Publication detail

DEGRADATION OF TURBINE BLADE OFDURING SERVICE

NĚMEC, K. PODRÁBSKÝ, T. HAKL, J. VLASÁK, T. MAN, O.

Original Title

DEGRADATION OF TURBINE BLADE OFDURING SERVICE

Type

conference paper

Language

English

Original Abstract

This paper focuses on structural degradation of material of first stage rotor blades on aircraft gas turbine M 601, cast of high temperature superalloy ZHS6K, having the nominal chemical composition: (wt. %) 0.16C, 10.75Cr, 4.75Co, 4.15Mo, 5W, 2.85Ti, 5.5Al, Zr, B, Ce, Nickel base.

Key words in English

Turbine Blade, Ni-base Superalloy, ŽS6K, Microstructure

Authors

NĚMEC, K.; PODRÁBSKÝ, T.; HAKL, J.; VLASÁK, T.; MAN, O.

RIV year

2005

Released

20. 9. 2005

Publisher

VUT v Brně

Location

Brno

ISBN

80-214-2984-4

Book

JUNIORMAT 05

Edition number

1

Pages from

279

Pages to

282

Pages count

4

BibTex

@inproceedings{BUT15760,
  author="Karel {Němec} and Tomáš {Podrábský} and Jan {Hakl} and Tomáš {Vlasák} and Ondřej {Man}",
  title="DEGRADATION OF TURBINE BLADE OFDURING SERVICE",
  booktitle="JUNIORMAT 05",
  year="2005",
  number="1",
  pages="4",
  publisher="VUT v Brně",
  address="Brno",
  isbn="80-214-2984-4"
}