Optimum Structural Design of a Triaxial Load Cell for Wind Tunnel Test

풍동용 3 축 로드셀의 구조최적설계

  • Received : 2010.11.08
  • Accepted : 2010.12.13
  • Published : 2011.02.01

Abstract

In this study, an optimized design of a triaxial load cell has been developed by the use of finite element analysis, design of experiment and response surface method. The developed optimal design was further validated by both stress-strain analysis and natural vibration analysis under an applied load of 30 kgf. When vertical, horizontal, and axial loads of 30 kgf were applied to the load cell with the optimal design, the calculated strains were satisfied with the required strain range of $500{\times}10^{-6}{\pm}10%$. The natural vibration analysis exhibited that the fundamental natural frequency of the optimally designed load cell was 5.56 kHz and higher enough than a maximum frequency of 0.17 kHz which can be applied to the load cell for wind-tunnel tests. The satisfactory sensitivity in all triaxial directions also suggests that the currently proposed design of the triaxial load cell enables accurate measurements of the multi-axial forces in wind-tunnel tests.

Keywords

References

  1. Karkehabadi, R., Rhew, R. D. and Hope, D. J., "Study and Analyses on the Structural Performance of a Balance," NASA TM-213263, 2004.
  2. Erm, L. P., "Development of a Two-Component Strain Gauge Balance Load Measurement System for the DSTO Water Tunnel," Air Vehicles Division Defence Science and Technology Organization, DSTO-TR-1835, 2006.
  3. Norman, T. R., Shinoda, P. M., Kitaplioglu, C., Jacklin, S. A. and Sheikman, A., "Low-Speed Wind Tunnel Investigation of a Full-Scale UH-60 Rotor System," NASA Ames Research Center, 2002.
  4. Vos, H. B., "Strain Gauge Balance Development at NLR," National Aerospace Laboratory NLR, 1996.
  5. Kang, D. I., Kim, G. S., Jeoung, S. Y. and Joo, J. W., "Design and Evaluation of Binocular Type Sixcomponent Load Cell by Using Experimental Technique," Trans. of the KSME A, Vol. 21, No. 11, pp. 1921-1930, 1997.
  6. Kang, D., Shin, H., Kim, J. and Park, Y., "Design and Analysis of Column Type Sensing Element for Large Compact Load Cell," Trans. of the KSME A, Vol. 27, No. 4, pp. 601-607, 2003. https://doi.org/10.3795/KSME-A.2003.27.4.601
  7. Lee, T. H., Lee, T. H., Byun, C. W. and Park, J. K., "Optimal Design of High-Capacity Column-Type Load Cell Using Response Surface Method," Proc. of KSPE Autumn Conference, pp. 754-758, 2002.
  8. Lee, M. J., Ham, D. S., Lee, S. W. and Han, G. J., "Shape Design of Indirect Adhesion type Load cell for Container Crane," Proc. of KSPE Autumn Conference, pp. 401-402, 2007.
  9. Joo, J. W., Na, K. S. and Kang, D. I., "Design and fabrication of a six-component force/moment sensor," Measurement, Vol. 32, No. 2, pp. 125-133, 2002. https://doi.org/10.1016/S0263-2241(02)00002-7
  10. Kim, G., Kang, D. and Rhee, S., "Design and evaluation of a six-component load cell," Sensors and Actuators A: Physical, Vol. 77, No. 3, pp. 209-220, 1999. https://doi.org/10.1016/S0924-4247(99)00208-3
  11. Zwemmer, R., Quartel, A. and Veltman, D. L., "Development and Operational Aspects of a Signal Transfer System for Use in Wind Tunnel Propeller Models," 19th International Congress on Instrumentation in Aerospace Simulation Facilities, pp. 353-359, 2001.
  12. Rhew, R. D., "A Fatigue Study of Electrical Discharge Machine (EDM) Strain-Gage Balance Materials," International Congress on Instrumentation in Aerospace Simulation Facilities, pp. 477-487, 1989.
  13. Park, S. H., "Modern design of experiments," Minyoung-Sa, pp. 413-435, 2003.
  14. ANSYS, http://www.ansys.com/
  15. Seo, S. K., "MINITAB Reliability Analysis," Eretec, 2009.
  16. Zahavi, E., "Fatigue Design," A Solomon Press Book, 1996.
  17. Han, M. and Cho, J., "The Analysis of Fatigue Damage in Structure under Variable Load," Transaction of the Korean Society of Automotive Engineers, Vol. 12, No. 4, pp. 85-93, 2004.