FIELD: chemistry.
SUBSTANCE: invention relates to protection of intermetallic alloys based on titanium aluminides against high temperature oxidation, and may be used to protect turbine or compressor blades operating at temperatures up to 800°C. The method comprises product treatment in a solution of phosphoric or phosphorous acid by immersion, and air drying. Moreover, a 5-molar solution of phosphoric or phosphorous acid is used, wherein the product is held for 23-25 hours, then washed by water and dried at a temperature of 110-130°C for 2-4 hours.
EFFECT: increased resistance of the intermetallic alloy based on titanium aluminide oxidation to high temperatures of up to 800 degrees due to surface modification by phosphates, reducing the oxide film growth rate.
1 tbl, 1 ex
Title | Year | Author | Number |
---|---|---|---|
METHOD OF PRODUCING TITANIUM ALLOY MULTILAYER PROTECTIVE COATING OF TURBOMACHINE BLADES | 2017 |
|
RU2667191C1 |
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RU2606368C1 |
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RU2772342C1 |
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RU2785110C1 |
Authors
Dates
2017-04-11—Published
2015-12-15—Filed