A rotor blade (2) for a gas turbine engine, comprising a blade tip 4. At least a portion of the blade tip (4) is provided with a wear-resistant coating (16), (18) comprising magnesium aluminate spinel. A corresponding method to coat a rotor blade tip (4) of a gas turbine engine with magnesium aluminate spinel. The use of magnesium aluminate spinel as a wear resistant coating.
Wear Resistant Coating and Use Thereof
Verschleißfeste Beschichtung und Verwendung davon
Revêtement résistant à l'usure et son utilisation
2017-10-11
Patent
Electronic Resource
English
Wear-Resistant, Thermally Conductive Coating
NTRS | 1988
|Waterproof wear-resistant coating as well as preparation method and application thereof
European Patent Office | 2023
|WEAR AND CORROSION RESISTANT COATING HAVING A ROUGHENED SURFACE
European Patent Office | 2018
|Application of wear resistant coating in fluid power transmissions
Automotive engineering | 1998
|