An additive manufacturing (AM) process has been used to fabricate beam components with unique internal geometries capable of reducing weight and inherently suppressing vibration of the structure. Using the laser powder bed fusion (LPBF) AM process, four unique designs are investigated to quantify and understand the damping effectiveness of this manufacturing concept. Forced-response tests are conducted to validate the damping capability of each internal design configuration. The effects of external geometry, thermal distribution associated with internal friction, strain amplitude, and loading rate dependence on damping performance are studied. The results of the studied beams are compared to the damping performance of a fully-fused, or solid baseline LPBF beam. With only 1–4% internal beam volume alteration, the four unique beams are capable of providing up to ten times damping into their respective systems compared to the baseline, solid beam. From the studies of different parameter effects on damping, the main mechanism for vibration suppression is identified. Validation of the vibration suppression physics allows for internal feature optimization via LPBF that can maximize damping effectiveness.
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ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition
June 11–15, 2018
Oslo, Norway
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5115-9
PROCEEDINGS PAPER
Investigating Damping Performance of Laser Powder Bed Fused Components With Unique Internal Structures
Onome Scott-Emuakpor,
Onome Scott-Emuakpor
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Tommy George,
Tommy George
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Brian Runyon,
Brian Runyon
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Casey Holycross,
Casey Holycross
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Bryan Langley,
Bryan Langley
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Luke Sheridan,
Luke Sheridan
Air Force Research Laboratory, Wright-Patterson AFB, OH
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Ryan O’Hara,
Ryan O’Hara
Air Force Institute of Technology, Wright-Patterson AFB, OH
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Phil Johnson,
Phil Johnson
Universal Technology Corporation, Dayton, OH
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Joseph Beck
Joseph Beck
Perceptive Engineering Analytics LLC, Minneapolis, MN
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Onome Scott-Emuakpor
Air Force Research Laboratory, Wright-Patterson AFB, OH
Tommy George
Air Force Research Laboratory, Wright-Patterson AFB, OH
Brian Runyon
Air Force Research Laboratory, Wright-Patterson AFB, OH
Casey Holycross
Air Force Research Laboratory, Wright-Patterson AFB, OH
Bryan Langley
Air Force Research Laboratory, Wright-Patterson AFB, OH
Luke Sheridan
Air Force Research Laboratory, Wright-Patterson AFB, OH
Ryan O’Hara
Air Force Institute of Technology, Wright-Patterson AFB, OH
Phil Johnson
Universal Technology Corporation, Dayton, OH
Joseph Beck
Perceptive Engineering Analytics LLC, Minneapolis, MN
Paper No:
GT2018-75977, V07CT35A020; 10 pages
Published Online:
August 30, 2018
Citation
Scott-Emuakpor, O, George, T, Runyon, B, Holycross, C, Langley, B, Sheridan, L, O’Hara, R, Johnson, P, & Beck, J. "Investigating Damping Performance of Laser Powder Bed Fused Components With Unique Internal Structures." Proceedings of the ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. Volume 7C: Structures and Dynamics. Oslo, Norway. June 11–15, 2018. V07CT35A020. ASME. https://doi.org/10.1115/GT2018-75977
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