Fiber reinforced polymers have various applications in the automotive and aerospace industries. This project focuses on development of an intelligent material design methodology using machine learning and evolutionary optimization algorithms that will provide the end user optimized permutations of g
Developmment of an intelligent design methodology for composite materials for various applications
Fiber reinforced polymers have various applications in the automotive and aerospace industries. This project focuses on development of an intelligent material design methodology using machine learning and evolutionary optimization algorithms that will provide the end user optimized permutations of glass and carbon fiber reinforced composite laminates under the given constraints of cost and mechanical properties. The advantages of the proposed work include time and cost savings as it would limit the amount of experimentations required by the end-user during the composite design process as this would help narrow down the choices available to the end-user to the best ones. The steps involved in the process include a market survey to collect data of available composite fabrics, the generation of fabric properties data using a commercial code and the development of a machine learning based optimization methodology for optimizing the composite material design. Afterwards analysis for a medium UAV wing is to be carried out where an optimum laminate configuration will be provided using the algorithm. Furthermore, physically testing will be carried out of the configuration under ASTM standards to give real life results of the configuration.
The objective of the project is the development of a machine learning based design strategy for layered woven fabric composites. The developed algorithm will be able to optimize the material and layup of the composite given the maximum allowed cost of the composite material. The tentative outcomes of our project include:
This project application is the use of composite laminate as wing of a medium UAV with a MTOW of 15 kg, an optimized laminate configuration will be predicted using the algorithm for the wing of the UAV and will be analyzed using FEA and physical experimentation.
The final deliverable obtained is an algorithm derived from the methodology which is able to provide the optimum bending stiffness for a hybrid composite laminate under a specified cost constraint or provide minimum cost for a specified bending stiffness constraint whichever condition is provided to the algorithm with the laminate comprised of carbon and glass fiber laminae and embedded core material for aerospace, automotive or structural applications.
| Item Name | Type | No. of Units | Per Unit Cost (in Rs) | Total (in Rs) |
|---|---|---|---|---|
| Release Agent | Equipment | 2 | 3030 | 6060 |
| Sealing Tape | Equipment | 2 | 990 | 1980 |
| Peel Ply | Equipment | 2 | 2096 | 4192 |
| Infusion Mesh | Equipment | 2 | 1768 | 3536 |
| Resin Infusion Spiral | Equipment | 1 | 465 | 465 |
| Infusion Silicon Connector | Equipment | 6 | 757 | 4542 |
| Vacuum bagging | Equipment | 2 | 498 | 996 |
| Vacuum hose | Equipment | 2 | 1386 | 2772 |
| Resin catch pot | Equipment | 1 | 18637 | 18637 |
| Line clamp | Equipment | 2 | 1223 | 2446 |
| resin | Equipment | 3 | 2707 | 8121 |
| Hardner | Equipment | 3 | 3851 | 11553 |
| Shipping | Miscellaneous | 1 | 10000 | 10000 |
| Shipping | Equipment | 1 | 4700 | 4700 |
| Total in (Rs) | 80000 |
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