Analysis of FOD on an LPC I stage rotor blade of an aircraft

Suresh Kumar, M and Madan, M and Venkataswamy, MA and Sujata, M and Bhaumik, SK (2006) Analysis of FOD on an LPC I stage rotor blade of an aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.

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Abstract

A damaged I stage LPC rotor blade belonging to an aeroengine was analyzed. The damage occurred as a result of impact of foreign object on the concave surface at the leading edge near the tip. Analysis of the damaged region showed that the foreign object was an aluminium alloy piece. The shape of the object could not be determined.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aeroengine;Compressor blade;FOD;Metallic object
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
Depositing User: Ms. Alphones Mary
Date Deposited: 27 Jul 2011 14:13
Last Modified: 27 Jul 2011 14:13
URI: http://nal-ir.nal.res.in/id/eprint/9694

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