Course # 602 –
Aircraft Structures and Repair Analysis II – Intermediate
When a student completes this course she/he should be able to:
- be familiar with buckling / crippling damaged structural repair
- check the repair for inter-rivet buckling
- determine proper corrosion and other blend-outs
- come up with beam repairs to restore the bending capability of damaged structure
- restore the compression capacity of structure before damage
- understand coldworking of holes, shot-peening and other life extension techniques
Prerequisite:
- preferably taken FATIGUE CONCEPTS 601 or Boeing/Airbus Beginners Structural Repair training
- some experience in OEM-approved aircraft structural repairs
- a Bachelor’s Degree in Engineering or equivalent experience
Who should take this training:
Managers / Engineers / Materials Scientists / Inspectors / DERs in:
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From Industries including but not limited to:
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Syllabus
- Review of Fundamentals of Aircraft Structures Analysis
- Sign Convention
- Aluminum, Steel, Magnesium and Titanium Properties
- Which Alloys are Used Where. And Why.
- Fatigue Fundamentals
- Basic Repair Guidelines
- Beam
- Design Philosophies
- Centroid Shift
- Moments of Inertia
- Steps to Draw a Mohr’s Circle
- Bending Stress Distribution
- Off-Axis Moment
- Elastic Flexural Formula
- Curved Beam
- Composite Beams
- Buckling
- Fundamentals – Euler Equation
- End Fixity Coefficients
- Euler-Engesser Column Buckling Equation
- Inter-rivet Buckling
- Local Peaking of Stresses Under Compression Loading
- Crippling
- Gerard Method
- Needham Method Advantages
- Utilization of Bulbs, Lips, Additional Bends
- Johnson-Euler Buckling
- Repair Philosophies
- Beam Repair
- Examples
- Fatigue Crack Propagation Life Extension Techniques
- Cold-working of Holes
- Shot-Peening Considerations
- Laser Shock Peening
This syllabus is for guidance only; the syllabus may change retaining the current flavor.