Email this article Weight optimization principles for turbine blade shroud platform
- Authors: Belousov A.I.1, Nazdrachev S.V.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 59, No 1 (2016)
- Pages: 51-57
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/229557
- DOI: https://doi.org/10.3103/S1068799816010086
- ID: 229557
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Abstract
The paper describes the development of NK-family engine shrouded turbine blades. Weight optimization principles are formulated with account for strength and manufacturability limits.
About the authors
A. I. Belousov
Samara State Aerospace University
Author for correspondence.
Email: aibelousov@mail.ru
Russian Federation, shosse Moskovskoe 34, Samara, 443086
S. V. Nazdrachev
Samara State Aerospace University
Email: aibelousov@mail.ru
Russian Federation, shosse Moskovskoe 34, Samara, 443086
