AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
Home Friction Article
PDF (6.8 MB)
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Research Article | Open Access

Tribological behaviors of turbofan seal couples from friction heat perspective under high-speed rubbing condition

Siyang GAOWeihai XUEDeli DUANShu LI( )
Institute of Metal Research, Chinese Academy of Sciences, Shenyang 110016, China
Show Author Information

Abstract

The tribological behaviors of two types of seal coatings, nickel–graphite and aluminum–hexagon-boron nitride (Ni–Cg and Al–hBN, respectively) versus a Ti–6Al–4V blade used in turbofan engines were investigated using a high-speed rubbing test. The wear status and damage mechanism of the friction couples were studied and the abradability of the seal coatings was evaluated. By analysis of the coating properties and damage mechanism of the seal couple, the friction heat effect was identified as the key factor influencing blade wear forms as well as coating abradability. A one-dimensional heat conduction model was established to estimate the effect of increasing temperature on the friction interface. The results indicated that in the Ni–Cg and Ti–6Al–4V seal couple, the temperature rising rate (TRR) of the Ti–6Al–4V blade was faster than that of the Ni–Cg coating, and so the Ti–6Al–4V blade softened earlier than the Ni–Cg coating, causing the blade to suffer severe wear. In the Al–hBN and Ti–6Al–4V seal couple, the TRR of the Ti–6Al–4V blade was slower than that of the Al–hBN coating, and so the Al–hBN coating softened first; thus, blade damage was reduced or even replaced by coating adhesion. The square root ratio of thermal diffusivity between the blade and the coating could be taken as an indicator of the ratio of TRR between the blade and coating to predict blade wear status as well as damage mechanism. The results of the model agreed well with the experiment results of the two seal couples used in this study.

References

[1]
Bill R C,Ludwig L P. Wear of seal materials used in aircraft propulsion systems. Wear 59: 165–189 (1980)
[2]
Hajmrle K, Fiala P, Chilkowich A P. Abradable seals for gas turbines and other rotary equipment. In Proceedings of ASME Turbo Expo 2004, 2004: 14–17
[3]
Chupp R E, Hendricks R C, Steinetz B M. Sealing in turbomachinery. Journal of Propulsion and Power 22(2): 313–349 (2006)
[4]
Ludwig L P, Bill R C. Gas Path Sealing in Turbine Engines. Tribol Trans 23(1): 1–22 (1980)
[5]
Bounazef M, Guessasma S, Ait Saadi B, Aourage H. Seal creation of abradable material NiCrAl-boron nitride-polyester. In Proceedings of the Third International Conference on Advances in Mechanical Engineering and Mechanics, Hammamet, Tunisie, 2006: 17–19
[6]
Emery A F, Wolak J, Etemad S. An experimental investigation of temperatures due to rubbing at the blade-seal interface in an aircraft compressor. Wear 91(2): 117–130 (1980)
[7]
Wolak J, Emery A F, Etemad S. Preliminary results on the abradability of porous, sintered seal material. Journal of Lubrication Technology (Transactions of the ASME) 105: 576–582 (1983)
[8]
Bill R C, Shiembob L T. Friction and wear of sintered fibermetal abradable seal materials. In Intern. Conf. on Wear of Materials, St. Louis, MO United States, 1977: 421–427.
[9]
Irissou E, Dadouche A, Lima RS. Tribological Characterization of plasma-sprayed CoNiCrAlY-BN abradable coatings. Journal of Thermal Spray Technology 23(1–2): 252–261 (2014)
[10]
Taylor T A, Thompson B W, Aton W. High speed rub wear mechanism in IN-718 vs. NiCrAl–Bentonite. Surf Coat Technol 202(4–7): 698–703 (2007)
[11]
Borel M O, Schmid R K, Nicoll A R. Improved abradable coatings using wear mechanism mapping and Microstructural modeling. In Proceedings of the 3rd National Thermal Spray Conference, California, Amearica, 1990: 119–123.
[12]
Borel M O, Nicoll A R, Schmid R K. The wear mechanisms occurring in abradable seals of gas turbines. Surf Coat Technol 39–40(Part 1): 117–126 (1989)
[13]
Wang H G. An analysis of turbine blade/abradable seal rubbing. In Proceedings of the 1st International Conference on Processing Materials for Properties, Hawaii, America, 1993: 1085–1088
[14]
Wang H G. Criteria for analysis of abradable coatings. Surf Coat Technol 79(1–3): 71–75 (1996)
[15]
Bounazef M, Guessasma S, Ait Saadi B. The wear, deterioration and transformation phenomena of abradable coating BN-SiAl-bounding organic element, caused by the friction between the blades and the turbine casing. Mater Lett 58(27–28): 3375–3380 (2004)
[16]
Ghasripoor F, Schmid R K, Dorfman M F, Russo L. A review of clearance control wear mechanism for low temperature aluminium silicon alloys. In Proceedings of the 15th International Thermal Spray Conference, Nice, France, 1998: 25–29.
[17]
Fois N, Watson M, Stringer J,Marshall M B. An investigation of the relationship between wear and contact force for abradable materials. In Proceedings of the Institution of Mechanical Engineers, Part J, Journal of Engineering Tribology Online Published, 2014: 1–15
[18]
Fois N, Stringer J, Marshall M B. Adhesive transfer in aero-engine abradable linings contact. Wear 304(1–2): 202–210 (2013)
[19]
Stringer J, Marshall M B. High speed wear testing of an abradable coating. Wear 294–295: 257–263 (2012)
[20]
Laverty W F. Rub energetics of compressor blade tip seals. Wear 75: 1–20 (1982)
[21]
Kennedy F E. Thermomechanical phenomena in high speed rubbing. Wear 59(1): 149–163 (1980)
[22]
Gao S Y, Liu S W, Li S, liu Y. Evaluation of wear resistance of abradable coating by a single-pass pendulum scratch method. Tribology 30(4): 385–391 (2010)
[23]
Johnston R E. Mechanical characterisation of AlSi-hBN, NiCrAl-Bentonite, and NiCrAl-Bentonite-hBN freestanding abradable coatings. Surf Coat Technol 205(10): 3268–3273 (2011)
[24]
Johnston R E, Evans W J. Freestanding abradable coatingmanufacture and tensile test development. Surf Coat Technol 202(4–7): 725–729 (2007)
[25]
Zhang H J. Heat Conduction. Beijing (China): Higher Education Press, 1982
[26]
Yan M G. Handbook on China Aeronautical Materials, Volume 4. Standars Press of China, 2001
Friction
Pages 176-190
Cite this article:
GAO S, XUE W, DUAN D, et al. Tribological behaviors of turbofan seal couples from friction heat perspective under high-speed rubbing condition. Friction, 2016, 4(2): 176-190. https://doi.org/10.1007/s40544-016-0114-x

682

Views

34

Downloads

20

Crossref

N/A

Web of Science

21

Scopus

3

CSCD

Altmetrics

Received: 14 January 2016
Revised: 14 March 2016
Accepted: 12 May 2016
Published: 15 June 2016
© The author(s) 2016

This article is published with open access at Springerlink.com

Open Access: The articles published in this journal are distributed under the terms of the Creative Commons Attribution 4.0 International License (http:// creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.

Return