SBIR/STTR Research Award

Hydration Tolerant, low Thermal Conductivity (K) Thermal Barrier Coatings

Award identifier a65d19f462d0df307f33493a014d4e09c1f515d998ec0e67057fd8dfe37f8b66Awarding agency Department of Defense · Air Force

Award amount

$149,932

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Directed Vapor Technologies International, Inc.
Proposal award date
2012-05-15
Contract end date
Not reported
UEI
F5KSRCP5R8D3
Solicitation number
2012.1
Topic code
AF121-175

Research abstract

ABSTRACT: Thermal barrier coating systems are desired for gas turbine engines. These coatings will increase the durability of hot-section engine components to significantly improve the time"on-wing", safety and readiness of these engines. In this work, research is proposed to investigate the feasibility of modifying the composition and architecture of thermal barrier coating (TBC) systems to enable enhanced resistance to hydration induced TBC spallation while retaining or improving overall system performance. To achieve this, novel coating synthesis techniques will be employed which enable the deposition of advanced compositions and architectures to achieve a comprehensive thermal barrier coating system that provides vastly improved resistance to damage from moisture attack. A low cost, high throughput processing approach for the application of this TBC system is also envisioned. The proposed Phase I effort will identify the failure mechanisms of current and advanced TBC systems exposed to high moisture containing environments through the use of both coupon and component scale testing. The successful completion of the Phase I work will lead to a follow-on Phase II program focused on down-selecting candidate approaches for optimization and applying the new coating onto real aircraft components BENEFIT: This research is anticipated to result in a thermal barrier coating system that provides significantly enhanced durability in moisture containing environments. This work will also improve the durability of TBC systems in general to enable the realization of advanced gas turbine engine designs while leading to several percent thrust improvement or specific fuel consumption reduction for current turbine engines. These advances will not only benefit military engines and aircraft, but also commercial gas turbine engines. In addition, the innovative approach proposed here will reduce the time and expense for refurbishing and repairing blades during engine overhauls, thus improving military readiness and reducing the cost of maintaining commercial aircraft.

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

53 SBIR/STTR records share this UEI (2002–2024). Reported award amounts total $22,949,232. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Energy, National Aeronautics and Space Administration, National Science Foundation

Agency intelligence

Department of Defense

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