FIELD: application of coatings. SUBSTANCE: friction surface, prior to be covered with molybdenum disulfide and subjected to ionic implantation with molybdenum ion beams, is preliminarily covered via vacuum deposition with a coating composed with superhard compounds of one of refractory metals selected from 1V-VI groups (Ti, Zr, Hf, Nb, Ta, Cr, W, Mo, V) with nitrogen, carbon, Boron, or silicon. Thickness of this coating 1-3 mcm. Invention can be applied in mechanical engineering. EFFECT: improved surface protection. 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR MANUFACTURING OF SPLINDLE FROM TITANIUM ALLOY FOR PIPELINE VALVES | 2007 |
|
RU2385792C2 |
| METHOD FOR GAS TURBINE BLADE PROCESSING | 2013 |
|
RU2533223C1 |
| PROCEDURE FOR APPLICATION OF ANTI-FRICTION WEAR RESISTANT COATING ON ITEM OUT OF METAL OR ALLOY | 2008 |
|
RU2392351C2 |
| METHOD FOR PRODUCTION OF ION-PLASMA NANOLAYER COATING ON TURBOMACHINE BLADES FROM TITANIUM ALLOYS | 2008 |
|
RU2388685C1 |
| ION-PLASMA COATING APPLICATION METHOD | 2008 |
|
RU2403316C2 |
| MULTILAYER COATING ON HARD ALLOY TOOL FOR TREATMENT OF TITANIUM ALLOYS AND PROCEDURE FOR ITS FABRICATION | 2009 |
|
RU2415198C1 |
| METHOD OF RECONDITIONING TURBO MACHINE NOZZLE VANES ASSEMBLY MADE FROM NICKEL AND COBALT ALLOYS | 2009 |
|
RU2426632C1 |
| PROCEDURE FOR ION-PLASMA NANO-LAYER COATING ON BLADES OF TURBO-MACHINES OUT OF ALLOYED STEEL | 2008 |
|
RU2413035C2 |
| CUTTING TOOL WITH MULTILAYER COATING | 2010 |
|
RU2542185C2 |
| METHOD OF PRODUCING HEAT-RESISTING COAT ON GAS TURBINE VANES | 2010 |
|
RU2441100C2 |
