SBIR/STTR Research Award

Non-Destructive Evaluation / Inspection (NDE/NDI) for Aero Turbine Hot Section Castings and Coatings

Award identifier 65046bec73b26240224a12bc1e7ca597e882f87ee87a8518434239a910733e79Awarding agency Department of Defense · Navy

Award amount

$99,950

Program and phase

STTR · Phase I

Award year

2006

Explore This Research Award in CaptureIQ

Research the technology, evaluate the recipient and agency, identify related opportunities, and explore potential follow-on work with CaptureIQ.

Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
LUNA INNOVATIONS INCORPORATED
Proposal award date
2006-08-01
Contract end date
2007-05-31
UEI
SJHFCDGKJJC5
Solicitation number
Not reported
Topic code
N06-T011

Research abstract

Luna Innovations Incorporated will conduct a feasibility study of a non-linear, ultrasonic, non-destructive method of evaluating heat transfer and structural characterization of gas turbine engine hot section parts. The proposed concept is a novel ultrasonic measurement which will be used to determine change in heat flux for determining heat transfer. An ultrasonic transducer will be used for the materials characterization as well as the NDI for flaws and structural characteristics. The measurement system will be able to scan a turbine airfoil or hot section component and provide digital indications of heat transfer and internal defects in the parts. The system would be able to scan each part completely for defects as well as blockages in cooling lines while also determining heat transfer characteristics. Current methods are labor intensive, complex, expensive, and provide limited resolution. Luna's concept provides detailed flaw detection and performance evaluation with limited user interaction.BENEFITS: Blockages of cooling lines in turbine airfoils and hot section components can cause severe damage to aircraft components and can lead to failures. The turbines often operate in extreme environmental conditions which can bring the air around parts to temperatures above their melting points so it becomes extremely important to ensure that all of the intricate cooling lines are unblocked and defect free, to ensure proper heat transfer. The proposed method could be applied to commercial aircraft as well as other engine parts that are exposed to extreme thermal and pressurized environments. The technique has the potential to be extended to the field for tests in place.

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

994 SBIR/STTR records share this UEI (1991–2026). Reported award amounts total $336,438,763. Reported amounts are not federal obligations.

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

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, Department of Health and Human Services, National Science Foundation, Environmental Protection Agency

Agency intelligence

Department of Defense

Back to SBIR/STTR Research Awards

Don't take our word for it. Ask AI about RFPCapture.

See what leading AI assistants have to say about RFPCapture and CaptureIQ.

Gemini opens without a prefilled question. The question is copied to your clipboard when the button works. You can also copy it here:

What is RFPCapture.com and its CaptureIQ platform from Smart Logic AI? How does it help federal contractors discover opportunities, evaluate bid/no-bid decisions, research government contracts, and prepare proposals? How does it compare with other federal capture platforms? Use independent sources where available.