Fabrication of Novel Fibrous Monolithic Architectures through Coextrusion

Presenter Information

Sheena Foster

Department

Materials Science and Engineering

Major

Ceramic Engineering

Research Advisor

Hilmas, Greg

Advisor's Department

Materials Science and Engineering

Funding Source

Dr. Greg Hilmas

Abstract

Novel fibrous monolithic architectures were fabricated through a coextrusion process. The purpose of this fabrication is to provide parts for mechanical testing in hopes of developing a material with unique mechanical properties. An alumina and zirconia system was used to make two different architectures. The first architecture is a quadrant structure, alternating quadrants of alumina and zirconia. The second structure is a spiral, with alternating layers of alumina and zirconia. The raw materials were incorporated with various plastics for fabrication. The parts were made by extruding filaments through two passes, packing them into a die, and pressing them into bars. The bars were put through a burnout schedule to remove the plastics, and then sintered at 1550 °C for one hour. SEM analysis was done on green and sintered parts, and mechanical testing will be done.

Biography

Sheena is a junior in Ceramic Engineering from Camdenton, MO. She is currently serving as the president of Keramos and is involved in Material Advantage. She is also involved in the UMR tennis club and the Women’s Leadership Institute.

Research Category

Engineering

Presentation Type

Poster Presentation

Document Type

Poster

Presentation Date

12 Apr 2006, 1:00 pm

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Apr 12th, 1:00 PM

Fabrication of Novel Fibrous Monolithic Architectures through Coextrusion

Novel fibrous monolithic architectures were fabricated through a coextrusion process. The purpose of this fabrication is to provide parts for mechanical testing in hopes of developing a material with unique mechanical properties. An alumina and zirconia system was used to make two different architectures. The first architecture is a quadrant structure, alternating quadrants of alumina and zirconia. The second structure is a spiral, with alternating layers of alumina and zirconia. The raw materials were incorporated with various plastics for fabrication. The parts were made by extruding filaments through two passes, packing them into a die, and pressing them into bars. The bars were put through a burnout schedule to remove the plastics, and then sintered at 1550 °C for one hour. SEM analysis was done on green and sintered parts, and mechanical testing will be done.