Patent · US Active

Adhesively joining airframe members at solid insert

US10450054B2 · kind B2 · utility

1Cited by
6References
21Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMay 22, 2017
Grant dateOct 22, 2019
Priority date
Expiry dateApr 12, 2038

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB32B2605/18
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

An airframe assembly for an aircraft. The airframe assembly includes a first airframe member having a first skin, a second skin, a large cell core joined between the first and second skins and a solid insert having a side surface. The solid insert is joined between the first and second skins such that at least a portion of the side surface is adjacent to the large cell core. The first skin has a first surface disposed opposite the solid insert. The airframe assembly also includes a second airframe member having a second surface. An adhesive joint is disposed between the first and second surfaces structurally bonding the first airframe member to the second airframe member such that the second airframe member is positioned opposite the solid insert.

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