Patent · US Active

Method for manufacturing at least one portion of a box structure of an aircraft comprising a forming step, and a central wingbox thus obtained

US12269576B2 · kind B2 · utility

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0References
14Claims
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Key dates

Filing dateFeb 3, 2023
Grant dateApr 8, 2025
Priority date
Expiry dateOct 20, 2043

Classification

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

Abstract

A method for manufacturing at least a portion of a box structure obtained from an outer skin and a plurality of sections each having a joining face in contact with the outer skin. The method comprises a step of positioning the sections on a mold, a step of obtaining a flat fiber preform having a thickness substantially equal to the outer skin, a step of placing a central portion of the fiber preform on the sections positioned on a first face of the mold and a step of forming a lateral extension of the fiber preform to press the fiber preform against a forming surface. A central wingbox obtained by the method is provided and a forming tool for carrying out the method.

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