FIELD: machine building.
SUBSTANCE: method involves ionic cleaning with argon ions and ion-implantation treatment of the part surface with nitrogen ions. Ionic cleaning is performed at the energy of 8 to 10 keV and current density of 130 McA/cm2 to 160 McA/cm2 during 0.3 to 1.0 hour. Ion-implantation treatment of the part surface is performed at the energy of 25 to 30 keV. Ionic implantation is performed either in a continuous, or in a pulse mode.
EFFECT: increasing endurance limit and cyclic durability of parts from titanium alloys.
12 cl, 1 ex
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ION-BOMBARDMENT PROCESSING OF COMPRESSOR VANES MADE OF NICKEL-BASED HIGH-ALLOY STEELS AND ALLOYS | 2011 |
|
RU2496910C2 |
| METHOD FOR OBTAINING ION-PLASMA COATING ON BLADES OF COMPRESSOR FROM TITANIUM ALLOYS | 2011 |
|
RU2478140C2 |
| PROCEDURE FOR PRODUCTION OF EROSION-RESISTANT COATING CONTAINING NANO-LAYERS FOR BLADES OF TURBO-MACHINES OUT OF TITANIUM ALLOYS | 2007 |
|
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| METHOD OF IMPROVING EROSION RESISTANCE OF COMPRESSOR BLADES OF GAS-TURBINE ENGINE MADE OF TITANIUM ALLOYS | 2013 |
|
RU2552201C2 |
| METHOD OF PROTECTING COMPRESSOR BLADES OF GAS-TURBINE ENGINE MADE OF TITANIUM ALLOY FROM ABRASIVE DUST EROSION | 2013 |
|
RU2552202C2 |
| METHOD OF OBTAINING EROSION-RESISTANT COATING CONTAINING NANO-LAYERS FOR BLADES OF TURBOMACHINES FROM ALLOYED STEELS | 2007 |
|
RU2386724C2 |
| FORMATION METHOD OF THERMAL PROTECTIVE COATING ON PARTS OF GAS TURBINES FROM NICKEL AND COBALT ALLOYS | 2011 |
|
RU2479666C1 |
| METHOD OF APPLYING HEAT COATING OF NICKEL OR COBALT ALLOY ON GAS TURBINE PARTS | 2011 |
|
RU2496911C2 |
| FABRICATION OF REINFORCED LAYER ON TREADED SURFACE OF PART FROM ALLOYED STEELS | 2013 |
|
RU2557183C2 |
| METHOD FOR GAS TURBINE BLADE PROCESSING | 2013 |
|
RU2533223C1 |
