Patent · US Active

Structural component and method for producing a structural component

US9988136B2 · kind B2 · utility

109Cited by
9References
16Claims
0Family size

Assignee

Inventors

Key dates

Filing dateOct 29, 2015
Grant dateJun 5, 2018
Priority date
Expiry dateJan 22, 2036

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02P10/25
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A structural component for reinforcing the fuselage of an aircraft or spacecraft is integrally formed and segmented into surface-like stiffening sections, whereby at least one stiffening section is formed as a rigid mesh section, and at least one stiffening section is formed as a solid section.

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