Hostname: page-component-cd9895bd7-p9bg8 Total loading time: 0 Render date: 2024-12-27T05:05:51.963Z Has data issue: false hasContentIssue false
  • English
  • Français

Case study on aircraft tyre wear in Y12 aircraft tyres

Published online by Cambridge University Press:  30 May 2018

K. A. Dulani Daminda Kuruppu  and
C. J. Hettiarachchi
K. A. Dulani Daminda Kuruppu*
Affiliation:
Department of Aeronautical Engineering, Faculty of Engineering, General Sir John Kotelawala Defence University, Ratmalana, Sri Lanka
C. J. Hettiarachchi
Affiliation:
Department of Aeronautical Engineering, Faculty of Engineering, General Sir John Kotelawala Defence University, Ratmalana, Sri Lanka
*
dkuruppu1985@yahoo.com
Get access Rights & Permissions [Opens in a new window]

Abstract

The primary objective of this research was to analyse the discrepancies in polymeric properties in Y12 aircraft tyres after 50 landings. Tensile strength and elongation test, abrasion test and hardness tests were carried out for the nose and main gear tyres after the completion of 50 landings. Surface morphologies of the tyre samples were observed using SEM. ISO specifications were followed for each experimental method during testing. There was a reduction in both median tensile strength and elongation at break in aircraft tyres after 50 landings but the reduction rate of both parameters were lower in Tyre 2 (nose wheel tyre) compared with Tyre 1 (left main wheel tyre) and Tyre 3 (right main wheel tyre). The highest percentage of mean volume loss was reported for Tyre 3 (3.88%). In addition, the least percentage of mean volume loss was obtained in Tyre 2 (2.98%). The percentage of hardness reduction was highest in Tyre 2 (6.9%). The surface roughness was induced to the tyre surface after completion of 50 landings.

Keywords

Aircraft tyreswearpolymeric properties
Type
Research Article
Information
The Aeronautical Journal , Volume 122 , Issue 1253 , July 2018 , pp. 1123 - 1144
Copyright
Copyright © Royal Aeronautical Society 2018 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1. Konde, A.K., Rosu, I., Lebon, F., Brardo, O. and Devesa, B. On the modeling of aircraft tire, Aerospace Science and Technology J, 2013, 27, pp 67–75.Google Scholar
2. Behroozi, M., Olatunbosun, O.A. and Ding, W. Finite element analysis of aircraft tyre – Effect of model complexity on tyre performance characteristics, Materials and Design J, 2012, 35, pp 810–819.Google Scholar
3. Guo, H., Bastien, C., Blundell, M. and Wood, G. Development of a detailed aircraft tyre finite element model for safety assessment, Materials and Design J, 2014, 53, pp 902–909.Google Scholar
4. Alroqi, A.A. and Wang, W. Comparison of aircraft tire wear with initial wheel rotational speed, Int J Aviation, Aeronautics and Aerospace, 2015, 2 (1), pp 1–28.Google Scholar
5. Clark, S.K. and Dodge, R.N. Heat generation in aircraft tires, J Computers & Structures, 1985, 20 (1-3), pp 535–544.Google Scholar
6. Good Year Company. Aircraft tire care and maintenance, 2017. Available at: https://www.goodyearaviation.com/resources/pdf/aviation_tyre_care_3_2017.pdf (accessed 3 November 2017).Google Scholar
7. Kongo, K.A., Rosu, I., Ebon, F., Brardo, O. and Devesa, B. Study of the rolling behavior of an airplane tire, AIRBUS, 316 Bayonne Road, 31060 Toulouse cedex 03.Google Scholar
8. Tanner, J.A., Dreher, R.C., Strubb, S.M. and Smith, E.G. Tire tread temperatures during antiskid braking and cornering at dry runway, NASA Technical Paper 2009, 1982.Google Scholar
9. Mc Carthy, J.L. and Tanner, J.A. Temperature distribution in an aircraft tire at low ground speed, NASA Technical Paper 2195, 1983.Google Scholar
10. Clark, S.K. and Doge, R. N. Heat generation in aircraft tires under free rolling conditions, NASA Contractor Report 3629, 1982.Google Scholar
11. Konde, A.K., Rosu, I., Lebon, F., Brardo, O. and Devesa, B. Thermomechanical analysis of an aircraft tire in cornering using coupled ale and lagrangian formulations, Central European J Engineering, 2013, 3 (2), pp 191–205.Google Scholar
12. Hamid, M. and Ghoreishy, R. Finite element analysis of the steel-belted radial tyre with tread pattern under contact load, Iranian Polymer J, 2006, 15 (8), pp 667–674.Google Scholar
13. All the World's Aircraft. Available at: http://www.aviaMarchket.org/china/hai/y-12.html (accessed 15 January 2018).Google Scholar
14. Introduction to aeronautics: A design perspective, Chapter 7, pp 215-239. Available at: https://www.southampton.ac.uk/~jps7/Aircraft%20Design%20Resources/Brandt%20Introduction%20to%20Aeronautics/Ch7Structure.doc (accessed 20 January 2018).Google Scholar
15. Rafei, M., Ghoreishy, M. H. R. and Naderi, G. Thermo-mechanical coupled finite element simulation of tire cornering characteristics - Effect of complex material models and friction law, Mathematics and Computers in Simulation, 2018, 144, pp 35–51.Google Scholar
16. Federal Aviation administration. Aviation maintenance technician handbook- airframe, 2012, 2. Available at: https://www.faa.gov/regulations_policies/handbooks_manuals/aircraft/amt_airframe_handbook/media/ama_Ch13.pdf (accessed 3 November 2017).Google Scholar
17. Xie, M., Tang, H. and Yao, H. Failure analysis of tire separation in two-sized tires on Airbus planes, Engineering Failure Analysis J, 2016, 61, pp 21–27.CrossRefGoogle Scholar