Failure analysis of intermediate casing of an aeroengine

Suresh Kumar, M and Madan, M and Venkataswamy, MA and Sujata, M and Parameswara, MA and Bhaumik, SK (2006) Failure analysis of intermediate casing of an aeroengine. Project Report. National Aerospace Laboratories, Bangalore.

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

Abstract

In continuation with the earlier investigation of a particular type of aeroengine build (NAL report No. MT-FA-945-09-2005 and MT-FA-945A-01-2006), intermediate casing was also sent to the laboratory for investigation. Examination revealed a crack along the fillet of the mounting area. Fractographic examination confirmed this crack to be a fatigue crack. This corroborates the earlier findings wherein it was established that high alternating stresses and/or vibration were transmitted to No.3 bearing mounting flange through intermediate casing due to problems elsewhere in the engine.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aeroengine;intermediate casing;fatigue;vibration
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: 15 Nov 2011 09:55
Last Modified: 15 Nov 2011 09:55
URI: http://nal-ir.nal.res.in/id/eprint/9994

Actions (login required)

View Item