Biomimetics Based Design of Damage Tolerant Airframe Panels

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: N/A
Agency Tracking Number: 992025
Amount: $578,125.00
Phase: Phase II
Program: SBIR
Awards Year: 2001
Solicitation Year: N/A
Solicitation Topic Code: N/A
Solicitation Number: N/A
Small Business Information
Aerochem Corporation
PO Box 90087, Gainesville, FL, 32607
DUNS: N/A
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Shao-Chun Liu
 Junior Engineer
 () -
 scliu@aero.ufl.edu
Business Contact
 Bruce Carroll
Title: President
Phone: (352) 392-4943
Email: bfc@aero.ufl.edu
Research Institution
N/A
Abstract
The specific innovation proposed is to design an advanced composite airframe panel for damage tolerance by incorporating biologic solutions to a similar problem found in nature, using a biomimetic approach. We will identify principal material (fiber) directions and density profiles about naturally occurring holes in bones through a microscopic and radiographic techniques. These holes are known to be damage tolerant, as they clinically do not represent a fracture or fatigue failure initiation site. In addition to its novel microstructure, bone is also a 2 fiber composite material, consisting of stiff bone mineral crystals embedded in a scaffold of compliant collagen fibers. We will demonstrate the expected low stress concentrations about the hole through mechanical testing and moir¿ interferometry. We will then incorporate these principal material directions and density and use a 2 fiber system in a computational model of a representative airframe panel. This model will be used to demonstrate the advantages of biomimetic design. We believe biomimetic design principles can be used to reduce aircraft weight, as bones are weight optimized due to the energy expenditure required to carry such a relatively heavy tissue. Furthermore, by increasing damage tolerance, life cycle costs of airframes can be reduced significantly.

* information listed above is at the time of submission.

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