Hollow structural rod and production method thereof
AssigneesAirbus France, Protac
InventorsVirginie Audart-Noel, Marc Canadas, Alain Grelier, Daniel Audri
Life of this patent
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AssigneesAirbus France, Protac
InventorsVirginie Audart-Noel, Marc Canadas, Alain Grelier, Daniel Audri
Estimating the term…
The invention relates to a hollow structural connecting rod (1) including a first end fitting (8a), a second end fitting (8b), as well as a hollow main portion (10) situated between the two end fittings. According to the invention, it includes first and second connecting rod elements (2a, 2b) integrally joined to one another and having, respectively, a first hollow shank (6a) made in one piece together with the first end fitting as well as a second hollow shank (6b) made in one piece with the second end fitting, the first and second connecting rod elements being joined by means of a joint (4) situated at mid-length on said connecting rod, and preferably being produced via flow-turning. Particular application to an assembly system intended to be interposed between an aircraft engine mounting structure and an engine.
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