• 제목/요약/키워드: Transfer Ratio

검색결과 2,123건 처리시간 0.036초

터빈 블레이드 냉각시스템에 관한 수치해석적 연구 (NUMERICAL STUDY OF TURBINE BLADE COOLING TECHNIQUES)

  • 김광용;이기돈;문미애;허만웅;김현민;김진혁
    • 한국전산유체공학회:학술대회논문집
    • /
    • 한국전산유체공학회 2010년 춘계학술대회논문집
    • /
    • pp.530-533
    • /
    • 2010
  • This paper presents numerical analysis and design optimization of various turbine blade cooling techniques with three-dimensional Reynolds-averaged Navier-Stokes(RANS) analysis. The fluid flow and heat transfer have been performed using ANSYS-CFX 11.0. A fan-shaped hole for film-cooling has been carried out to improve film-cooling effectiveness with the radial basis neural network method. The injection angle of hole, lateral expansion angle of hole and ratio of length-to-diameter of the hole are chosen as design variables and spatially averaged film-cooling effectiveness is considered as an objective function which is to be maximized. The impingement jet cooling has been performed to investigate heat transfer characteristic with geometry variables. Distance between jet nozzle exit and impingement plate, inclination of nozzle and aspect ratio of nozzle hole are considered as geometry variables. The area averaged Nusselt number is evaluated each geometry variables. A rotating rectangular channel with staggered array pin-fins has been investigated to increase heat transfer performance ad to decrease friction loss using KRG modeling. Two non-dimensional variables, the ratio of the eight diameter of the pin-fins and ratio of the spacing between the pin-fins to diameter of the pin-fins selected as design variables. A rotating rectangular channel with staggered dimples on opposite walls are formulated numerically to enhance heat transfer performance. The ratio of the dimple depth and dimple diameter are selected as geometry variables.

  • PDF

종횡비가 다른 납작관 내 응축열전달 및 압력손실 (Condensation Heat Transfer and Pressure Drop in Flat Tubes with Different Aspect Ratios)

  • 김내현;박지훈;차상진
    • 대한기계학회논문집B
    • /
    • 제34권12호
    • /
    • pp.1111-1119
    • /
    • 2010
  • 본 연구에서는 내경 5.0mm 원관을 납작하게 한 납작관에 대하여 R-410A 를 사용하여 응축열전달 실험을 수행하였다. 실험은 포화온도와 열유속을 각각 $45^{\circ}C$ 와 10kW/$m^2$으로 고정한 상태에서 질량유속과 건도를 변화시키며 수행되었다. 실험결과 납작관의 종횡비가 열전달계수에 미치는 영향은 유동양식에 따라 달리 나타났다. 환상류에서는 종횡비가 증가할수록 증가하고 성층류에서는 종횡비가 증가할수록 감소하였다. 한편 납작관의 마찰손실은 종횡비가 증가할수록 증가하였다. 기존 상관식들은 납작관의 열전달계수와 마찰계수를 적절히 예측하였다.

곡관부를 가지는 내부 냉각유로에서 회전수 변화에 따른 열전달 및 유동 특성 ( I ) - 엇갈린 요철배열 덕트 - (Effects of Rotation Speed on Heat Transfer and Flow in a Coolant Passage with Turning Region ( I ) - Cross Ribbed Duct -)

  • 김경민;김윤영;이동호;조형희
    • 대한기계학회논문집B
    • /
    • 제29권6호
    • /
    • pp.737-746
    • /
    • 2005
  • The present study investigates heat/mass transfer and flow characteristics in a ribbed rotating passage with turning region. The duct has an aspect ratio (W/H) of 0.5 and a hydraulic diameter ($D_h$) of 26.67 mm. Rib turbulators are attached in the cross arrangement on the leading and trailing surfaces of the passage. The ribs have a rectangular cross section of $2\;mm\;(e){\times}\;mm\;(w)$ and an attack angle of $70^{\circ}$. The pitch-to-rib height ratio (p/e) is 7.5, and the rib height-to-hydraulic diameter ratio ($e/D_h$) is 0.075. The rotation number ranges from 0.0 to 0.20 while the Reynolds number is constant at 10,000. To verify the heat/mass transfer augmentation, internal flow structures are calculated for the same conditions using a commercial code FLUENT 6.1. The heat transfer data of the smooth duct for various Ro numbers agree well with not only the McAdams correlation but also the previous studies. The cross-rib turbulators significantly enhance heat/mass transfer in the passage by disturbing the main flow near the surfaces and generating one asymmetric cell of secondary flow skewing along the ribs. Because the secondary flow is induced in the first-pass and turning region, heat/mass transfer discrepancy is observed in the second-pass even for the stationary case. When the passage rotates, heat/mass transfer and flow phenomena change. Especially, the effect of rotation is more dominant than the effect of the ribs at the higher rotation number in the upstream of the second-pass.

