Fabrication and Evaluation of an Amino Modified Epoxy Coating for Anti-Scouring and Anti-Corrosion Application

Article Preview

Abstract:

Excellent performance is necessary for compressor blade when aircraft engine serves in harsh environment, where it will go through scouring from jet-stream and extraneous sand, shaking of blades and corrosion from corrosive medium, taking moisture, salt, SO2 for example. Due to the shortage of scouring resistant and anti-corrosion property, shedding of damaged coating is a fundamental reason for the breakdown of aircraft engine blades, which is also the technique bottleneck that hinders the engineering application of compressor blades. Aiming at such problems, an amino modified epoxy coating which performed excellent scouring resistent and anti-corrosion property was fabricated on blades in this paper. Physical properties, anti-corrosion performance, abrasion resistant profiles and scouring resistant test were comprehensively evaluated. Results showed that the coating displayed a high hardness (pendulum hardness 0.9), overlong pot life, well anti-corrosion performance and excellent scouring resistant property. Pot life extends from 8h which is that of common coatings to 36h, so that it is benefit to large scale coating in engineering application. The anti-corrosion performance is similar to traditional aluminizing/inorganic silicate protect coatings, and abrasion resistant property is superior to common protect coatings. Moreover, scouring resistance performance is 3~4 times that of traditional coatings. Hence, such protective coatings could ensure the long lasting of blades protection.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

684-689

Citation:

Online since:

March 2015

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2015 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] W. Chen, Erode protective coating fabricated by MTU [J]. Aviation repair and engineering, 2008, 6: 34-35.

Google Scholar

[2] J. Sun. Attrition of metal [M]. Beijing Metallurgical Industry Press, (1992).

Google Scholar

[3] X. Xu, S. Liu, et al. The efficacy losing of aviation turbine engine and technology of protective coating [J]. Aviation engineering and repair, 2000, 6: 21-23.

Google Scholar

[4] W. Chen, Anti-attrition coating of helicopter compressor [J]. Aviation repair and engineering, 2008, 3: 39-40.

Google Scholar

[5] W. Huo, H. Sun. Advanced coating technology of aviation turbine engine blades [J]. Aviation science and technology, 2001, 3: 34-36.

Google Scholar

[6] B. Zouari, M. Touratier. Simulation of organic coating removal by particle impact [J]. Wear, 2002, 235: 488-497.

DOI: 10.1016/s0043-1648(02)00141-2

Google Scholar

[7] M. Papini, J. K. Spelt. Organic coating removal by particle impact [J]. Wear, 1997, 213: 185-199.

DOI: 10.1016/s0043-1648(97)00062-8

Google Scholar

[8] L.C. Jones. Low angle scouring erosion behaviour of elastomeric materials [J]. Wear, 2011, 271: 1411-1417.

DOI: 10.1016/j.wear.2010.12.057

Google Scholar

[9] I. R. Sare, J. I. Mardel, A. J. Hill. Wear-resistant metallic and elastomeric materials in the mining and mineral processing industries-an overview [J]. Wear, 2001, 250: 1-10.

DOI: 10.1016/s0043-1648(01)00622-6

Google Scholar

[10] W. Zeno, Jr. Wicks, et al. Organic coatings: Science and Technology [M]. John Wiley & Sons, Inc., (2007).

Google Scholar