Detail publikace
THE INFLUENCE COMPARISON OF CREEP TESTING AND AIR TRAFFIC ON MICROSTRUCTURE OF CAST NICKEL BASE SUPERALLOY INCONEL 713 LC
NĚMEC, K. PODRÁBSKÝ, T. VĚCHET, S. JULIŠ, M. POSPÍŠILOVÁ, S.
Anglický název
THE INFLUENCE COMPARISON OF CREEP TESTING AND AIR TRAFFIC ON MICROSTRUCTURE OF CAST NICKEL BASE SUPERALLOY INCONEL 713 LC
Typ
Článek recenzovaný mimo WoS a Scopus
Jazyk
en
Originální abstrakt
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.
Vydáno
2003-11-25
ISSN
1429-6065
Ročník
76
Číslo
290
Strany od–do
177–
Počet stran
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",
year="2003",
volume="76",
number="290",
pages="6"
}