Patent · US Active

Aircraft refuelling device and method for manufacturing a wing coupling for such a device

US11845565B2 · kind B2 · utility

0Cited by
3References
11Claims
0Family size

Assignee

Inventor

Key dates

Filing dateMar 5, 2019
Grant dateDec 19, 2023
Priority date
Expiry dateDec 8, 2040

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64F5/10
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

Aircraft refuelling device including a fuel circulation pipe of which the downstream end is equipped with a wing coupling for connecting it to an inlet orifice of a fuel tank of the aircraft. The wing coupling includes a body which defines a fuel circulation duct at the end of the pipe, a sensor for measuring the value of a parameter indicative of a flow of fuel passing through the wing coupling, and at least one battery electrically powering the sensor. The sensor and the electrical power supply battery are housed in two half-shells mounted together around the body of the wing coupling.

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