colon and rectum. Colonoscopy revealed irregular and ulcerated mucosal surface, mass and luminal narrowing of colorectal lesions. There were thickened wall and contrast enhancement of the lesion in colorectal region on the computed tomography. The cytologic examination suggested the adenocarcinoma. Postmortem histopathologic examination revealed adenocarcinoma. Based on these findings, the dog was diagnosed with annular colorectal adenocarcinoma.

4방향 스풀밸브의 중립특성에 관한 연구 (A Study on Null Characteristics of 4-way Spool Valve)

  • 함영복;윤소남;이근호;김성동
    • 한국정밀공학회지
    • /
    • 제17권8호
    • /
    • pp.165-171
    • /
    • 2000
  • In this study the 4-way spool valve characteristics are clearly defined and clearly defined and proposed new type of spool valve. This paper presents governing equations of the flow through clearances between sleeve and spool as a model of orifice flow for null characteristics analysis and programmed analysis software of it. This software is possible to basically analysis that not only which case of open center closed center or critical center but _ -displacement of spool lab position boundary region and spool opening of the valve and to estimate the pressure variation in the spool and external leak flow variation. We are convinced that the scale of load pressure difference is changed as lab condition of valve and this scale is changed with boundary point on the annular clearance. It is vary useful to designer and user of spool valve with this design data and analysis software.

  • PDF

Reset-first Resistance Switching Mechanism of HfO2 Films Based on Redox Reaction with Oxygen Drift-Diffusion

  • Kim, Jong-Gi;Lee, Sung-Hoon;Lee, Kyu-Min;Na, Hee-Do;Kim, Young-Jae;Ko, Dae-Hong;Sohn, Hyun-Chul
    • 한국진공학회:학술대회논문집
    • /
    • 한국진공학회 2012년도 제42회 동계 정기 학술대회 초록집
    • /
    • pp.286-287
    • /
    • 2012
  • Reset-first resistive switching mechanism based on reduction reaction in HfO2-x with oxygen drift-diffusion was studied. we first report that the indirect evidence of local filamentary conductive path formation in bulk HfO2 film with local TiOx region at Ti top electrode formed during forming process and presence of anion-migration at interface between electrode and HfO2 during resistive switching through high resolution transmission electron microscopy (HRTEM), electron disperse x-ray (EDX), and electron energy loss spectroscopy (EELS) mapping. Based on forming process mechanism, we expected that redox reaction from Ti/HfO2 to TiOx/HfO2-x was responsible for an increase of initial current with increasing the post-annealing process. First-reset resistive switching in above $350^{\circ}C$ annealed Ti/HfO2 film was exhibited and the redox phenomenon from Ti/HfO2 to TiOx/HfO2-x was observed with high angle annular dark field (HAADF) - scanning transmission electron microscopy (STEM), EDX and x-ray photoelectron spectroscopy. Therefore, we demonstrated that the migration of oxygen ions at interface region under external electrical bias contributed to bipolar resistive switching behavior.

  • PDF

고정된 터빈 블레이드의 베인에 대한 상대위치 변화가 끝단면 및 슈라우드의 열/물질전달 특성에 미치는 영향 (Effect of Vane/Blade Relative Position on Heat/Mass Transfer Characteristics on the Tip and Shroud for Stationary Turbine Blade)

  • 이동호;조형희
    • 대한기계학회논문집B
    • /
    • 제30권5호
    • /
    • pp.446-456
    • /
    • 2006
  • The effect of relative position of the stationary turbine blade for the fixed vane has been investigated on blade tip and shroud heat transfer. The local mass transfer coefficients were measured on the tip and shroud fur the blade fixed at six different positions within a pitch. A low speed stationary annular cascade with a single turbine stage was used. The chord length of the tested blade is 150 mm and the mean tip clearance of the blade having flat tip is 2.5% of the blade chord. A naphthalene sublimation technique was used for the detailed mass transfer measurements on the tip and the shroud. The inlet flow Reynolds number based on chord length and incoming flow velocity is fixed to $1.5{\times}10^5$. The results show that the incoming flow condition and heat transfer characteristics significantly change when the relative position of the blade changes. On the tip, the size of high heat/mass transfer region along the pressure side varies in the axial direction and the difference of heat transfer coefficient is up to 40% in the upstream region of the tip because the position of flow reattachment changes. On shroud, the effect of tip leakage vortex on the shroud as well as tip gap entering flow changes as the blade position changes. Thus, significantly different heat transfer patterns are observed with various blade positions and the periodic variation of heat transfer is expected with the blade rotation.