SBIR/STTR Research Award

Durable High Temperature Coatings For Utility Scale Gas Turbine Hot Gas Path Components

Award identifier 860fc88ecbebe444c8302c523f41352709cdc28b411ed4b78ce7a38d0d5afdffAwarding agency Department of Energy

Award amount

$849,935

Program and phase

STTR · Phase II

Award year

2015

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Award details

Awarding agency
Department of Energy
Branch
Not reported
Recipient company
UES INC
Proposal award date
2015-04-06
Contract end date
2017-04-05
UEI
FV5WK6YTN215
Solicitation number
DE-FOA-0001193
Topic code
14c

Research abstract

For advanced gas turbines where turbine inlet temperature reaches 2650F and beyond, the current state-of-the-art thermal barrier coating (TBC) systems are not adequate to provide the needed protection for the metallic components of the turbine engine. Thus there is a need to develop new chemistries for TBC systems, consisting of bond coat and top coat, with enhanced durability. We propose to modify the coating chemistry of high temperature top coat material to impart higher toughness needed for high temperature durability. We also propose to develop highly durable bond coat chemistry. The Phase I approach consists of the feasibility demonstration of the developed coating chemistries whereas the phase II approach involves optimization of the bond coat and top coat chemistries in relation to their relevant properties. In the Phase I work, appropriate top and bond coat materials were selected and appropriately processed to render their chemistry suitable for high temperature applications. The processed top and bond coats were characterized to show that they have the desired characteristics that were lacking for application at higher temperature with enhanced durability. In the Phase II work, the top and bond coat chemistries will be further optimized to impart optimal desired characteristics. Also in Phase II, approaches will be developed to manufacture optimal top coat material on a commercial scale. Complete TBC systems with optimal top and bond coat will be manufactured and characterized to demonstrate their relevant characteristics needed for high temperature applications. Commercial Applications and Other Benefits: The TBC systems developed in this program will have application in turbine engines utilized in electric power production, propelling aircraft, pumping fluids etc. Successful completion of the project will enable gas turbine engines to operate at elevated temperatures with higher efficiency (lower cost), lower emission (less environmental pollution) and increased reliability and performance.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

294 SBIR/STTR records share this UEI (1983–2023). Reported award amounts total $73,979,003. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, Department of Energy, National Science Foundation, National Aeronautics and Space Administration, Department of Health and Human Services, Nuclear Regulatory Commission

Contractor profile

UES, INC.

Historical federal award activity, when published, is on that contractor profile. Matched by UEI only.

Agency intelligence

Department of Energy

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