Search
All articles by "Sapronov D.V."
Constructing a turbine blade damage accumulation model for accounting the long-term operating time
| Authors: Sapronov D.V., Khudyakova A.D., Semenov A.V., Kosovsky D.V., Selivanov A.N. | Published: 16.11.2024 |
| Published in issue: #11(776)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: damage accumulation model, turbine blade service life, operating time, long-term strength, material creep |
Methods of Creating Functional Models of Gas Turbine Engine Parts by Means of Numerical Modeling and Machine Learning Algorithms Using a Turbine Disk as an Example
| Authors: Reznik S.V., Sapronov D.V., Vasilyev B.E., Semenov A.V. | Published: 26.11.2019 |
| Published in issue: #11(716)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: gas turbine engine, turbine disk, functional model, machine learning |
The Determination of Rational Parameters of Lock Joints of Ceramic Blades with a Metal Disk in Advanced Aircraft Gas Turbine Engines. Part II. Testing of the Rotor Model
| Authors: Reznik S.V., Sapronov D.V., Karimbaev T.D., Mezencev M.A. | Published: 23.07.2019 |
| Published in issue: #7(712)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: gas turbine engine, impeller, lock joint, ceramic blade |
The Determination of Rational Parameters of Lock Joints of Ceramic Blades with a Metal Disk in Advanced Aircraft Gas Turbine Engines. Part I. Models of Mechanical and Thermal Contact of Ceramic and Metal Parts of the Turbine Impeller
| Authors: Reznik S.V., Sapronov D.V., Karimbaev T.D., Mezencev M.A. | Published: 18.06.2019 |
| Published in issue: #6(711)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: gas turbine engine, lock joint, ceramic blades, contact interaction |
Designing interlocking joints between ceramic blades and a gas turbine metal disc
| Authors: Reznik S.V., Sapronov D.V. | Published: 08.09.2014 |
| Published in issue: #9(654)/2014 | |
| Category: Calculation and Design of Machinery | |
| Keywords: gas turbine, ceramic blade, hot-pressed silicon nitride OTM-914 |
Study of the static strength of a ceramic blade inserted in a gas turbine metal disk
| Authors: Reznik S.V., Sapronov D.V. | Published: 22.04.2014 |
| Published in issue: #4(649)/2014 | |
| Category: Calculation and Design of Machinery | |
| Keywords: gas turbine engine, turbine, ceramic blade, hot-pressed silicon nitride OTM-914, brittle fracture criterion |