A Portable, Vibro-Acoustic Based NDI System for Composite Structures

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,853.00
Award Year:
2008
Program:
SBIR
Phase:
Phase I
Contract:
FA8501-08-M-0013
Agency Tracking Number:
F073-117-0531
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
IMPACT TECHNOLOGIES, LLC
200 Canal View Blvd, Rochester, NY, 14623
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
073955507
Principal Investigator:
Michael Roemer
Director of Engineering
(585) 424-1990
mike.roemer@impact-tek.com
Business Contact:
Mark Redding
President
(585) 424-1990
mark.redding@impact-tek.com
Research Institution:
n/a
Abstract
Impact Technologies, in collaboration with our commercialization partner Boeing, propose to develop a portable, non-destructive inspection (NDI) system that can quickly and accurately determine the damage state of an aircraft composite structure using vibro-acoustic feature analysis. The high-frequency analysis method proposed can be applied in an automated manner using a modal hammer and vibro-acoustic accelerometers capable of assessing the location and severity of various forms of damage, including dis-bonds and delamination. The application of the proposed developments will be focused on the F-15 vertical stabilator region, which our commercialization partner Boeing to assist with design specific knowledge. The core innovations of this project include: 1) Implementation of practical, real-time, non-destructive inspection (NDI) methods (including sensors and signal processing software) that can be applied to critical regions of aircraft structures using piezo-electric response measurements for damage assessments; 2) Development of an integrated frequency, damping and mode shape sensitivity algorithm for damage detection and localization; 3) Development of a stress wave analysis algorithm that incorporates an optimized triangulation procedure for improved damage localization once damage is detected; and 4) Validation of the portable NDI system prototype (including hardware, software and sensors) based on performing a series of well-organized and realistic tests on composite panels with various levels of external and internal damage and baseline testing of the F-15 vertical stabilator region.

* information listed above is at the time of submission.

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