Failure analysis of engine attachment support and hydraulic reservoir guard of an aircraft

Madan, M and Bhuvana, R and Sujata, M and Venkataswamy, MA and Bhaumik, SK (2009) Failure analysis of engine attachment support and hydraulic reservoir guard of an aircraft. Project Report. National Aerospace Laboratories, Bangalore, India.

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

Abstract

Damaged components-starboard turnbuckle engine attachment support and hydraulic reservoir guard belonging to an aircraft were analyzed. Analysis showed that the hydraulic reservoir guard material had suffered severe heat effects and as a result, the guard material got cracked/fractured. There were no evidences of progressive failure such as fatigue or corrosion or stress corrosion cracking. Also, no material defects were found responsible for the failure. Evidences suggest that the engine attachment support had deformed due to overload. A detailed analysis of the failure is presented in this report.

Item Type: Monograph (Project Report)
Uncontrolled Keywords: Aircraft;Hydraulic reservoir guard;Heat effect;Overload
Subjects: AERONAUTICS > Aeronautics (General)
CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
Depositing User: Users 11 not found.
Date Deposited: 18 Jul 2011 05:36
Last Modified: 18 Jul 2011 05:36
URI: http://nal-ir.nal.res.in/id/eprint/9418

Actions (login required)

View Item View Item