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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 |
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 |