Improving Durability of Turbine Components Through Trenched Film Cooling and Contoured Endwalls Email Page
email
Print This Page
print
Performer: 
University of Texas at Austin
The combined cooling effects of TBC (Thermal Barrier<br/>Coating) and film cooling are shown in the distributions of<br/>overall cooling effectiveness, f, presented here for<br/>no TBC, moderate thickness TBC, and thick TBC.
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.
Website:  University of Texas at Austin
Award Number:  FE0005540
Project Duration:  10/01/2010 – 09/30/2014
Total Award Value:  $627,802.00
DOE Share:  $500,000.00
Performer Share:  $127,802.00
Technology Area:  Hydrogen Turbines
Key Technology:  Hydrogen Turbines
Location:  Austin, Texas

Presentations, Papers, and, Publications


Back