Failure Investigation of 1st Stage LPCR Blade Pertaining to Aero-Engine No. 8831010

Munda, Parikshit and Das, Swapan K and Husain, M M and Ghosh Chowdhury, S and Parida, N (2011) Failure Investigation of 1st Stage LPCR Blade Pertaining to Aero-Engine No. 8831010. Other (TMP). National Metallurgical Laboratory, Jamshedpur. (Submitted)

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Abstract

The 1st stage LPCR blade of aero-engine no.8831010 got damaged. Metallurgical analysis has been carried out to find out the cause of damage. The blade is made of Ti based
alloy having and + structure. SEM-EDS analysis showed that the blade was damaged due to an impact of an iron bearing metallic material.

Item Type: Project Reports (Other (TMP))
Uncontrolled Keywords: LPCR Blade, Shear fracture, Ti alloy, alpha and alpha+beta structure
Subjects: Materials Science
Divisions: Material Science and Technology
Depositing User: Dr. A K Sahu
Date Deposited: 19 Dec 2011 07:23
Last Modified: 16 Jun 2021 18:14
URI: http://eprints.nmlindia.org/id/eprint/4442

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