Analysis of Labyrinth rings and pins of an aeroengine

Bhaumik, SK (2003) Analysis of Labyrinth rings and pins of an aeroengine. Project Report. National Aerospace Laboratories, Bangalore.

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

Abstract

Labyrinth rings/pins belonging to a particular type of aeroengine were sent to the laboratory for analysis. Examination revealed presence of fatigue crack in the pins from all the three engines. Fatigue cracks were found to have initiated at the deformation marks at about 4.5 mm from the pinhead. It appears most probable that these depression marks were formed by hot deformation at the disc/Labyrinth interface due to axial movement of the labyrinth ring.

Item Type: Proj.Doc/Technical Report (Project Report)
Uncontrolled Keywords: Aeroengine labyrinth rings;labyrinth pins;fatigue;hot deformation
Subjects: AERONAUTICS > Aeronautics (General)
CHEMISTRY AND MATERIALS > Chemistry and Materials (General)
Division/Department: Materials Science Division
Depositing User: Mrs Manoranjitha M D
Date Deposited: 14 Jul 2011 16:39
Last Modified: 14 Jul 2011 16:39
URI: http://nal-ir.nal.res.in/id/eprint/9361

Actions (login required)

View Item