Analysis of failed HPTR blades of an aeroengine

Suresh Kumar, M and Madan, M and Parameswara, MA and Venkataswamy, MA and Sujata, M and Bhaumik, SK (2005) Analysis of failed HPTR blades of an aeroengine. Project Report. National Aerospace Laboratories, Bangalore.

Full text not available from this repository. (Request a copy)

Abstract

Two fractured HPTR blades belonging to an aeroengine were sent to the laboratory for investigation. The tip of the blades was damaged due to exposure to high temperature. Microstructural study suggests that the minimum temperature was in the vicinity of 1650 K. The coating was found peeled off in the affected regions due to temperature effects. There was no abnormality in the coating.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aeroengine;HPT rotor blades;high temperature;incipient melting
Subjects: AERONAUTICS > Aeronautics (General)
CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
Division/Department: Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division, Materials Science Division
Depositing User: Mrs Manoranjitha M D
Date Deposited: 20 Jul 2011 09:51
Last Modified: 20 Jul 2011 09:51
URI: http://nal-ir.nal.res.in/id/eprint/9468

Actions (login required)

View Item