High pressure turbine rotor blades heating duration experimental estimates prior to the bypass turbofan engine start for reducing thermal stresses

A. A. Ametov; B. A. Chichkov

Civil Aviation High Technologies
Nauchnyi Vestnik MGTU GA

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Ametov A.A., Chichkov B.A. High pressure turbine rotor blades heating duration experimental estimates prior to the bypass turbofan engine start for reducing thermal stresses. Civil Aviation High Technologies. 2024;27(1):8-17. https://doi.org/10.26467/2079-0619-2024-27-1-8-17

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This work is licensed under a Creative Commons Attribution 4.0 License.

ISSN 2079-0619 (Print)
ISSN 2542-0119 (Online)

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Eliseev B.P.

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About the Authors

A. A. Ametov
Moscow State Technical University of Civil Aviation
Russian Federation

Aziz A. Ametov - Postgraduate Student, Moscow State Technical University of Civil Aviation.

Moscow

B. A. Chichkov
Moscow State Technical University of Civil Aviation
Russian Federation

Boris A. Chichkov - Doctor of Technical Sciences, Professor, Professor of the Aircraft Engines Chair, Moscow State Technical University of Civil Aviation.

Moscow