Analysis of repaired gas turbine and compressor blades

Analysis of repaired gas turbine and compressor blades

In order to reach desired levels of efficiency and power output of jet engines, advanced gas turbine and compressor blades made from Ti‐6AL‐4V alloy operate at very high temperatures (up to 600°C) and speeds (up to 10000 rpm) [3–4]. Pressure of springing streams and inertial forces are main reasons...

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Bibliographic Details
Main Authors: Alexander Tishkunov, Sergejs Gluhihs, Aleksandrs Korjakins, Andris Popovs
Format: Article
Language:English
Published: Vilnius Gediminas Technical University 2008-06-01
Series:Aviation
Subjects:
turbine blade
compressor blade
modelling
streams
internal cooling
damage simulation
Online Access:https://journals.vgtu.lt/index.php/Aviation/article/view/6735

Internet

https://journals.vgtu.lt/index.php/Aviation/article/view/6735

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