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Methods in forcing a gas turbine engine
| Authors: Pismennyi V.L. | Published: 17.09.2024 |
| Published in issue: #9(774)/2024 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: gas turbine engine, stoichiometric engine, hypersonic aviation, hyperboost, turbine boost, turbojet engine, methods of boosting a gas turbine engine |
Methods and techniques used in increasing gas temperature in front of the gas turbine engine turbine
| Authors: Pismennyi V.L. | Published: 05.06.2023 |
| Published in issue: #6(759)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: heat resistance of materials, blade cooling, gas temperature, circulating heat exchanger, heat-shielding coatings, gas turbine engine, air-liquid cooling |
Digital Simulation Verification and Validation
| Authors: Salnikov A.V., Frantsuzov M.S., Vinogradov K.A., Pyatunin K.R., Nikulin A.S. | Published: 09.09.2022 |
| Published in issue: #9(750)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: verification and validation, mathematical model, computer simulation, digital twin, gas turbine engine |
Digital Twins — a Platform for Aircraft Engine Lifecycle Management
| Authors: Salnikov A.V., Gordin M.V., Shmotin Yu.N., Nikulin A.S., Makarov P.V., Frantsuzov M.S. | Published: 01.04.2022 |
| Published in issue: #4(745)/2022 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: digit twin, gas turbine engine, requirement matrix, digital platform, life cycle, mathematical modeling |
Analysis of Methods for Reducing Power Losses in the Compressor Impeller when Balancing the Turbine Generator Rotor at the Operating Speed
| Authors: Kalashnikov D.A., Pugachuk A.S., Kalashnikova E.O., Chernyshev A.V. | Published: 15.01.2021 |
| Published in issue: #2(731)/2021 | |
| Category: Energy and Electrical Engineering | Chapter: Vacuum and Compressor Technology and Pneumatic Systems | |
| Keywords: rotor balancing, gas turbine engine, power losses, field test |
A Method for Determining the Conversion Factors to Convert Gas Turbine Engine Parameters to Normal Values Based on Test Results in a Thermal Pressure Chamber
| Authors: Grigoriev V.A., Kalabukhov D.S. | Published: 16.12.2019 |
| Published in issue: #12(717)/2019 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
| Keywords: gas turbine engine, normal values of parameters, experimental thermal pressure chamber, conversion factor, production tests, control law |
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 |
Trial Test Results on Intake Manifold Mounting Elements of the Combustion Chamber of the NK-38ST Gas Turbine Engine
| Authors: Baklanov A.V., Neumoin S.P., Vakhitov A.R. | Published: 28.04.2018 |
| Published in issue: #4(697)/2018 | |
| Category: Energy and Electrical Engineering | Chapter: Turbomachines and Combination Turbine Plants | |
| Keywords: fuel manifold, mounting system, combustion chamber, gas turbine engine, fuel pipe strain-gaging |