Transfer case의 구동변환을 위한 유성기어장치 구동부 설계 (Design of Planetary Gear Drive Unit for Drive Conversion of Transfer case)

  • 염광욱
    • 한국가스학회지
    • /
    • 제26권2호
    • /
    • pp.21-26
    • /
    • 2022
  • 사륜구동은 구동력을 4바퀴에 모두 전달하기 때문에 노면과의 접지력이 상승하여 구동력이 상승한다. 하지만 그로 인해 연비가 저하되는 단점을 가지고 있다. 따라서 평소에 이륜구동으로 주행하다가 필요에 의해 선택적 사륜구동으로 변환하는 방법으로 사륜구동을 많이 사용한다. 이러한 선택적 사륜구동은 운전자가 보내는 전기적 신호를 Transfer case에서 기계적으로 바꿔서 구동력을 변환시킨다. 본 연구에서는 전기적 신호를 기계적으로 바꿔주기 위해 모터에 감속기를 적용하여 토크를 증대시켜 기능을 수행하였다. 따라서, 본 연구에서는 구동을 변환시켜주기 위해 적용되는 Transfer case내부에 있는 모터에 적용할 수 있는 감속메커니즘을 도출하고 그에 따른 유성기어형태를 적용한 감속비를 최적화하였다. 그리고 도출된 감속비를 토대로 링기어를 공통으로 사용하는 유성기어 2세트를 적용하여 입력축과 출력축이 동일상에서 감속이 진행되는 유성기어 기어치형의 개발 및 Transfer csae 내에 있는 구동변환장치 구동부의 최적화 설계를 진행하였다.

단섬유 복합체에서 탄성계수비가 내부응력에 미치는 영향 (Effects of Elastic Modulus Ratio on Internal Stresses in Short Fiber Composites)

  • 김홍건;노홍길
    • 한국공작기계학회논문집
    • /
    • 제13권4호
    • /
    • pp.73-78
    • /
    • 2004
  • The conventional SLT(Shear Lag Theory) which has been proven that it can not provide sufficiently accurate strengthening predictions in elastic regime when the fiber aspect ratio is small. This paper is an extented work to improve it by modifying the load transfer mechanism called NSLT(New Shear Lag Theory), which takes into account the stress transfer across the fiber ends and the SCF(Stress Concentration Factor) that exists in the matrix regions near the fiber ends. The key point of the model development is to determine the major controlling factor among the material and geometrical coefficients. It is found that the most affecting factor is the fiber/matrix elastic modulus ratio. It is also found that the proposed model gives a good result that has the capability to correctly predict the elastic properties such as interfacial shear stresses and local stress variations in the small fiber aspect ratio regime.

충돌수분류(衝突水噴流)에 의한 Semi-cylinder면(面)에서의 열전달(熱傳達)에 관(關)한 실험적(實驗的) 연구(硏究) (An Experimental Study on Heat Transfer of Semi-cylindrical Surface by Impinging Water Jet)

  • 염기찬;최국광;서정윤
    • 대한설비공학회지:설비저널
    • /
    • 제17권6호
    • /
    • pp.708-716
    • /
    • 1988
  • Local heat transfer coefficients were measured on semi-cylinders on which a circular water jet impinged in crossflow. The ratio of the semi-cylinder's diameter and the nozzle outlet diameter were varied parametrically, as were the Reynolds number and the supplementary water heights. The measurements showed that the circumferential distribution of the heat transfer coefficient peaked at the stagnation point. For a fixed supplementary water height, the peak heat transfer coefficient was not depend on the curvature of test specimen(d/D). Optimum height of supplementary water which brought about the augmentation of heat transfer at the stagnation point was S/D=1. The Nusselt number decreased as the circumferential distance or angle increased. The circumferential distribution of dimensionless heat transfer (Nu/Nus) was independent of d/D ($d/D{\geq}8.33$), but for the d/D<8.33, it was depended on d/D. At a fixed angle of specimen, dimensionless heat transfer (Nu/Nus) decreased as the ratio d/D increased. The extent of the decrease between d/D=6.67 and 8.33 was markedly greater than that between d/D=8.33 and 10, or d/D=10 and 11.67.

