DEGRADATION OF TURBINE BLADE OFDURING SERVICE
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F05%3APU51795" target="_blank" >RIV/00216305:26210/05:PU51795 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
DEGRADATION OF TURBINE BLADE OFDURING SERVICE
Original language description
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.
Czech name
Degradace turbínové lopatky v průběhu provozu
Czech description
Příspěvek je zaměřen na strukturní změny litých lopatek ze superslitiny ŽS6K vlivem provozu v leteckém motoru M 601.
Classification
Type
D - Article in proceedings
CEP classification
JG - Metallurgy, metal materials
OECD FORD branch
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Result continuities
Project
<a href="/en/project/GA106%2F02%2F1088" target="_blank" >GA106/02/1088: Optimization of the chemical composition and heterogeneity, structure, properties and use of cast nickel alloys for the combustion turbine production</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2005
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
JUNIORMAT 05
ISBN
80-214-2984-4
ISSN
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e-ISSN
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Number of pages
4
Pages from-to
279-282
Publisher name
VUT v Brně
Place of publication
Brno
Event location
Brno
Event date
Sep 20, 2005
Type of event by nationality
CST - Celostátní akce
UT code for WoS article
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