Aircraft Sustainment and Repair

Description

Aircraft Sustainment and Repair is a one-stop-shop for practitioners and researchers in the field of aircraft sustainment, adhesively bonded aircraft joints, bonded composites repairs, and the application of cold spray to military and civil aircraft. Outlining the state-of-the-art in aircraft sustainment, this book covers the use of quantitative fractography to determine the in-service crack length versus flight hours curve, the effect of intergranular cracking on structural integrity and the structural significance of corrosion. The book additionally illustrates the potential of composite repairs and SPD applications to metallic airframes.

Key Features

• Covers corrosion damage assessment and management in aircraft structures
• Includes a key chapter on U.S. developments in the emerging field of supersonic particle deposition (SPD)
• Shows how to design and assess the potential benefits of both bonded composite repairs and SPD repairs to metallic aircraft structures to meet the damage tolerance requirements inherent in FAA ac 20-107b and the U.S. Joint Services

Readership

Materials and aerospace scientists and engineers; practitioners in airworthiness, fatigue and fracture, adhesive bonding, maintenance and aircraft certification, fleet management; Researchers in the fields of cold spray, surface treatments and structural integrity

Table of Contents

1. Introduction and overview
2. Fatigue requirements for aircraft structures
3. Typical fatigue-initiating discontinuities in metallic aircraft structures
4. Practical computational fracture mechanics for aircraft structural integrity
5. Crack growth from naturally occurring material discontinuities
6. Adhesively bonded repair/reinforcement of metallic airframe components: materials, processes, design and proposed through-life management
7. Surface treatment and repair bonding
8. Analysis, design and assessment of composite repairs to operational aircraft
9. Repair of multi-site damage in civil transport aircraft – an example of the damage tolerant design of composite repairs
10. The F111C wing pivot fitting repair and implications for the design/assessment of bonded joints and composite repairs
11. Development and validation of bonded composite double repairs for commercial aircraft
12. Computing the growth of naturally-occurring disbonds in adhesively-bonded joints
13. Delamination growth in polymer-matrix fibre composites and the use of fracture mechanics data for material characterisation and life prediction
14. Introduction to supersonic particle deposition
15. Additive metal technologies for aerospace sustainment
16. Applications of SPD to enhance the structural integrity of corroded airframes
17. Application of SPD to enhance the structural integrity of fuseage skins and centre barells
18. Multiplicative manufacturing and aircraft sustainment