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NĚMEC, K. PODRÁBSKÝ, T. VĚCHET, S. JULIŠ, M. POSPÍŠILOVÁ, S.
Original Title
THE INFLUENCE COMPARISON OF CREEP TESTING AND AIR TRAFFIC ON MICROSTRUCTURE OF CAST NICKEL BASE SUPERALLOY INCONEL 713 LC
Type
journal article - other
Language
English
Original Abstract
In the working conditions of the jet engines gas turbines of supersonic plane blades are loaded by the cycles, this process is the function of the time, temperature and stress. The blade are exposed to influence of degradable processes namely of the high-temperature corrosion, fatigue process and creep. As the result of short overloading as it happens for instance during the starts and landing, eventually in some other irregularities of the jet engine function, the increase of stress and temperature leads to the changes of microstructure and properties.
Key words in English
Superalloy, microstructure, creep testing
Authors
NĚMEC, K.; PODRÁBSKÝ, T.; VĚCHET, S.; JULIŠ, M.; POSPÍŠILOVÁ, S.
RIV year
2003
Released
25. 11. 2003
ISBN
1429-6065
Periodical
Zeszyty naukowe politechniki Opolskiej seria Mechanika
Year of study
76
Number
290
State
Republic of Poland
Pages from
177
Pages to
182
Pages count
6
BibTex
@article{BUT45435, author="Karel {Němec} and Tomáš {Podrábský} and Stanislav {Věchet} and Martin {Juliš} and Simona {Hutařová}", title="THE INFLUENCE COMPARISON OF CREEP TESTING AND AIR TRAFFIC ON MICROSTRUCTURE OF CAST NICKEL BASE SUPERALLOY INCONEL 713 LC", journal="Zeszyty naukowe politechniki Opolskiej seria Mechanika", year="2003", volume="76", number="290", pages="6", issn="1429-6065" }