FEM Simulation of Different Engine Mount Models in an Aircraft Piston Diesel Engine
Artykuł w czasopiśmie
MNiSW
100
Lista 2021
| Status: | |
| Autorzy: | Magryta Paweł, Pietrykowski Konrad, Borowiec Piotr |
| Dyscypliny: | |
| Aby zobaczyć szczegóły należy się zalogować. | |
| Rok wydania: | 2022 |
| Wersja dokumentu: | Drukowana | Elektroniczna |
| Język: | angielski |
| Numer czasopisma: | 5 |
| Wolumen/Tom: | 16 |
| Strony: | 230 - 241 |
| Impact Factor: | 1,1 |
| Web of Science® Times Cited: | 0 |
| Scopus® Cytowania: | 0 |
| Bazy: | Web of Science | Scopus |
| Efekt badań statutowych | NIE |
| Finansowanie: | This work has been realized in cooperation with The Construction Office of WSK “PZL-KALISZ” S.A.” and is part of Grant Agree-ment No. POIR.01.02.00-00-0002/15 financed by the Polish National Centre for Research and Development. The project/research was financed in the ramework of the project Lublin University of Technology – Regional Excellence Initia-tive, funded by the Polish Ministry of Sci- ence and Higher Education (contract no. 030/RID/2018/19). |
| Materiał konferencyjny: | NIE |
| Publikacja OA: | TAK |
| Licencja: | |
| Sposób udostępnienia: | Otwarte czasopismo |
| Wersja tekstu: | Ostateczna wersja opublikowana |
| Czas opublikowania: | W momencie opublikowania |
| Data opublikowania w OA: | 1 listopada 2022 |
| Abstrakty: | angielski |
| he article presents the results of numerical simulations using the FEM (Finite Element Method) of the engine mount strength for mounting an aircraft diesel engine with opposite pistons called PZL-100. Four versions of the mount prepared by aircraft engine producer WSK “PZL-Kalisz” company were analyzed. Tests were performed in Catia v5 software in the Generative Structure Analysis module. The boundary conditions were engine gravity force, propeller thrust force, and propeller torque. S235JR steel was defined as the material. A design grid with tetrahedral elements with a single element size of 2 mm was used. As part of the simulation study, four structural solutions for the test engine mounts were calculated in terms of strength. The results of stress maps and the mag- nitude of deformation of the mount elements were compared. Based on the obtained results, one of the mount versions was recommended for actual fabrication. |
