United States of America As Represented by the Secretary of the Air Force

Ryan Durscher

Alexander Pankonien

Joshua Deaton

Nitin Bhagat

A method and system for measuring strain in a 3D printed part is disclosed herein. The printed part can be formed with internal features that can be analyzed with a digital image correlation system to determine strain levels in internal regions of the part. The features are visually identifiable due to a different color, shape, design or other visually distinguishable characteristics relative to that of the base structural material. The features can be the formed from the same material or a different material from that of the base structure material.

Method and system for measuring strain in a 3D printed part

Additive and subtractive manufacturing (e.g. 3D Printing) is used to form aeroelastic airfoils with control surface region(s) having conventional rib/spar structural topologies and a continuous skin (e.g smooth surface) formed over the entire outer surface of the airfoil. The control surface is moved with internal actuators resulting in a 'morphing' airfoil as the skin stretches to follow the moving structure of the control surface region. The airfoil can include a plurality of different material moduli and geometric featuring to balance the appropriate control of stiffness with topological requirements.

Growing community of inventors

Loveland, OH, United States of America

Ryan Durscher