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Damage and Repair of Aerospace Composite Materials / Y. Charles Lu.
- Format:
- Book
- Author/Creator:
- Lu, Y. Charles, author.
- Language:
- English
- Subjects (All):
- Composite materials.
- Physical Description:
- 1 online resource (146 pages)
- Edition:
- 1st ed.
- Place of Publication:
- Warrendale, Pennsylvania, USA : SAE International, 2019.
- Summary:
- Reports the latest developments on the detection and repair of composite structures from the perspective of ten SAE technical papers. This micro-collection of papers offers an overview of composite utilization on large-scale commercial aircraft as well as an outline of general damage inspection and repair of composite structures.
- Contents:
- Cover
- OVERALL COMPOSITE USAGE
- CHAPTER 1 Composite Structure Utilization-Commercial Airplanes
- Introduction
- Airplane Structure
- Honeycomb Structure
- Core Materials
- Foam Core
- Fluted Core
- Syntactic Core
- Nomex Core
- New Generation Aramid Core
- Carbon/Carbon Core
- Laminate Materials
- A-Stage Materials
- Carbon Fiber Reinforcement
- Kevlar Fiber Reinforcement
- Glass Fiber Reinforcement
- B Stage Materials
- Carbon/Epoxy Prepreg
- Kevlar/Epoxy Prepreg
- Fiberglass/Epoxy Prepreg
- Adhesives
- Laminate Structure
- Design Considerations
- Manufacturing Considerations
- Maintenance Considerations
- In-Service Inspection
- In-service Repairs
- Nondestructive Inspection of Composite Structure
- Tap Testing
- Automated Tap Test Devices
- Ultrasonics
- Generation of Two and Three Dimensional Images to Produce Wide Area Inspection Methods
- A-Scan Mode
- Wide Area Inspections Aided by C-Scan Mode
- Mechanics of C-Scan System
- Low Frequency Bond Testing
- Mechanical Impedance Analysis
- Thermography
- Conclusion
- Contact Information
- References
- DAMAGE DETECTION OF COMPOSITE STRUCTURES
- CHAPTER 2 Porosity Assessment in Large Composite Components: Realization and Challenges
- Typical Defects in Composite Structures
- Ultrasonic Inspection Techniques
- Semi-Automated Inspection System
- Automated Inspection System
- Defects Signature - Pulse Echo
- Defects Signature - Through Transmission
- Porosity Assessment - Pulse Echo
- Porosity Curves Development
- Void Content Assessment
- Thickness Dependency
- Averaging
- Frequency Dependency
- Morphology Dependency
- Laminar Indications Area
- Pulse Echo Porosity Assessment Limitation
- Attenuation vs Void Content: Porosity Curves
- Transfer Values
- Arithmetic for Transfer Value.
- Transfer Value - Material Composition
- Transfer Value - Surface Coating
- Transfer Value - Interface
- Porosity Assessment - Through Transmission
- Porosity Assessment - Through Transmission Results
- Summary/Conclusions
- CHAPTER 3 Detecting Damage and Damage Location on Large Composite Parts Using RFID Technology
- Presentation of the Solution
- Acoustic Ultrasonic
- Technology/Application Discriminators
- Technology Inhibitors
- Accelerometers
- 3. Radio Frequency (RF) Sensors (Shock Vibration)
- Technology Tests
- Sensor Positioning/Location
- Radio Frequency (RF) Sensors (Shock Vibration)
- Test Results
- Conclusions and Recommendations
- Acknowledgements
- CHAPTER 4 Discrimination between Damaging and Non-Damaging Impact Events on Composite Structure using SHM Sensor Signal Analysis
- Experimental Approach
- Experimental Results
- Impact Damage Classification Based on Sensor Signal Characterisitcs
- Acknowledgments
- CHAPTER 5 AFP Automated Inspection System Performance and Expectations
- Inspection Process Overview
- Ply Boundary Inspection
- Overlap/Gap Inspection
- Inspection User Interface
- Inspected Part Model
- Overlap/Gap Interface
- Fully-Automatic
- Semi-Automatic
- Pointing to Defects
- Inspection Time
- Ply Boundary
- Overlap and Gap
- Inspection Data
- Accuracy
- Ply Report
- Data Volume
- Data Value and Utility
- Resource Burden
- Hardware Cost
- Summary/Conclusions.
- Contact Information
- Definitions/Abbreviations
- DAMAGE REPAIR OF COMPOSITE STRUCTURES
- CHAPTER 6 Design and Evaluation of Novel Composite Aircraft Repairs
- Typical Metallic Doubler Installation
- Typical Composite Doubler Installation
- Assessment of DC-10 Composite Doubler Design
- Fatigue Tests: Flawed Specimens
- Fatigue Tests: Baseline (Unflawed) Specimens
- Effects of Impact
- Finite Element Analysis
- Damage Tolerance
- Repair Design Validation
- Nondestructive Inspection (NDI)
- Pitch/Catch Impulse Testing
- Pilot Program
- CHAPTER 7 Design and Analysis of Aeronautical Repair: Fastened × Bonded
- Finite Element Model
- Damaged Plate
- Bonded Repair
- Computational Toll (SAJ)
- Fastened Repair
- Results
- Summary and Conclusions
- CHAPTER 8 Economical Repair of Damaged and Discrepant Holes in Metals and Composites
- Expanded Bushing Methods
- Composite or Composite/Metal Joint Repair
- Panel Repair
- Summary
- CHAPTER 9 New Cutting Tools for Repairs of Composites
- 1. Introduction
- 1.1 Milling Thin CFRP Layers
- 1.2 Scarfing of CFRP: The Right Strategy
- 1.3 The Right Tools Scarfing CFRP
- 2. Experimental Testing and Results
- 3. Conclusions
- CHAPTER 10 End-Effector for Automatic Shimming of Composites
- Description of Concept
- Shimming End-Effector
- Extrusion Head
- Hot-End
- Bed Heating System
- Control System
- Validation of the Concept: Results
- Conclusions
- References.
- Notes:
- Includes bibliographical references and index.
- ISBN:
- 9781523140336
- 152314033X
- 9780768001181
- 0768001188
- 9780768001129
- 0768001129
- OCLC:
- 1302007075
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