SBIR-STTR Award

Aircraft Corrosion Inspection
Award last edited on: 3/2/2007

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$1,130,037
Award Phase
2
Solicitation Topic Code
AF04-274
Principal Investigator
Lawrence J Busse

Company Information

USUT Labs Inc

12505 East 55th Street Suite A
Tulsa, OK 74146
   (918) 852-5460
   dwulf@usutlabs.com
   www.usutlabs.com
Location: Single
Congr. District: 01
County: Tulsa

Phase I

Contract Number: ----------
Start Date: ----    Completed: ----
Phase I year
2004
Phase I Amount
$99,825
The objective of this proposal is to develop a portable and accurate means of detecting and accurately characterizing corrosion in multiple layered structures made of dissimilar metals. The proposed approach is to apply technology that was developed for ultrasonic imaging. Of particular interest are aircraft structures such as wings that are made dissimilar metal layers. The objective is to demonstrate the ability to detect corrosion between layers of material without requirements for disassembly.

Keywords:
Ultrasound, Non-Destructive Testing, Real-Time Imaging, Inspections, Linear Array, Corrosion

Phase II

Contract Number: ----------
Start Date: ----    Completed: ----
Phase II year
2005
Phase II Amount
$1,030,212
This project will develop an inspection technology capable of accurately detecting and characterizing flaws and/or corrosion in multi-layered structures made of dissimilar metals. The inspection target of this project is the F-15 splice joint at wing station 155 where tapered surfaces of aluminum and titanium are joined with steel fasteners. This region is subject to corrosion and is particularly difficult to inspect with conventional UT or eddy current methods. This technology has broader applications to other areas of aircraft structures. Advanced ultrasonic imaging hardware (capable of providing high resolution B-scans using linear arrays), specialized probe designs and coupling systems will be developed to enable these F-15 structures to be quickly and easily inspected with little or no aircraft preparation. Fast, in-situ inspection of these types of interfaces (without requiring disassembly) provides substantial cost and time savings at the repair depot as well as extra safety margin for Air Force personnel. This technology produces a record of results for comparison to future inspections and allows more frequent inspections of critical structural components in the field or depot.

Keywords:
NON-DESTRUCTIVE TESTING, ULTRASONIC IMAGING, LINE