Patent · US Active

Aircraft with composite assembly and a method of manufacture

US12263664B2 · kind B2 · utility

0Cited by
3References
9Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMar 8, 2023
Grant dateApr 1, 2025
Priority date
Expiry dateMar 8, 2043

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2039/105
  • WIPO fieldSurface technology, coating
  • WIPO sectorChemistry

Abstract

A composite assembly for a blended wing body aircraft, the composite assembly comprising: a first assembly comprising a first molded part, wherein the first molded part comprises a first plurality of fibers, the first molded part partially infused with a first resin, a second assembly oriented relative to the first assembly, the second assembly comprising a second molded part wherein the second molded part comprises a second plurality of fibers, the second molded part partially infused with a second resin, and a joining region, the joining region comprising at least a portion of first plurality of fibers and at least a portion of second plurality of fibers, the at least a portion of first plurality of fibers and the at least a portion of second plurality of fibers substantially adjacent and infused with a third resin.

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