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Design of bimetallic impeller for gas turbine
- Authors: Magerramova L.A.1
-
Affiliations:
- Central Institute of Aviation Motors
- Issue: Vol 10, No 2 (2011)
- Pages: 177-185
- Section: MECHANICAL ENGINEERING AND POWER ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/1680
- DOI: https://doi.org/10.18287/2541-7533-2011-0-2(26)-177-185
- ID: 1680
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Abstract
A bimetallic impeller structure obtained by HIP made out of powder and cast Ni-base super alloys was developed. The strength estimations were carried out by the ANSYS program with the help of 2D models.
About the authors
L. A. Magerramova
Central Institute of Aviation Motors
Author for correspondence.
Email: MAG@CIAM.ru
Candidate of Technical Sciences
Senior Researcher
Head of Group
Russian FederationReferences
- J.-P. Auger, G. Raisson, M. Pierronet. Design and Manufacture of Engineered Components by HIP. /Hot Isostatic PressingTheory and Applications. Proceedings of the Third International Conference. Elsevier Applied Science, 1992.
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- Magerramova L. А., Kratt Е. P., Zakharova Т. P., Yacinsky V. V. The structural and technological design feature of bimetallic blisks for high temperature gas turbine aviation engines: 2nd European conference for aerospace sciences (EUCASS). Brussels. 2007.
- Magerramova L. A., Shorr B. F., Melnikova G. V., Zakharova T. P. Problems of dynamic characteristics and damping of bimetallic gas turbine blisks produced by HIP technology: Proceeding of international conference /HIP’05. Paris. 2005. С. 97.
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