Ageformable panels for commercial aircraft-Reference-Cited by-同舟云学术

Ageformable panels for commercial aircraft

Published:2008-06-01 Issue:6 Volume:222 Page:873-886
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Eberl F¹,Gardiner S²,Campanile G³,Surdon G⁴,Venmans M⁵,Prangnell P⁶

Affiliation:

1. Alcan Rhenalu, Issoire Cedex, France

2. Airbus UK Ltd, Filton, Bristol, UK

3. ALENIA AERONAUTICA — Engineering, Materials Processes and NDT Technology, Napoli, Italy

4. Dassault Aviation, Advanced Technologies Development Center, Argenteuil, France

5. SABCA, Chaussée de Haecht, Brussels, Belgium

6. UMIST, Manchester Materials Science Centre, Manchester, UK

Abstract

After a quick reminder of the principles of creep form process, a detailed comparison of the 6056, 2022, and 7475 alloys will be presented using experimental techniques for creep relaxation under tension and bending. Microstructural investigations using transmission electronic microscopy and small angle scattering techniques show the evolution of the hardening precipitation during the ageform process of the different alloys investigated. Damage tolerance and static properties of creep-formed products are discussed in detail. The results of an industrial sized demonstrator of an Airbus A340 fuselage panel are presented as a conclusion showing the strong potential of this cost-efficient process.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1243/09544100JAERO290

Reference5 articles.

1. 1 Dieter G. E. Mechanical metallurgy, S.I. Metric edition, 1988, p. 439 (McGraw-Hill, London).

2. 2 Honeycombe R. W. K. The plastic deformation of metals, 2nd edition, 1984, p. 358 (Edward Arnold, London).

3. Microstructural Interactions during Stress Ageing a 7475 Aerospace Alloy

4. Through Thickness Microstructural Gradients in 7475 and 2022 Creep - Ageformed Bend Coupons

5. Understanding and Modelling the Mechanical and Corrosion Properties of 6056 for Aerospace Applications

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