| Autor: |
Grinev, M. A., Anoshkin, A. N., Pisarev, P. V., Zuiko, V. Yu., Shipunov, G. S. |
| Předmět: |
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| Zdroj: |
AIP Conference Proceedings; 2016, Vol. 1783 Issue 1, p1-4, 4p, 1 Diagram, 2 Graphs |
| Abstrakt: |
The present work is devoted to the detailed stress-strain analysis of the composite outlet guide vane (OGV) for aircraft engines with a special focus on areas with twisted layers where the initiation of high interlaminar stresses is most expected. Various polymer composite materials and reinforcing schemes are researched. The technological scheme of laying-out of anisotropic plies and the fastening method are taken into account in the model. The numerical simulation is carried out by the finite element method (FEM) with the ANSYS Workbench software. It is shown that interlaminar shear stresses are most dangerous. It is found that balanced carbon fiber reinforced plastic (CFRP) with the [0°/±45°] reinforcing scheme allows us to provide the double strength margin under working loads for the developed OGV. [ABSTRACT FROM AUTHOR] |
| Databáze: |
Complementary Index |
| Externí odkaz: |
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