  • PDF

가스터빈용 열교환기의 주름진 덕트에서 종횡비 변화가 열전달 특성에 미치는 영향 (Effects of Duct Aspect Ratio on Heat Transfer in Wavy Duct of Heat Exchanger of Gas Turbine)

  • 김한호;황상동;조형희;최재호;전승배
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
    • /
    • pp.339-344
    • /
    • 2001
  • The present study investigates convective heat/mass transfer and flow characteristics in wavy ducts of primary surface heat exchanger. Experiments using a naphthalene technique are carried out to determine the local transfer characteristics for flow in the corrugated wall duct. The aspect ratios of the rectangular duct cross-section are 7.3, 4.7 and 1.8 with a corrugation angle of $145^{\circ}$. The Reynolds numbers, based on the duct hydraulic diameter, are ranged from 1000 to 5000. The local heat/mass transfer measurement is conducted in the spanwise directions. The results show that Tayler-Gortler vortices exist on the pressure surface. Flow separation on the suction surface appears at a high Reynolds number resulting in a sharp decrease in the local transfer rates, but relatively high transfer rates are obtained in the reattachment region.

  • PDF

응축용 특수 전열관의 열전달 특성에 관한 연구 (Experimental Study on Condensation Heat Transfer Characteristics of Special Heat Transfer Tubes)

  • 한규일;박종운;권영철;조동현
    • 설비공학논문집
    • /
    • 제13권9호
    • /
    • pp.827-835
    • /
    • 2001
  • In this study, condensation heat transfer characteristics were conducted with special heat transfer tubes of SH-C type. Experiments were carried out the saturated vapor temperature of 334K and the wall subcooling of 1.5-4.5K. The refrigerant was R-113 and the enhanced tubes used in the present study were SH-CDR, SH-CYR and SH-CHR. The experimental results showed that the condensation heat transfer coefficients of SH-C type tubes were about 23-66% higher than those of a low integral-fin tube. It was visualized that the condensed liquid on the outer surface of SH-C type tubes flowed continuously down unlike a low integral-fin tube and a plain tube, due to a 3-D extending fin on the outer surface of SH-C type tubes. As a result, the thermal resistance of the condensed liquid decreased and the heat transfer coefficient increased. Also, the enhancement ratio of SH-CDR tube was the highest, and it was about 9-11 times as compared to that of a plain tube.

  • PDF

Shear strength analysis and prediction of reinforced concrete transfer beams in high-rise buildings

  • Londhe, R.S.
    • Structural Engineering and Mechanics
    • /
    • 제37권1호
    • /
    • pp.39-59
    • /
    • 2011
  • Results of an experimental investigation on the behavior and ultimate shear capacity of 27 reinforced concrete Transfer (deep) beams are summarized. The main variables were percent longitudinal(tension) steel (0.28 to 0.60%), percent horizontal web steel (0.60 to 2.40%), percent vertical steel (0.50to 2.25%), percent orthogonal web steel, shear span-to-depth ratio (1.10 to 3.20) and cube concrete compressive strength (32 MPa to 48 MPa).The span of the beam has been kept constant at 1000 mm with100 mm overhang on either side of the supports. The result of this study shows that the load transfer capacity of transfer (deep) beam with distributed longitudinal reinforcement is increased significantly. Also, the vertical shear reinforcement is more effective than the horizontal reinforcement in increasing the shear capacity as well as to transform the brittle mode of failure in to the ductile mode of failure. It has been observed that the orthogonal web reinforcement is highly influencing parameter to generate the shear capacity of transfer beams as well as its failure modes. Moreover, the results from the experiments have been processed suitably and presented an analytical model for design of transfer beams in high-rise buildings for estimating the shear capacity of beams.

모듈형 편평원관군 열교환기의 열전달 특성 해석 (Analysis of Geometrical Effects on Heat Transfer Characteristics in a Modular Flat Tube-Bundle Heat Exchanger)

  • 박병규;이준식
    • 설비공학논문집
    • /
    • 제17권11호
    • /
    • pp.1014-1021
    • /
    • 2005
  • Flow channels with non-circular cross-sections are encountered in a wide variety of heat exchangers. Accurate friction factor and Colburn j factor data are essential for the design and viable applications of such heat exchangers. In this study, an analysis is con ducted on heat transfer and pressure drop characteristics for tube-bundle heat exchanger with various arrangements of tubes, of which their geometry could easily be modified from a circular one in a harsh environment. The parameters investigated are aspect ratio, pitch, and inclined angle of tubes. The results obtained are: (1) Aspect ratio has larger influence on the j and f factor than pitch; (2) As aspect ratio increases, both j and f factors decrease; (3) The high performance is achieved when the pitch and aspect ratio are in the range of 1.5${\~}$2.5 and 1.25${\~}$2.0, respectively; and (4) the inclined arrangements of tubes show unfavorable results for both heat transfer and pressure drop characteristics in spite of the positive possibility of condensate removals in a latent heat recovery system.