Now a days composite material is used in our day to day life due to its light weight and high strength to weight ratio .Fabrication and due to easy machinability students can able to fabricate it in their own labrotory.Students can able to fabrication of product by using hand lay-up, Spray up and vacuum bag technique.
Composite fabrication practice
Composite fabrication practice
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Code(Credit) : 2-2-0
| Scheme | Skill for Success (SFS) |
| NSQF Level | 5 |
| Duration | 4 Months |
| Sector | Aerospace and Aviation |
| Occupations | Composite manufacturing technician |
| Entry Qualification | BSc in Physics/Chemistry, BTech |
| Minimum Age | 19 Years |
| Aligned to (QP) | |
Course Objectives:
The objectives of this subject are:
- Learn design of a composite material and design a system using the composite.
- To test the composite and control quality.
After completing this program-
- know composite materials, synthesis, characterization, properties and applications.
- be able to develop and develop an understanding of perspective on SDGs.
- be an expert on the designing of different composite moulds by Catia.
- implement activities and organize resources to meet desired outcomes.
- Can join the industry as Composite Manufacturing Trainee and will progress further as a Composite Design engineer then to Composite Project manager.
- Can become an entrepreneur in the related field.
Learning Record:
The trainee will submit a Practice/Project/Learning record after each class/session.
Assessment Process:
- The trainee should score a minimum of 70% in the overall assessment.
- The assessment of the theory/knowledge will be based on a written test/viva-voce or both while the skill test shall be hands-on practical.
Course Syllabus/Contents:
All Modules
| 1 | Monitoring material property variations over time |
| 2 | Define minimum standards for aerospace grade fiber, resin, fabric/braid |
| 3 | Define minimum standards for aerospace prepreg – Material qualification, material specification, process control document |
| 4 | Factors affecting Quality of Composites made by hand lay-up |
| 5 | Factors affecting fabrication factors, stacking sequence, fiber volume fraction, cure |
| 6 | Material selection criteria for new generation aircraft |
| 7 | Structural Requirements for Certification, |
| 8 | Material Qualification Procedures, Material Property Development |
| 9 | Material Screening and Selection, |
| 10 | Material and Process Specification Development |
| 11 | Material and Process Control,QCs for Composite Part Manufacturing,Material Acceptance |
| 12 | Mechanical test of laminates and sandwiches |
| 13 | Test for adhesives and sealants |
| 14 | Chemical and physical tests for material composition |
| 15 | Thermal analysis for composite materials |
| 16 | Aging tests by chemical aging |
| 17 | Thermal and humidity aging |
| 18 | Radiation aging test |
| 19 | Reappear test, fire and smoke test |
| 20 | Non destructive test, Ultrasonic Phased Array test,2D X-Ray test on field |
Reference Book :
- Geographic Information Systems for Transportation: Principles and Applications (Spatial Information Systems) by Harvey J Miller and Shih-Lung Shaw.
- Remote Sensing of Land Use and Land Cover: Principles and Applications (Remote Sensing Applications Series)” by Chandra P Giri.
- Manual of Remote Sensing: Principles and Applications of Imaging Radar by Floyd M Henderson and Anthony J Lewis.
Session Plan:
Section 1
- Monitoring material property variations over time
Section 2
- Define minimum standards for aerospace grade fiber, resin, fabric/braid
Section 3
- Define minimum standards for aerospace prepreg – Material qualification, material specification, process control document
Section 4
- Factors affecting Quality of Composites made by hand lay-up
Section 5
- Factors affecting fabrication factors, stacking sequence, fiber volume fraction, cure
Section 6
- Material selection criteria for new generation aircraft
Section 7
- Structural Requirements for Certification
Section 8
- Material Qualification Procedures, Material Property Development
Section 9
- Material selection criteria for new generation aircraft
Section 10
- Structural Requirements for Certification
Section 11
- Structural Requirements for Certification
Section 12
- Mechanical test of laminates and sandwiches
Section 13
- Test for adhesives and sealants
Section 14
- Chemical and physical tests for material composition
Section 15
- Thermal analysis for composite materials
Section 16
- Aging tests by chemical aging
Section 17
- Thermal and humidity aging
Section 18
- Radiation aging test
Section 19
- Reappear
Section 20
- Non destructive test, Ultrasonic Phased Array test, 2D X-Ray test on field
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