Turbines Project Information
Advanced Combustion Turbines
Agreement Number Project Title Performer Name
FE0011722 Microstructure Sensitive Crystal Viscoplasticity for Ni-Base Superalloys Georgia Tech Research Corporation
FE0011762 Evaluation of Flow and Heat Transfer Inside Lean Pre-Mixed Combustor Systems Under Reacting Flow Conditions Virginia Polytechnic Institute and State University 
FE0011778 High-Pressure Turbulent Flame Speeds and Chemical Kinetics of Syngas Blends with and without Impurities Texas Engineering Experiment Station
FE0011796 New Mechanistic Models of Creep-Fatigue Interactions for Gas Turbine Components Purdue University
FE0011822 Effects of Exhaust Gas Recirculation (EGR) on Turbulent Combustion and Emissions in Advanced Gas Turbine Combustors with High-Hydrogen-Content (HHC) Fuels Purdue University
FE0011875 Thermally Effective and Efficient Cooling Technologies for Advanced Gas Turbines University of North Dakota
FE0011929 Abradable Sealing Materials for Emerging IGCC-Based Turbine System University of California, Irvine
FE0012005 An Experimental and Modeling Study of NOx-CO Formation in High Hydrogen Content Fuels Combustion in Gas Turbine Applications University of South Carolina
FE0012053 Predictive Large Eddy Simulation Modeling and Validation of Turbulent Flames and Flashback in Hydrogen Enriched Gas Turbines University of Texas at Austin
FE0023955 Ceramic Matrix Composite Advanced Transition for 65% Combined Cycle Siemens Energy
FE0023965 Advanced Multi-Tube Mixer Combustion for 65% Efficiency General Electric Company
FE0024006 High Temperature CMC Nozzles for 65% Efficiency General Electric
FE0025011 Improving Turbine Efficiencies Through Heat Transfer and Aerodynamic Research in the Steady Thermal Aero Research Turbine (START) Pennsylvania State University
FE0025320 Revolutionizing Turbine Cooling with Micro-Architectures Enabled by Direct Metal Laser Sintering Ohio State University
FE0025344 High Temperature Low Nox Combustor Concept Development Georgia Tech
FE0025495 Understanding Transient Combustion Phenomena in Low-NOx Gas Turbines Pennsylvania State University
FE0025793 Design, Fabrication and Performance Characterization of Near-Surface Embedded Cooling Channels (NSECC) with an Oxide Dispersion Strengthened (ODS) Coating Layer University of Pittsburgh
FWP-2012.03.02 Turbine Thermal Management NETL-ORD
FWP-AL05205018 Analysis of Gas Turbine Thermal Performance Ames National Laboratory
SC0004356 High Temperature Unique Low Thermal Conductivity Thermal Barrier Coating (TBC) Architectures UES Inc.
SC0007544 Ultra-High Temperature Thermal Barrier Coatings HiFunda, LLC
SC0008218 Air-Riding Seal Technology for Advanced Gas Turbine Engines Florida Turbine Technologies Inc.
SC0009592 Computational Materials Design of Castable SX Ni-based Superalloys for IGT Blade Components QuesTek Innovations LLC
SC0010175 Rapid Manufacturing Method for High-Temperature Turbine Components Mikro Systems Inc.
SC0011335 Durable High Temperature Coatings for Utility Scale Gas Turbine Hot Gas Path Components UES, Inc.
SC0013098 Advanced Bond Coats for Thermal Barrier Coating Systems Based on High Entropy Alloys Directed Vapor Technologies International Inc.
SC0013220 Exploration of High Entropy Alloys for Turbine Applications QuesTek Innovations LLC
SC0015179 Nanoscale Metal Oxide Coatings for Corrosion Protection of Superalloy Materials Calabazas Creek Research, Inc.
SC0015743 Superalloy MMC Components for Advanced Turbine Systems Advanced Powder Solutions Inc.
SC0015941 A Suite of Ultra High-Temperature Ceramic Components for Advanced Turbine Systems Based on Polymer-Derived Ceramics Sporian Microsystems Inc.

Pressure Gain Combustion
Agreement Number Project Title Performer Name
FE0023983 Rotating Detonation Combustion for Gas Turbines-Modeling and System Synthesis
Aerojet Rocketdyne
FE0025315 A Joint Experimental/Computational Study of Non-Idealities in Practical Rotating Detonation Engines
Regents of the University of Michigan
FE0025343
Advancing Pressure Gain Combustion in Terrestrial Turbine Systems
Purdue University
FE0025525
Effect of Mixture Concentration Inhomogeneity on Detonation Properties in Pressure Gain Combustion
Pennsylvania State University

Supercritical CO2 Turbomachinery
Agreement Number Project Title Performer Name
FE0023998
Advanced Turbomachinery Components for Supercritical CO2 Power Cycles
Institute of Gas Technology
FE0024007 Development of Low-Leakage Shaft End Seals for Utility-Scale Supercritical Carbon Dioxide (SCO2) Turbo Expanders General Electric
FE0024041
High Inlet Temperature Combustor for Direct Fired Supercritical Oxy-Combustion
Southwest Research Institute
FE0025174
Investigation of Autoignition and Combustion Stability of High Pressure Supercritical Carbon Dioxide Oxy-Combustion Georgia Tech
FE0025260
Chemical Kinetic Modeling Development and Validation Experiments for Direct Fired Supercritical CO2 Combustor University of Central Florida
FWP-FEAA123
Advanced Materials Issues in Supercritical Carbon Dioxide
ORNL - Oak Ridge National Laboratory
SC0013691
An Advanced Gas Foil Bearing Using Supercritical Carbon Dioxide as the Working Fluid
Mechanical Solutions, Inc.
SC0015101
Ceramic-Metal Joining by a Novel Flame Processing
NGimat Company
SC0015111
Ceramic-Metal Joining of Components Used at High-Temperature and High Pressure
Physical Sciences Inc.
SC0015118
Novel Materials for Metal to Ceramic Transitions
HiFunda, LLC
SC0015144
Ceramic to Metal Joints
Physical Sciences Inc.
SC0015181
Corrosion and Erosion Resistant Surface Features for High Pressure Supercritical Carbon Dioxide Heat Exchangers
Altex Technologies Corporation
SC0015192
Ceramic-to-Metal Joining for High Temperature, High Pressure Heat Exchangers
Electron Technologies, Inc.
SC0015951
Improving Efficiency and Reducing Costs for the Supercritical CO2 Design Process
Concepts NREC, LLC