Patent · US Active

Metallic fittings for coupling composite ribs to skin panels of aircraft wings

US10913548B2 · kind B2 · utility

1Cited by
1References
26Claims
0Family size

Assignee

Inventor

Key dates

Filing dateJan 14, 2019
Grant dateFeb 9, 2021
Priority date
Expiry dateAug 2, 2039

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF16B37/047
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Metallic fittings for coupling composite ribs to skin panels of aircraft wings are described. An example metallic fitting includes a through hole configured to receive a fastener. The fastener is configured to couple the metallic fitting to a composite rib of an aircraft wing. The example metallic fitting further includes a bore configured to receive a bolt. The example metallic fitting further includes a cavity intersecting the bore. The cavity has an access opening. The example metallic fitting further includes a barrel nut located within the cavity. The barrel nut is configured to threadably engage the bolt to couple the metallic fitting to a skin panel of the aircraft wing. The example metallic fitting further includes a seal located within the cavity. The seal is configured to close the access opening.

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