Patent · US Active

Aircraft lubrication system

US10816085B2 · kind B2 · utility

4Cited by
0References
18Claims
0Family size

Assignee

Inventors

Key dates

Filing dateJan 18, 2018
Grant dateOct 27, 2020
Priority date
Expiry dateDec 10, 2038

Classification

  • Technology area (CPC B)Performing Operations; Transporting
  • CPC primaryB64C29/0091
  • WIPO fieldTransport
  • WIPO sectorMechanical engineering

Abstract

A system is provided in one example embodiment and may include a first reservoir for a lubricant; a second reservoir for the lubricant, wherein the first reservoir and the second reservoir are interconnected; a first pumping element to pump the lubricant from the first reservoir at a first flow rate; a second pumping element to pump the lubricant at a second flow rate, wherein the first flow rate and the second flow rate are different; and a gearbox coupled to the first pumping element and the second pumping element. The first reservoir may have a larger volume than the second reservoir and the first flow rate may be higher than the second flow rate.

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