Tube having a hybrid-type structure, in particular for an aircraft seat

A hybrid tube, in particular for an aircraft seat structure includes ribs intended to receive the hybrid tube. The hybrid tube includes a monolithic carbon tube and at least one sleeve made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-molding.

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Bibliographic Details
Main Authors Portoles, Jose, Landais, Matthieu, Nogues, Dominique
Format Patent
LanguageEnglish
Published 09.07.2019
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
BEDS
CHAIRS
COFFEE MILLS
COSMONAUTICS
DOMESTIC ARTICLES OR APPLIANCES
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
FURNITURE
HUMAN NECESSITIES
PARACHUTES
PERFORMING OPERATIONS
SOFAS
SPICE MILLS
SUCTION CLEANERS IN GENERAL
TRANSPORTING
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Summary:A hybrid tube, in particular for an aircraft seat structure includes ribs intended to receive the hybrid tube. The hybrid tube includes a monolithic carbon tube and at least one sleeve made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-molding.
Bibliography:Application Number: US201515500960