Abradable Sealing Materials for Emerging IGCC-Based Turbine System Email Page
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Performer: Regents of the University of California
Schematic of a section through a gas turbine engine<br/>high-pressure stage showing where an abradable coating<br/>is used and how gas leaks through this seal lead to performance loss.
Schematic of a section through a gas turbine engine
high-pressure stage showing where an abradable coating
is used and how gas leaks through this seal lead to performance loss.
Website: University of California, Irvine
Award Number: FE0011929
Project Duration: 08/15/2013 – 08/31/2017
Total Award Value: $625,000
DOE Share: $500,000
Performer Share: $125,000
Technology Area: Advanced Turbines
Key Technology: Advanced Combustion Turbines
Location: Irvine, California

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