Gas turbines use ???abradable??? coatings for clearance-control seals, Sealing Technology, vol.2002, issue.1, pp.7-8, 2002. ,
DOI : 10.1016/S1350-4789(02)80002-2
Abradable seal having improved properties,uS Patent 6, p.264, 2002. ,
Gas turbine coatings ??? An overview, Engineering Failure Analysis, vol.26, issue.0, pp.355-369, 2012. ,
DOI : 10.1016/j.engfailanal.2012.07.007
An overview of compressor abradable thermal sprays, Surface Engineering International Thermal Spray Conference ITSC, pp.406-412, 2000. ,
Rotor to stator contacts in turbomachines. Review and application, Mechanical Systems and Signal Processing, vol.40, issue.2, pp.401-420, 2013. ,
DOI : 10.1016/j.ymssp.2013.05.010
URL : https://hal.archives-ouvertes.fr/hal-00934050
A statistical model for the effect of casing treatment recesses on compressor rotor performance, Experimental Thermal and Fluid Science, vol.31, issue.8, pp.1165-1176, 2007. ,
DOI : 10.1016/j.expthermflusci.2006.12.005
Development of Higher Temperature Abradable Seals for Gas Turbine Applications, Volume 4: Turbo Expo 2004, pp.221-229, 2004. ,
DOI : 10.1115/GT2004-53029
Labyrinth seal leakage test: tooth profile, tooth thickness, and eccentricity effects, ASME J. Eng. Gas Turbines Power, vol.130, p.11, 2008. ,
DOI : 10.1115/gt2007-27223
Effect of rub-groove wall angle on the leakage of abradable stepped labyrinth seals, Tribology Trans, pp.443-449, 2005. ,
The effects of wear on abradable honeycomb labyrinth seal, 2006. ,
Rotordynamics of impeller eye seals with wear-damaged teeth in centrifugal compressors, Tribol. Trans, vol.49, issue.3, pp.328-337, 2006. ,
The degradation of abradable honeycomb labyrinth seal performance due to wear, Sealing Technology, vol.2008, issue.8, pp.7-10, 2008. ,
DOI : 10.1016/S1350-4789(08)70451-3
Developpement of abradable and rub tolerant seal materials for application in centrifugal compressors and steam turbines, Proceeding of the Thirty Third Turbomachinery Synopsium, 1991. ,
The investigation of suitability of abradable seal materials for application in centrifugal compressors and steam turbines, Proceedings of the Twentieth Turbomachinery Symposium, 1991. ,
Thermoplastic labyrinth seals for centrifugal compressors, Proceeding Proceedings of the Thirty Third Turbo Symposium, 2004. ,
Ensuring tight seals, 2007. ,
An experimental study of the high speed interaction between a labyrinth seal and an abradable coating in a turbo-engine application, Wear, vol.316, issue.1-2, pp.109-118, 2014. ,
DOI : 10.1016/j.wear.2014.04.023
URL : https://hal.archives-ouvertes.fr/hal-01060023
The wear mechanisms occurring in a labyrinth seal/abradable contact depending on the incursion depth parameter, Mechanics & Industry, vol.262, issue.293, 2016. ,
DOI : 10.1016/j.wear.2006.03.055
Experimental study of the high speed blade-abradable interactions: influence of the material and of the microstructure, 2015. ,
Mechanisms of incursion accommodation during interaction between a vibrating blade and an abradable coating, Wear, vol.330, issue.331, pp.406-418, 2015. ,
DOI : 10.1016/j.wear.2015.01.014
URL : https://hal.archives-ouvertes.fr/hal-01203253
Test bench and test method for a dynamic sealing system, wO Patent App, p.204, 2014. ,
The third-body approach: A mechanical view of wear, Wear, vol.100, issue.1-3, pp.43-452, 1984. ,
DOI : 10.1016/0043-1648(84)90025-5
Velocity accommodation sites and modes in tribology, Eur. J. Mech. A Solids, vol.11, pp.35-47, 1992. ,
DOI : 10.1016/0043-1648(88)90191-3
Wear Particle Life in a Sliding Contact Under Dry Conditions : Third Body Approach, Fundamentals of Tribology and Bridging the Gap Between the Macro-and Micro/Nanoscales, pp.393-411, 2001. ,
DOI : 10.1007/978-94-010-0736-8_28
URL : https://hal.archives-ouvertes.fr/hal-00508127
Maurice Godet's Third Body, pp.21-30, 1996. ,
DOI : 10.1016/S0167-8922(08)70766-1
Mécanisme et tribologie, 1988. ,