Flow Characteristics in Two-Leg Internal Coolant Passages of Gas Turbine Airfoils With Film-Cooling Hole Ejection

Author:

Chanteloup D.1,Bo¨lcs A.1

Affiliation:

1. Ecole Polytechnique Fe´de´rale de Lausanne (EPFL), Laboratoire de Thermique applique´e et de Turbomachines (LTT), 1015 Lausanne, Switzerland

Abstract

A study of flow in two stationary models of two-pass internal coolant passages is presented, which focuses on the flow characteristics in the 180-deg bend region, and downstream of the bend, where the flow is redeveloping. A stereoscopic digital PIV system measured all three velocity components simultaneously to obtain mean velocity, and turbulence quantities of the flow field. The coolant passage model consisted of two square passages, each having a 20 hydraulic diameter length, separated by a rounded-tip web of 0.2 passage widths, and connected by a sharp 180-deg bend with a rectangular outer wall. Ribs were mounted on the bottom and top walls of both legs, with a staggered arrangement, and at 45 deg to the flow. The rib height and spacing were 0.1 and 1.0 passage heights, respectively. The measurements were obtained for a flow condition, with a Reynolds number of 50,000. The geometries are similar in both sections except for one, which is equipped with extraction holes to simulate holes for film cooling. Two series of holes are placed solely in the bottom wall, four holes are located in the bend, and 12 in the downstream leg. The global extraction through the holes was set to 50% of the inlet massflow. This paper presents new measurements of the flow in the straight legs, as well as in the bend of the passage equipped with holes, detailed comparison of the flow upstream, inside and downstream of the bend region between both configurations, and the effects of extraction inside the cooling channels.

Publisher

ASME International

Subject

Mechanical Engineering

Reference20 articles.

1. Rowbury, D., Parneix, S., Chanteloup, D., and Lees, A., 2001, Research into the influence of Rotation on the Internal Cooling Turbine Blades, Proc. AVT Symposium, Heat Transfer and Cooling in Propulsion and Power Systems, Loen, Norway.

2. Rau, G., Cakan, M., Moeller, D., and Arts, T., 1998, “The Effect of Periodic Ribs on the Local Aerodynamic and Heat Transfer Performance of a Straight Cooling Channel,” ASME J. Turbomach., 120, pp. 368–375.

3. Schabacker, J., 1998, “PIV Investigation of the Flow Characteristics in an Internal Coolant Passages of Gas Turbine Airfoils With Two Ducts Connected by a Sharp 180 deg Bend,” Ph.D. thesis (Ecole Polytechnique fede´rale de Lausanne), Vol. no. 1816.

4. Chanteloup, D., and Bo¨lcs, A. 2001, “PIV Investigation of the Flow Characteristics in 2-Leg Internal Coolant Passages of Gas Turbine Airfoils,” Proc. Euroturbo, 4th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics. Firenze, Italy.

5. Bons, J. P., and Kerrebrock, J. L., 1999, “Complementary velocity and heat transfer measurements in a rotating cooling passage with smooth walls,” ASME J. Turbomach., 121, pp. 651–662.

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3