TY - GEN
T1 - Nonplanar Technique for 3D Printing Wings
AU - Lamagna Reiter, Stephen R.
AU - Valenti, Justin D.
AU - Yukish, Michael A.
N1 - Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc.. All rights reserved.
PY - 2022
Y1 - 2022
N2 - This work develops a technique for printing an unmanned aerial vehicle wing with its span parallel to the build plate using material extrusion. Stair-stepping from planar additive manufacturing often leads a designer to choose a vertical build orientation; however, this limitation can now be overcome by leveraging recent advances in nonplanar printing techniques. This paper documents available nonplanar methods and demonstrates the use of nonplanar slicing combined with gcode post-processing to print a wing lying down. The advantages of this technique are the potential for faster printing times, improved resistance to bending along the wing’s span, and open access to internal components. The disadvantages of this technique are larger time requirements in the design and slicing phases, the need for a large support structure or complex build platform, and additional post-processing of the printed wing. By presenting this technique, this paper expands the available design space for engineers producing small-scale aircraft with material extrusion.
AB - This work develops a technique for printing an unmanned aerial vehicle wing with its span parallel to the build plate using material extrusion. Stair-stepping from planar additive manufacturing often leads a designer to choose a vertical build orientation; however, this limitation can now be overcome by leveraging recent advances in nonplanar printing techniques. This paper documents available nonplanar methods and demonstrates the use of nonplanar slicing combined with gcode post-processing to print a wing lying down. The advantages of this technique are the potential for faster printing times, improved resistance to bending along the wing’s span, and open access to internal components. The disadvantages of this technique are larger time requirements in the design and slicing phases, the need for a large support structure or complex build platform, and additional post-processing of the printed wing. By presenting this technique, this paper expands the available design space for engineers producing small-scale aircraft with material extrusion.
UR - http://www.scopus.com/inward/record.url?scp=85123897386&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85123897386&partnerID=8YFLogxK
U2 - 10.2514/6.2022-2476
DO - 10.2514/6.2022-2476
M3 - Conference contribution
AN - SCOPUS:85123897386
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -