FIELD: metallurgy.
SUBSTANCE: invention relates to metallurgy, namely to composition and method of manufacturing a composite material with predetermined properties, for example high-class armor protection elements, cutting elements, machine components. Composite material based on a titanium alloy consists of a base metal of a titanium alloy and a modified surface layer. Modified surface layer consists of a face layer with a ceramic structure, layer with a cermet structure and a layer with a transition structure from the cermet layer to the base metal of the titanium alloy and contains a saturated solid solution of nitrogen in titanium with TiNx ceramic particles embedded in it, and/or TiCx, and/or TixNyCz. Face layer has a thickness of 0.08 mm to 0.5 mm and a hardness of at least 62 HRC. Layer with a cermet structure has a thickness of 0.5 to 24 mm and a hardness of 50 HRC to 74 HRC. Layer with a transition structure has a thickness of 5 to 10 % of thickness of cermet layer and a hardness of 60 to 30 HRC, reducing during the transition from the layer with the cermet structure to the base metal of the titanium alloy. Method of manufacturing a composite material includes heating surface of a titanium alloy with a highly concentrated moving source of thermal energy in a gas atmosphere, containing modifying components. Heating and remelting of the surface of the titanium alloy is carried out by a plasma submerged arc of direct action with a specific heat flux at the center of the spot from 104 to 105 W/cm2, current strength of 50–450 A, arc voltage from 20 to 40 V, and a travel speed of a thermal energy source relative to the surface of the titanium alloy from 0.003 to 0.01 m/s, and the gas atmosphere contains a mixture of argon with the addition of modifying nitrogen and/or carbon components in the form of a carbon-containing gas.
EFFECT: material is characterized by high strength, hardness, thermal and corrosion resistance and wear resistance.
8 cl, 3 dwg, 1 tbl
| Title | Year | Author | Number | 
|---|---|---|---|
| MULTILAYER CERMET COMPOSITE MATERIAL AND METHOD OF ITS PRODUCTION | 2020 | 
									
  | 
                RU2731398C1 | 
| BULLET-PROOF ARMOR PLATE | 2012 | 
									
  | 
                RU2491494C1 | 
| COMBINED UNIT OF ADDITIONAL PROTECTION OF EQUIPMENT AGAINST BULLETS OF AUTOMATIC FIRE | 2024 | 
									
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                RU2837935C1 | 
| APPLICATION OF ANTIFRICTION WEAR-PROOF COAT ON TITANIUM, ALLOYS | 2012 | 
									
  | 
                RU2502828C1 | 
| METHOD FOR PULSE ELECTRON-ION-PLASMA HARDENING OF HARD-ALLOY TOOL OR ITEM | 2014 | 
									
  | 
                RU2584366C1 | 
| MULTILAYERED ARMORED OBSTACLE FOR MEANS OF INDIVIDUAL PROTECTION | 2005 | 
									
  | 
                RU2296288C2 | 
| METHOD OF PRODUCTION OF ITEMS OUT OF TITANIUM ALLOYS AND ITEMS PRODUCED BY THIS METHOD (VERSIONS) | 2007 | 
									
  | 
                RU2338811C1 | 
| METHOD FOR STRENGTHENING PARTS BY INDUCTION SURFACING | 2002 | 
									
  | 
                RU2228242C1 | 
| METHOD OF ION-PLASMA TREATMENT OF STEEL AND HARD ALLOY PARTS | 2008 | 
									
  | 
                RU2370570C1 | 
| PROCEDURE FOR APPLICATION OF ANTI-FRICTION WEAR RESISTANT COATING ON ITEM OUT OF METAL OR ALLOY | 2008 | 
									
  | 
                RU2392351C2 | 
Authors
Dates
2018-03-21—Published
2016-08-03—Filed