Centre Fuselage Metal Cover Weight Optimization of Combat Aircraft using CFC |
Author(s): |
| Kasi Vishwanath MH , Nagarjuna College of Engineering and Technology; Balaji Y S, Nagarjuna College of Engineering and Technology; Prabhakar C G, Nagarjuna College of Engineering and Technology |
Keywords: |
| CFC, Finite Element Methods, and Isotropic Plates |
Abstract |
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The hydraulic, electrical, avionics and ECS systems are to regular monitoring and maintain is very much required, where the doors and covers also included in an war aircrafts. The covers of such aircrafts are fastener by TRIDAIR attachments, depends upon the load acting on such covers can be used to determine the number of fasteners required under different parameters(weather). The work deals with design and analysis of aircraft fuselage by using carbon fiber composite (CFC) under bending loads and given boundary conditions, CATIA V5is used as modeling tool to model cover and MSC PATRAN and NASTRAN is used for analysis. To validate the results obtained from the NASTRAN, the theoretical calculations are done, CFC covers are better withstanding capacity compared with metallic and the weight on cover is reduced nearly 50% as compared to metallic cover. |
Other Details |
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Paper ID: IJSRDV7I50423 Published in: Volume : 7, Issue : 5 Publication Date: 01/08/2019 Page(s): 847-850 |
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