Bonded Repair of Aircraft Structures [E-Book] / edited by A. A. Baker, R. Jones.
The conventional approach to through-life-support for aircraft structures can be divided into the following phases: (i) detection of defects, (ii) diagnosis of their nature and significance, (iii) forecasting future behaviour-prognosis, and (iv) pre scription and implementation of remedial measures...
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Full text |
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Personal Name(s): | Baker, A. A., editor |
Jones, R., editor | |
Imprint: |
Dordrecht :
Springer,
1988
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Physical Description: |
XIII, 214 p. online resource. |
Note: |
englisch |
ISBN: |
9789400927520 |
DOI: |
10.1007/978-94-009-2752-0 |
Series Title: |
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Engineering Application of Fracture Mechanics ;
7 |
Subject (LOC): |
- 1. Introductory chapter
- 1.1 Bonded vs bolted repairs
- 1.2 Combined bonded/bolted repairs
- 1.3 Adhesives
- 1.4 Adhesive testing
- 1.5 Surface preparation
- 1.6 Environmental behaviour
- 1.7 Summary
- 2. Surface treatments for bonded repairs of metallic components
- 2.1 Introduction
- 2.2 Background
- 2.3 Structural aluminium alloys
- 2.4 Phosphoric acid anodizing
- 2.5 Chromic acid anodizing
- 2.6 Titanium alloys
- 2.7 Summary
- 3. Design and analysis of bonded repairs for metal aircraft structures
- 3.1 Introduction
- 3.2 Design of adhesive bonded repairs in thin sheet metal construction
- 3.3 Residual strength of flawed or damaged bonded joints
- 3.4 Acceptance criteria for bonded flaws and damage
- 3.5 The pitfalls of life prediction for adhesive-bonded joints
- 3.6 Surface preparation for adhesive bonded repair of metal structure
- 3.7 Conclusions
- 4. Crack patching: design aspects
- 4.1 Introduction
- 4.2 The finite element formulation
- 4.3 Repair of cracks in Mirage III lower wing skin — a design study
- 4.4 Neutral axis offset effects
- 4.5 Initial design procedures
- 4.6 Comparison with experimental and 3-D results
- 4.7 Repair of semi elliptical surface flaws
- 4.8 Repair of cracked holes
- 4.9 Repair of cracked fastener holes
- Appendix A
- 5. Theoretical analysis of crack patching
- 5.1 Introduction
- 5.2 Formulation and notation
- 5.3 Load transfer to bonded reinforcements
- 5.4 Two stage analytical solution
- 5.5 Residual thermal stress due to adhesive curing
- 5.6 Bending effects
- 5.7 Partial reinforcement
- 5.8 Conclusion
- 6. Crack patching: experimental studies, practical applications
- 6.1 Introduction
- 6.2 Adhesive system and process selection
- 6.3 Thermal and residual stress problems
- 6.4 Design correlations and materials allowables
- 6.5 A preliminary design approach
- 6.6 Crack propagation behaviour
- 6.7 Applications of crack patching
- 7. Repair of composite aircraft
- 7.1 Introduction
- 7.2 Composite fabrication
- 7.3 Defects
- 7.4 Repair materials
- 7.5 Bonded repair — composite repair concepts
- 7.6 Effect of moisture on bonded repairs of composites
- 7.7 Design of bonded repairs
- 7.8 Composite service damage experience
- 7.9 Specific component repair
- 7.10 Future requirements.