Patent · US Active

Method for manufacturing an aircraft seat part

US12128602B2 · kind B2 · utility

0Cited by
0References
14Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJul 20, 2022
Grant dateOct 29, 2024
Priority date
Expiry dateJul 20, 2042

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64D11/0638
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A method for manufacturing a part for an aircraft seat includes positioning a heating frame around a stacked structure, locally heating an edge of the stacked structure using a heating frame, externally heating the entire stacked structure, positioning the stacked structure inside a thermoforming mould provided with cutting punches, closing the thermoforming mould and applying a vacuum to the interior of the thermoforming mould, to simultaneously perform, during the same step of shaping the first cover and the second cover, a step of heat sealing an edge of the first cover to an edge of the second cover, bonding the first cover and the second cover to the foam core, and cutting the stacked structure along the circumference thereof using cutting punches.

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