Device for attaching a lift member to the fuselage of an...

Details Device for attaching a lift member to the fuselage of an... Device for attaching a lift member to the fuselage of an...

B - Operations, Transporting

64

C

B64C 1/26 (2006.01)

Patent

CA 2683596

The invention relates to an aircraft furnished with at least one device for attaching a lift member (9) to the fuselage (8) which comprises elastic articulations (1) whose rigidity in translation and in rotation can be programmed axially (X), vertically (Z) and transversely (Y). In particular the air foil can be connected to the body of the fuselage by means of these elastic articulations.

L'invention concerne un avion muni d'au moins un dispositif de fixation d'un organe de sustentation (9) au fuselage (8) qui comporte des articulations élastiques (1) dont la rigidité en translation et en rotation est paramétrable axialement (X), verticalement (Z) et transversalement (Y). Notamment, on prévoit de relier la voilure au corps du fuselage par l'intermédiaire de ces articulations élastiques.

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