Patent · US Active

Noise-reducing aircraft landing gear tow bar fitting

US11530051B2 · kind B2 · utility

0Cited by
2References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJun 4, 2020
Grant dateDec 20, 2022
Priority date
Expiry dateFeb 17, 2041

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C2025/003
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A tow bar fitting for towing an aircraft is disclosed. The tow bar fitting includes a mount, a pin support, and a tow pin. The mount includes an upper attachment and a lower attachment for affixing the tow bar fitting to a landing gear of the aircraft. The pin support extends from the mount away from the landing gear. The tow pin is positioned in the pin support such that a tow pin plane that horizontally bisects the tow pin is lower than a mount plane that horizontally bisects the upper attachment and the lower attachment when the aircraft is right-side-up on the ground.

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