SBIR/STTR Research Award
High Temperature Corrosion Resistant Nanocomposite Materials for Turbine Engine Applications
Award amount
$99,000Program and phase
SBIR · Phase IAward year
2006Award details
- Awarding agency
- Department of Defense
- Branch
- Defense Advanced Research Projects Agency
- Recipient company
- MATERIALS MODIFICATIONS INC
- Proposal award date
- 2006-11-28
- Contract end date
- 2007-07-31
- UEI
- PXFHME8QVPT6
- Solicitation number
- 2006.2
- Topic code
- SB062-003
Research abstract
The operating temperature and efficiency of turbine engines is limited by the thermal properties of the coatings that are used to protect the underlying superalloys. Additionally, surface deposits that penetrate through the thermal barrier coating (TBC) system cause hot corrosion and premature failure of the coating. In order to extend the operational temperature and life of the turbines, a systems approach to develop new or improved coatings are required. The proposed effort by Materials Modification, Inc., will develop a nanocomposite coating system that is designed by taking into consideration the thermodynamic compatibility of the bond coat and the TBC along with minimizing thermal transport through the coating.
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- Co-polymer composites for high voltage insulation wraps for superconducting magnet coils- C57-22
- Ceramic Composite Nanofiber Aerogel Insulation for EVA Suits
- PFAS-free chemical barrier elastomers for breathable, protective garments
- Superrepellent powder coating of dry storage canisters for spent nuclear fuel- Topic 40 b
- Critical Minerals And Materials Recovery From Oil And Gas Produced Water Topic 8a
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- High Temperature Corrosion Resistant Nanocomposite Materials for Turbine Engine Applications
- High Temperature Anticorrosion Ceramic Nanocomposite Coatings for Current and Next Generation Turbine Engines
- Advanced Multi-Layer Thermal Barrier Coatings with Enhanced Durability Against Calcium Magnesium Alumino-Silicate (CMAS) Corrosion
- Innovative Silicon Nitride - Zirconium Dioxide Nanocomposites for Turbine Engine Applications
- NANOSTRUCTURED THERMAL BARRIER COATING BASED ON FILTERED ARC PLASMA SOURCE ION DEPOSITION
Research funding history
166 SBIR/STTR records share this UEI (1986–2024). Reported award amounts total $34,897,489. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration, National Science Foundation, Department of Energy, Environmental Protection Agency, Department of Commerce