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Methods of the blade release at casings containment capability
- Authors: Baluev B.A.1
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Affiliations:
- “Baranov’s Central Institute of Aircraft Engine Designing”, Moscow
- Issue: Vol 7, No 3 (2008): Special Issue
- Pages: 119-125
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/621
- DOI: https://doi.org/10.18287/2541-7533-2008-0-3(16)-119-125
- ID: 621
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Abstract
The review and the analysis of existinq methods blades is presented. The constructive decisions and technique of definition of additional loading conditions for maintenance of destruction of fan blade on the set frequencies of rotation are proposed. The experimental investigations of determination of a efficiency control by destruction of fan blades for maintenance of check of casings containment capability are carried out.
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About the authors
B. A. Baluev
“Baranov’s Central Institute of Aircraft Engine Designing”, Moscow
Author for correspondence.
Email: vest@ssau.ru
Russian Federation
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