Frequency Screening of First Stage Turbine Blades in the T56-A-7B Engine
Abstract
Historically it has been difficult to obtain accurate and repeatable frequency data for the first bending mode of turbine blades. This report summarises the technique used by AMRL to screen first stage T56-A-713 turbine blades for the Royal Australian Air Force as part of an investigation into the failure of these blades in service.
Document Details
- Document Type
- Technical Report
- Publication Date
- Aug 01, 1999
- Accession Number
- ADA369721
Entities
People
- Andrew Becker
- Paul Marsden
Organizations
- Defence Science and Technology Group