Fracture of aircraft titanium alloys under high-frequency loading
Abstract The paper is devoted to the problem of fatigue failure of two-phase titanium alloy VT3-1 under the action of high-frequency cyclic loading. Samples for the tests were made from the compressor disk of aviation engine D30-Ku installed on Tupolev Tu-154 planes. Repeated alternating loading was...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Springer
2023-02-01
|
| Series: | SN Applied Sciences |
| Subjects: | |
| Online Access: | https://doi.org/10.1007/s42452-022-05266-8 |
| _version_ | 1811171550702862336 |
|---|---|
| author | Alexander D. Nikitin Pavel S. Shesterkin Sergey S. Lopatin |
| author_facet | Alexander D. Nikitin Pavel S. Shesterkin Sergey S. Lopatin |
| author_sort | Alexander D. Nikitin |
| collection | DOAJ |
| description | Abstract The paper is devoted to the problem of fatigue failure of two-phase titanium alloy VT3-1 under the action of high-frequency cyclic loading. Samples for the tests were made from the compressor disk of aviation engine D30-Ku installed on Tupolev Tu-154 planes. Repeated alternating loading was carried out by displacements of small amplitude at 20 kHz, coinciding with the first harmonic of longitudinal elastic vibrations of the sample. Analysis of specimen fracture surfaces shows predominant subsurface fracture. Analysis of areas of fatigue nucleation allows identifying elements of microstructure associated with crack nucleation. The results of the study can be used in the interpretation of fracture scenarios of structural elements in operation. Increasing the resource of products under such loads is possible through the use of damping layers or tapes, where possible. |
| first_indexed | 2024-04-10T17:16:58Z |
| format | Article |
| id | doaj.art-228f4a06d28f40c9bd48be0a8cbabc0f |
| institution | Directory Open Access Journal |
| issn | 2523-3963 2523-3971 |
| language | English |
| last_indexed | 2024-04-10T17:16:58Z |
| publishDate | 2023-02-01 |
| publisher | Springer |
| record_format | Article |
| series | SN Applied Sciences |
| spelling | doaj.art-228f4a06d28f40c9bd48be0a8cbabc0f2023-02-05T12:20:37ZengSpringerSN Applied Sciences2523-39632523-39712023-02-015211110.1007/s42452-022-05266-8Fracture of aircraft titanium alloys under high-frequency loadingAlexander D. Nikitin0Pavel S. Shesterkin1Sergey S. Lopatin2Moscow Aviation Institute, National Research UniversityMoscow Aviation Institute, National Research UniversityMoscow Aviation Institute, National Research UniversityAbstract The paper is devoted to the problem of fatigue failure of two-phase titanium alloy VT3-1 under the action of high-frequency cyclic loading. Samples for the tests were made from the compressor disk of aviation engine D30-Ku installed on Tupolev Tu-154 planes. Repeated alternating loading was carried out by displacements of small amplitude at 20 kHz, coinciding with the first harmonic of longitudinal elastic vibrations of the sample. Analysis of specimen fracture surfaces shows predominant subsurface fracture. Analysis of areas of fatigue nucleation allows identifying elements of microstructure associated with crack nucleation. The results of the study can be used in the interpretation of fracture scenarios of structural elements in operation. Increasing the resource of products under such loads is possible through the use of damping layers or tapes, where possible.https://doi.org/10.1007/s42452-022-05266-8Titanium alloyFatigue failureCompressor diskMicrostructureCrack initiationCrack growth |
| spellingShingle | Alexander D. Nikitin Pavel S. Shesterkin Sergey S. Lopatin Fracture of aircraft titanium alloys under high-frequency loading SN Applied Sciences Titanium alloy Fatigue failure Compressor disk Microstructure Crack initiation Crack growth |
| title | Fracture of aircraft titanium alloys under high-frequency loading |
| title_full | Fracture of aircraft titanium alloys under high-frequency loading |
| title_fullStr | Fracture of aircraft titanium alloys under high-frequency loading |
| title_full_unstemmed | Fracture of aircraft titanium alloys under high-frequency loading |
| title_short | Fracture of aircraft titanium alloys under high-frequency loading |
| title_sort | fracture of aircraft titanium alloys under high frequency loading |
| topic | Titanium alloy Fatigue failure Compressor disk Microstructure Crack initiation Crack growth |
| url | https://doi.org/10.1007/s42452-022-05266-8 |
| work_keys_str_mv | AT alexanderdnikitin fractureofaircrafttitaniumalloysunderhighfrequencyloading AT pavelsshesterkin fractureofaircrafttitaniumalloysunderhighfrequencyloading AT sergeyslopatin fractureofaircrafttitaniumalloysunderhighfrequencyloading |