Analysis of material removal on radial compressor wheel of aircraft engine after finishing production operations using CMM

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F18%3A00325212" target="_blank" >RIV/68407700:21220/18:00325212 - isvavai.cz</a>

Výsledek na webu

<a href="http://www.mmscience.eu/november-2018.html#201818" target="_blank" >http://www.mmscience.eu/november-2018.html#201818</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.17973/MMSJ.2018_11_201818" target="_blank" >10.17973/MMSJ.2018_11_201818</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Analysis of material removal on radial compressor wheel of aircraft engine after finishing production operations using CMM

Popis výsledku v původním jazyce

This paper deals with the dimensional analysis of the turboprop aircraft engine radial compressor wheel. The radial compressor wheel is very complex component. This part is manufactured by turning and five-axis milling technology. Due to the high stress of this part in service life, the residual stress in the surface layer is important. Desirable are the compressive stress levels to prevent cracks. For this reason, research is being carried out on technologies that influence the surface layer. They are the finishing technologies vibrational tumbling and superfinishing. The article describes the method used to measure the thickness variation of blade of the compressor wheel after vibrational tumbling and superfinishing. In terms of shape complexity a coordinate measuring machine with a rotary table was used.

Název v anglickém jazyce

Analysis of material removal on radial compressor wheel of aircraft engine after finishing production operations using CMM

Popis výsledku anglicky

This paper deals with the dimensional analysis of the turboprop aircraft engine radial compressor wheel. The radial compressor wheel is very complex component. This part is manufactured by turning and five-axis milling technology. Due to the high stress of this part in service life, the residual stress in the surface layer is important. Desirable are the compressive stress levels to prevent cracks. For this reason, research is being carried out on technologies that influence the surface layer. They are the finishing technologies vibrational tumbling and superfinishing. The article describes the method used to measure the thickness variation of blade of the compressor wheel after vibrational tumbling and superfinishing. In terms of shape complexity a coordinate measuring machine with a rotary table was used.

Druh

J_SC - Článek v periodiku v databázi SCOPUS

CEP obor

—

OECD FORD obor

20301 - Mechanical engineering

Projekt

<a href="/cs/project/TH01011405" target="_blank" >TH01011405: Zvyšování životnosti a možnosti oprav lopatkových dílů kompresoru z Ti6Al4V v turbovrtulových motorech</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2018

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

MM Science Journal

ISSN

1803-1269

e-ISSN

1805-0476

Svazek periodika

4_2018

Číslo periodika v rámci svazku

4

Stát vydavatele periodika

CZ - Česká republika

Počet stran výsledku

5

Strana od-do

2521-2525

Kód UT WoS článku

—

EID výsledku v databázi Scopus

2-s2.0-85057342204