Automation of a Glow Discharge Spectrometer
David DeHaro, Eric Montejo-Francisco, Louis King, Micah Cerros
Department of Mechanical and Aerospace Engineering
University of California San Diego
Sponsored by Professor Kenneth Vecchio
Overview
Objective
References:
[1]Vecchio, Kenneth S, et al. “High-Throughput Rapid Experimental Alloy Development (HT-READ).” Science Direct, Acta Materialia Inc., 29 Sept. 2021
[2]LECO Corporation. “Glow Discharge Atomic Emission Spectrometer.” Elemental Analysis, 2024.
Acknowledgments:
We would like to thank Professors Jerry Tustaniwskyj and Marko Lubarda for the mentorship through the project, Professor Kenneth Vecchio and Dr. Haoren Wang for sponsoring and supporting the project, as well as the engineering staff — Tom Chalfant, Steve Mercsak, Steve Roberts, Ed Pogue, and Ian Richardson — for their help and expertise in electronics, mechanical design and machining.
Fig. 1: a) LECO GDS900 Spectrometer[2]
b) Wagon wheel metal alloy samples
Design Solution:
Vertical (Z) Axis Assembly
Horizontal (Y) Axis Assembly
Gripper Assembly
a)
b)
Hardware Performance
Impact on Society
Future Improvements
Industry | Application |
Aerospace | Lighter aircraft components |
Military | High performing, reliable, military-grade armor |
Renewable Energy | Efficient and sustainable wind turbine blades |
Software (API) Architecture:
Electronic Components:
Lower Bound
Accuracy
Precision
Accuracy
Precision
Upper Bound
Into the Machine axis
Fig. 11: Precision and accuracy of the mechanism, assessed by creating an 70x70mm grid with points every 10mm.
Calibration Buttons
Fig. 3: Gripper Assembly CAD
Fig. 4: Vertical Axis Assembly CAD
Fig. 7: X-Axis Assembly CAD
Fig. 5 Horizontal axis assembly
Fig.9: Graphic user interface( GUI) (left) & vacuum error message (right)
GDS O-Ring
Vertical Axis
Horizontal Axis
Sample Gripper
Analysis: Deflection of Y-Axis Support
Fig. 6: FEA and analytical deflection analysis. Max deflection = 0.36mm and deflection at measured spoke = 0.13mm
Finite Element Analysis
Analytical Solution
Spoke Location
Max Deflection
Fig. 2: Final assembled mechanism
Fig. 8: Overall Design Solution Components
Fig. 10: System(Top) and PLC(Bottom) State Machine Diagram