Patent · US Active

Structural component, method for producing a structural component, pressure fuselage for a vehicle comprising a structural component

US10549488B2 · kind B2 · utility

1Cited by
7References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 9, 2017
Grant dateFeb 4, 2020
Priority date
Expiry dateApr 21, 2038

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/40
  • WIPO fieldSurface technology, coating
  • WIPO sectorChemistry

Abstract

A structural component has a main body formed of a fibre composite material, a plurality of first reinforcement parts and a plurality of second reinforcement parts, wherein the main body is formed as a domed body having a peripheral edge and a vertex, wherein the first reinforcement parts are connected to the main body and in each case have a concave curvature course in relation to a first plane, and wherein the second reinforcement parts are connected to the main body and also have a concave curvature course in each case in relation to a second plane.

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