Patent · US Active

Composite assembly for unhardened fuselage components

US11597044B2 · kind B2 · utility

0Cited by
1References
30Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 10, 2021
Grant dateMar 7, 2023
Priority date
Expiry dateNov 10, 2041

Classification

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

Abstract

Systems and methods are provided for fabricating a preform for a fuselage section of an aircraft. The method includes advancing a series of arcuate mandrel sections in a process direction through an assembly line, laying up fiber reinforced material onto the arcuate mandrel sections via layup stations, uniting the series of arcuate mandrel sections into a combined mandrel; and splicing the fiber reinforced material laid-up onto the arcuate mandrel sections.

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