SBIR/STTR Research Award

Multi-Layer Deep Structure NDI

Award identifier c2d592e3a4e7d95eac6175277fae02e3d2e81558d76aef5129b7471006d0adb8Awarding agency Department of Defense · Air Force

Award amount

$149,658

Program and phase

SBIR · Phase I

Award year

2015

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Innovative Materials Testing Technologies, Inc.
Proposal award date
2015-09-02
Contract end date
2016-06-02
UEI
EL5QQJ9LXJN6
Solicitation number
2015.1
Topic code
AF151-159

Research abstract

ABSTRACT: An innovative NDI method, General Remote Field Eddy Current (GRFEC) method, is proposed for aircraft multi-layer deep structure NDI. GRFEC method is characterized by its deep penetration and high sensitivity features in multi-layer and complex deep structure NDI. The outstanding features have been proved by the AFRL validation/evaluation programs and published at 2014 AA&S Conference and 2014 ASIP Conference. Due to the deep penetration ability flaw can be detected directly from surface of a structure. This improves flaw detection beyond the first layer in multi-layered, complex, and difficult to access structures. Two approaches are proposed to upgrade GRFEC method. 1). to validate GRFEC systems ability in determining hidden flaw parameters and conditions directly from the structure surface, such as flaw location, length and orientation of a crack, single or multiple cracks, etc. Influence to flaw signal from structure geometry, such as edge condition and distance between fasteners, will also be addressed. The goal is enable straightforward NDI inverse problem solutions to avoid complicated inverse-problem algorithms and numerical modeling. 2). to provide easy airplane data capture and periodical NDI data storage approaches. Instant display of long-term periodical NDI data will be enabled in GRFEC system for a large number of inspected locations/fasteners. Any sudden change in inspected signal of a location/fastener should be a strong indication of possible defect or structure variation at the location before the last inspection time. Since no structure disassembly is involved in implementation of the NDI, all the work can be done quickly. Furthermore, the 2nd approach may possibly become a new way of Structure Health Monitoring (SHM) using a GRFEC system. ; BENEFIT: Anticipated Benefits/Potential Commercial Applications of the Research or Development. Significant improvement of overall NDI capabilities is promised by using the proposed GRFEC method, not only in reduction of the burden of time and cost intensive inspection, but also in insurance of the reliability of the inspection results, as well as in increase of the safety of continuous operation for the aging Air Force aircraft fleets.

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

5 SBIR/STTR records share this UEI (1999–2015). Reported award amounts total $1,668,276. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense

Agency intelligence

Department of Defense

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