SBIR/STTR Research Award

In-Situ Functionally Graded Oxide Matrix Composite for Gas Turbine Applications

Award identifier 0994990ff1605ca4e8049d96c0d03582ad400e3dc632dd43f3683e3148934ba3Awarding agency Department of Energy

Award amount

$749,920

Program and phase

SBIR · Phase II

Award year

2007

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Award details

Awarding agency
Department of Energy
Branch
Not reported
Recipient company
UES INC
Proposal award date
Not reported
Contract end date
Not reported
UEI
FV5WK6YTN215
Solicitation number
DE-FG01-05ER05-28
Topic code
28

Research abstract

Currently, ceramic matrix composites (CMCs), which generally are lighter and more thermally stable than their metallic counterparts, are under evaluation for use in industrial gas turbine engines. The use of CMC could permit higher operating temperatures and reduced cooling, thereby contributing to higher fuel efficiency and lower NOx and CO emissions. State-of-the-art oxide-based composites require a thermal protection system (TPS) coating to mitigate the thermal gradients endured by the material during exposure. However, this coating can delaminate or erode, leading to exposure of the underlying composite, which contains a mullite-based fiber that is prone to attack in a moist combustion environment. This project will develop a non-silica-containing composite with a TPS that is integral and fabricated in situ. This oxide-based composite design will be resistant to environmental attack on the hot side, and will support a low thermal gradient on the cold side to minimize thermal stresses. In Phase I, a compositionally graded oxide matrix composite was exposed in a simulated combustion environment for 100 hours. The results provided a clear direction for Phase II, in which two different composite design options will be evaluated. The optimal design will be down-selected based on mechanical and thermal property data. Subscale components of the functionally graded composite material will be fabricated and tested in a subscale test facility, and then a full-scale component will be fabricated and tested. Commercial Applications and Other Benefits as described by the awardee: The functionally graded oxide matrix composite should resist degradation in the moisture-containing combustion environments that exist in high temperature gas turbine engines, providing significant economic and environmental benefits. The market for industrial gas turbine engine applications is expected to grow over the next decade, due to the closing of aging coal plants and the need for increased global power demands, particularly in Asia. The materials also would have potential use in propulsion-related applications in the industrial, military, and commercial sectors.

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.

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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