FIELD: chemothermal treatment of metals.
SUBSTANCE: composition of mixture for repetitive chrome-calorizing of refractory nickel alloys contains 13-21% aluminum, 29-37% chromium, and 50% alumina. Composition can be used in mechanical engineering for protection of gas-turbine engine parts against gas corrosion.
EFFECT: enabled multiple chrome-calorizing at preservation of characteristics of coatings and endurance and reliability of parts operated under thermomechanical loadings and high-temperature oxidation.
4 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| PROCEDURE OF APPLICATION OF PROTECTIVE COATING ON PARTS OUT OF NICKEL ALLOYS | 2008 | 
 | RU2375497C1 | 
| METHOD OF DEPOSITION OF THE COMBINED HOT-RESISTANT COATING ON THE TURBINE BLADES | 2004 | 
 | RU2272089C1 | 
| METHOD OF COMBINATION HEAT-RESISTANT COATING ON TURBINE BLADES OF GAS-TURBINE ENGINE | 2007 | 
 | RU2349679C1 | 
| METHOD OF APPLICATION OF COMBINED HEAT-RESISTANT COATING | 1996 | 
 | RU2145363C1 | 
| PROCEDURE FOR APPLICATION OF COMBINED HEAT INSULATED COATING ON PARTS OUT OF HEAT RESISTANT ALLOYS | 2009 | 
 | RU2402639C1 | 
| SUSPENSION FOR ALUMINIUM CHROMOSILICONISING OF PARTS MADE OF HEAT-RESISTANT NICKEL ALLOYS | 2006 | 
 | RU2326183C1 | 
| METHOD FOR COATING OF PARTS MADE FROM NICKEL-BASED ALLOYS | 2006 | 
 | RU2320774C1 | 
| APPLICATION METHOD OF COMBINED THERMAL PROTECTIVE COATING TO PART FROM HEAT-RESISTANT ALLOYS | 2011 | 
 | RU2469129C1 | 
| METHOD OF CHEMICAL-HEAT TREATMENT OF PARTS OF NICKEL ALLOYS | 2011 | 
 | RU2462535C1 | 
| METHOD FOR APPLYING COMBINED HEAT-RESISTANT COATING TO TURBINE BLADES OF GTE | 2020 | 
 | RU2755131C1 | 
Authors
Dates
2005-12-20—Published
2004-06-07—Filed