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Damping devices in the construction of compressor vanes of engines of the "NK" family
- Authors: Frolov V.A.1, Belousov A.I.1
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Affiliations:
- Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
- Issue: Vol 10, No 3-3 (2011): Special Issue
- Pages: 242-250
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6887
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-242-250
- ID: 6887
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Abstract
Here, I present the designs of compressor vanes with a damping device, developed in a research laboratory at the Department of "Construction and design of aircraft engines". The results of the use of dampers in GTD NK-12, NK-14 and NK-8, "E" and "P" products, are shown.
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About the authors
V. A. Frolov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Author for correspondence.
Email: kpdla@ssau.ru
Candidate of technical sciences
Associate Professor at the Department of "Construction and design of aircraft engines"
A. I. Belousov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: kpdla@ssau.ru
Doctor of technical sciences
Professor at the Department of "Construction and design of aircraft engines"
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