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58results about How to "High heat and corrosion resistance" patented technology

Laser surface treatment method for improving thermal corrosion resistance of thermal barrier coating

The invention discloses a laser surface treatment method for improving the thermal corrosion resistance of a thermal barrier coating, belonging to the technical field of treatment of thermal barrier coatings. The method comprises the following steps: S1, ultrasonically cleaning the surface of the thermal barrier coating, and adjusting the spot shape of a laser to a rectangular shape; S2, adjustingthe laser in the step S1 to emit low energy density laser, and carrying out self-preheating scanning on the thermal barrier coating treated in the step S1; S3, adjusting the laser in the step S1 to emit high energy density laser, and carrying out re-melting scanning on the thermal barrier coating treated in the step S2; S4, adjusting the laser in the step S1 to emit medium energy density laser, and performing a slow-cooling scanning on the thermal barrier coating treated in the step S3; S5, naturally cooling the thermal barrier coating treated in the step S4 to room temperature, and then using compressed air to remove impurities on the surface of the coating cooled to room temperature. After the coating is treated by using the method, the coating is smooth and dense, the thermal corrosionof corrosive salt is inhibited, and the service life of the coating is prolonged.
Owner:CHINA UNIV OF PETROLEUM (EAST CHINA)

High-temperature alloy core rod applied to planetary rolling mill for rolling copper and copper and preparation method of high-temperature alloy core rod

ActiveCN109402424AGood high temperature fatigue performanceLess copper stickingFoundry mouldsSolid state diffusion coatingSuperalloyMechanical property
The invention relates to a high-temperature alloy core rod applied to planetary rolling mill for rolling copper and copper and a preparation method of the high-temperature alloy core rod, and belongsto the technical field of metal machining. The high-temperature alloy core rod comprises 11.50-14.00% of Cr, 3.80-5.2% of Mo, 5.50-6.50% of Al, 0.50-1.00% of Ti, 1.80-2.80% of Nb and Ta, 0.005-0.020%of B, 0.08-0.20% of C, 0.050-0.20% of Zr, 0-0.50% of Si, 0-0.50% of Mn, 0-0.015% of P, 0-0.015% of S, 0-2.50% of Fe and the balance Ni. In the preparation process, a mother alloy cast ingot is prepared through vacuum induction smelting, vacuum induction remelting is carried out, a high-temperature alloy core rod blank is prepared through investment casting, the blank is subjected to hot isostaticpressure treatment and subsequent heat treatment, then the blank is polished and subjected to finish machining, and finally the core rod is subjected to surface aluminizing treatment to improve the surface hardness and corrosion resistance at high temperature. The high-temperature alloy core rod prepared through the preparation method has relatively high comprehensive mechanical property, long infatigue life and high in high-temperature strength, the service life of a die is obviously prolonged, the preparation process is simple, and the process is short.
Owner:JIANGSU LONGDA SUPERALLOY MATERIAL CO LTD

Nickel-based superalloy wear surface size repairing method

The invention discloses a method for repairing the size of a nickel-based superalloy wear surface, relates to the field of aero-engine maintenance, and aims to repair the size of a wear surface of a part made of a nickel-based superalloy material. According to the technical scheme, the nickel-based high-temperature alloy abrasion surface size repairing method comprises the steps that S1, repairing pretreatment is conducted, specifically, the abrasion surface of a part is cleaned, shielding protection before sand blasting is conducted on the portion outside a repairing area, and then sand blasting coarsening is conducted on the repairing area; s2, NiAl powder is subjected to plasma spraying on the repaired area, and a bonding bottom layer is formed; s3, CoCrNiW powder is subjected to plasma spraying on the bonding bottom layer, and a working face layer is formed; and S4, the repaired area is machined, so that the thickness and the surface roughness of the coating meet the technological requirements. The method is used for carrying out size repair on the worn surface of the part made of the nickel-based superalloy material, for example, the method is used for carrying out size repair on the end face of a shell of an outer cover of a gas turbine of an aero-engine.
Owner:PLA NO 5719 FACTORY

A Laser Surface Treatment Method for Improving Thermal Corrosion Resistance of Thermal Barrier Coatings

The invention discloses a laser surface treatment method for improving the thermal corrosion resistance of a thermal barrier coating, belonging to the technical field of treatment of thermal barrier coatings. The method comprises the following steps: S1, ultrasonically cleaning the surface of the thermal barrier coating, and adjusting the spot shape of a laser to a rectangular shape; S2, adjustingthe laser in the step S1 to emit low energy density laser, and carrying out self-preheating scanning on the thermal barrier coating treated in the step S1; S3, adjusting the laser in the step S1 to emit high energy density laser, and carrying out re-melting scanning on the thermal barrier coating treated in the step S2; S4, adjusting the laser in the step S1 to emit medium energy density laser, and performing a slow-cooling scanning on the thermal barrier coating treated in the step S3; S5, naturally cooling the thermal barrier coating treated in the step S4 to room temperature, and then using compressed air to remove impurities on the surface of the coating cooled to room temperature. After the coating is treated by using the method, the coating is smooth and dense, the thermal corrosionof corrosive salt is inhibited, and the service life of the coating is prolonged.
Owner:CHINA UNIV OF PETROLEUM (EAST CHINA)
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