Method for producing an especially large aeronautical part

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United States of America Patent

PATENT NO 10737343
APP PUB NO 20170203378A1
SERIAL NO

15468138

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Abstract

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The present disclosure relates to a method for producing a final metal part for a nacelle of a turbojet. The method includes brazing at least two parts, one being an inner part having an inner surface and the other being an outer part having an outer surface. The method further includes a step of heating the outer surface of the outer part using an external heating means, and a step of heating the inner surface of the inner part using an internal heating means.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN NACELLESROUTE DU PONT VII GONFREVILLE-L'ORCHER 76700

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bienvenu, Philippe Gonfreville l'Orcher, FR 28 97
Julienne, Charlotte Gonfreville l'Orcher, FR 1 0
Malot, Helene Gonfreville l'Orcher, FR 4 37

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