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Benefits of the Complementary use of Archaeometry Investigations and Historical Research in the Study of Ancient Airplanes: the Breguet Sahara’s Rivets

Published online by Cambridge University Press:  22 August 2014

Audrey Cochard
Affiliation:
CEMES, CNRS, Université de Toulouse, 29 rue J. Marvig, 31055 Toulouse, France.
Joël Douin
Affiliation:
CEMES, CNRS, Université de Toulouse, 29 rue J. Marvig, 31055 Toulouse, France.
Bénédicte Warot-Fonrose
Affiliation:
CEMES, CNRS, Université de Toulouse, 29 rue J. Marvig, 31055 Toulouse, France.
Julitte Huez
Affiliation:
CIRIMAT-ENSIACET-INPT, 4 allée Emile Monso, BP 44362 Toulouse Cedex 4, France.
Luc Robbiola
Affiliation:
TRACES-UTM, 5 allées Antonio Machado, 31058 Toulouse Cedex 9, France.
Jean-Marc Olivier
Affiliation:
FRAMESPA-UTM, 5 allées Antonio Machado, 31058 Toulouse Cedex 9, France.
Philippe Sciau
Affiliation:
CEMES, CNRS, Université de Toulouse, 29 rue J. Marvig, 31055 Toulouse, France.
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Abstract

The aim of this paper is to show that historical technical archives and complementary physico-chemical studies can be combined to obtain relevant information on the materials and processes used in the manufacturing of a Breguet 765 Sahara airplane. This will be useful both in history of sciences and technology and in the renovation of this more than fifty years old airplane.

The Breguet 765 Sahara plane is the last version of a family of French double-deck transport aircraft produced by Breguet between 1948 and 1960. The gathering of multi-disciplinary information from the literature of the period of production with laboratory investigations has revealed that a “new” aluminum-copper-magnesium alloy was used in the rivets of the Breguet 765. The A-U3G alloy was developed to meet properties requirements of the aeronautical industry for joining sheets of aluminum and was used in the Breguet 765 Sahara to strengthen the joints. Analytical techniques included TEM, EPMA microprobe and metallography.

Type
Articles
Copyright
Copyright © Materials Research Society 2014 

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References

REFERENCES

Dollfus, C., Les divers domaines d’applications : L’Aviation, Revue de l’Aluminium, 211 (1954) pp. 201209.Google Scholar
Breguet, E., Breguet, un siècle d’aviation, édition Privat, pp. 9197, (coll. Aviation, Toulouse, 2012).Google Scholar
Hartmann, D., Sauver Brigitte ou le sauvetage et la récupération du Breguet 765 « SAHARA » d’Évreux à Toulouse, pp.37-39 , (http://www.calameo.com/subscriptions/57493).Google Scholar
Service Technique de l’Aéronautique, Clauses techniques du Breguet 765, édition 2bis (1956).Google Scholar
Hardouin Duparc Olivier, Alfred Wilm et les débuts de Duralumin, Cahiers d’histoire de l’aluminium 64, (Institut pour l’Histoire de l’Aluminium, Paris, 2005) p.62.Google Scholar
Saulnier, A., Le durcissement structural des alliages aluminium-cuivre 4%, Revue de l’Aluminium 217, pp.4146 (1955).Google Scholar
Dubost, B., Saintfort, P., Durcissement par précipitation des alliages d’aluminium, Dossier Techniques de l’ingénieur M240, pp.24 (1991).Google Scholar
Penel, P., Le rivetage- première et deuxième partie, Encyclopédie du travail de l’Aluminium fiche G81, pp.11251127 (1958).Google Scholar
Tournaire, M., Renouard, M., Alliages pour rivets de la famille du Duralumin, Revue de l’Aluminium 217 (1955).Google Scholar
American Society for Metals Handbook committee, Metals Handbook vol. 8: Metallography, Structures and Phase Diagrams. Edited by American Society for Metals, p.124, (Metals Park, Ohio, 1973)Google Scholar