Registration Number
0218U003795,
0116U007400
, R & D reports
Title
The development of intermetallic alloys based on titanium aluminides for details of gas turbine engines and aerospace engineering
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Head
Belokon' Y.A.,
Registration Date
24-07-2018
Organization
Zaporozhye State Engineer Academy
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The possibility of obtaining intermetallic titanium alloys for compressor blades of gas turbine engines based on the method of self-propagating high-temperature synthesis (SHS). It was shown that the developed formulations of SHS mixtures and technological modes of SHS process, allow to create intermetallic alloys based aluminides titanium. The results of microprobe analysis were used to prove the receipt of TiAl in a two-phase structure of the alloy with intermetallic phase TiAl + Ti3Al. It was established that the safety factor of the compressor blades of modern gas turbine engine made of intermetallic titanium alloys meet the requirements of normative documents.
Product Description
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Бєлоконь К.В.
Бєлоконь Юрій Олександрович
Бондаренко Ю.В.
Васильченко Т.О.
Воденнікова Ок. С.
Воденнікова Ол.С.
Гітуляр А.А.
Жеребцов О.А.
Кругляк Д.О.
Прохорова А.Д.
Середа Д.Б.
Чейлитко А.О.
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2020-04-02
