Patent · US Active

Method for producing a frame component for a door frame structure of an aircraft, frame component, and door frame structure

US11548659B2 · kind B2 · utility

1Cited by
3References
15Claims
0Family size

Assignee

Inventors

Key dates

Filing dateNov 20, 2018
Grant dateJan 10, 2023
Priority date
Expiry dateAug 5, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB29L2031/724
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A method for producing a frame component for a door frame structure of an aircraft. A connecting zone is generated on a first and a second assembly surface of a connecting component in each case by generating a surface texture on the assembly surfaces, wherein the connecting component is formed from a metal material. The assembly surfaces of the connecting component are placed against a door frame member and against an attachment member, wherein the door frame member and the attachment member are each formed from a fiber-reinforced thermoplastics material. Furthermore, the connecting component and the door frame member are welded, and the connecting component and the attachment member are welded. A frame component and a door frame structure are also described.

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