Publication detail
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.
English title
THE INFLUENCE COMPARISON OF CREEP TESTING AND AIR TRAFFIC ON MICROSTRUCTURE OF CAST NICKEL BASE SUPERALLOY INCONEL 713 LC
Type
Peer-reviewed article not indexed in WoS or Scopus
Language
en
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.
Released
2003-11-25
ISSN
1429-6065
Volume
76
Number
290
Pages from–to
177–
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",
year="2003",
volume="76",
number="290",
pages="6"
}