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.
Aircraft lubrication system
2020-10-27
Patent
Electronic Resource
English
Engineering Index Backfile | 1951
|Engineering Index Backfile | 1951
|AIRCRAFT GEARBOX LUBRICATION SYSTEM WITH MULTIPLE LUBRICATION SUBSYSTEMS
European Patent Office | 2020
|