Project No: FE0005540
Performer: University of Texas at Austin
Richard A. Dennis Technology Manager, Turbines National Energy Technology Laboratory 3610 Collins Ferry Road P.O. Box 880 Morgantown, WV 26507-0880 304-285-4515 firstname.lastname@example.org Robin Ames Project Manager National Energy Technology Laboratory 3610 Collins Ferry Road P.O. Box 880 Morgantown, WV 26507-0880 304- 285-0978 email@example.com David G. Bogard Principal Investigator University of Texas at Austin Department of Mechanical Engineering 1 University Station C2200 Austin, TX 78712 512-471-3128 firstname.lastname@example.org
DOE Share: $500,000.00
Performer Share: $127,802.00
Total Award Value: $627,802.00
Performer website: University of Texas at Austin - http://www.utexas.edu
Wind tunnel facilities at The Pennsylvania State University (Penn State) and University of Texas at Austin (UT) have been specifically designed to simulate film cooling of turbine vanes, blades, and endwalls. These facilities incorporate equipment that simulates the deposition of contaminants in the turbine by using molten wax particles to simulate the molten contaminant particles that occur at actual engine conditions. The wax particles used in the test facilities are sized appropriately to simulate the inertial behavior of particles that exist in engine conditions. The use of wax also allows for the simulation of the liquid-to-solid phase change that is essential to the primary deposition mechanism.
UT will be focusing on the performance of shallow trench film cooling configurations for various positions on the suction and pressure sides of a simulated vane with active deposition. Meanwhile, Penn State will be investigating the effect of active deposition on various endwall cooling configurations. Preliminary results show that deposition could be simulated dynamically using wax and that the effects of deposition could be quantified using infrared thermography. New endwall and vane surface film cooling configurations will be developed to minimize deposition and maximize cooling performance under contaminated conditions.
The combined cooling effects of TBC (Thermal Barrier Coating) and film cooling are shown in the distributions of overall cooling effectiveness, f, presented here for no TBC, moderate thickness TBC, and thick TBC.
Program Background and Project Benefits
This project will utilize wind tunnel facilities to simulate film cooling of turbine vanes, blades, and endwalls using molten wax. Turbine aerodynamics and heat transfer research will develop advanced cooling technology that will allow for higher firing temperatures which translate into increased cycle efficiency. Specifically, this project will analyze the wax particle depostion for shallow trench cooling configurations of a simulated vane and various endwall cooling configurations using infrared thermography.