Patent · US Active

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

US10343780B2 · kind B2 · utility

6Cited by
20References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 16, 2015
Grant dateJul 9, 2019
Priority date
Expiry dateNov 5, 2035

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

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.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.