Failure analysis of Torque plate of an aircraft brake unit

Madan, M and Sujata, M and Venkataswamy, MA and Bhaumik, SK (2008) Failure analysis of Torque plate of an aircraft brake unit. Project Report. National Aerospace Laboratories, Bangalore, India.

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

Abstract

Evidences suggest that the torque plate has failed by stress corrosion cracking (SCC). Microstructural study revealed that the SCC was promoted in the component due to unsatisfactory microstructure resulting from overheating during solution heat treatment. The situation was found to be further aggravated due to wrong fabrication of the component from the wrought stock. A detailed analysis of the failure is presented in this report and a few recommendations suggested for prevention of similar failure.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aircraft;Brake unit;Torque plate;SCC;Overheated structure; Wrong fabrication
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
Depositing User: Ms. Alphones Mary
Date Deposited: 20 Jul 2011 09:57
Last Modified: 20 Jul 2011 09:57
URI: http://nal-ir.nal.res.in/id/eprint/9484

Actions (login required)

View Item