IP Library › Granted Patent US 12,442,446
Granted Patent B2
US 12,442,446 · App. 17/476,730 · Granted Oct 14, 2025

Lubrication system with a reserve tank

Inventors: Laurent Zamponi (Vitrolles, FR); Jerome Belmonte (Aix en Provence, FR); Eric Fabrigat (Velaux, FR)
Assignee: AIRBUS HELICOPTERS
F16H57/0442F16H57/0404F16H57/0435F16H57/0443F16H57/0449F16H57/045F16H57/046B64C27/12F01M2011/0095
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Quick Facts
Patent No.
US 12,442,446
App. No.
17/476,730
Granted
Oct 14, 2025
Kind
B2
Abstract

A lubrication system for a mechanical system, the lubrication system comprising a main tank, a reserve tank and a main lubrication circuit. The main lubrication circuit comprises, in particular, a pump drawing in the lubricating liquid from the main tank via a main suction point and a main suction pipe connecting the main suction point to the pump. The reserve tank is supplied with lubricating liquid either directly from the main tank or via the main lubrication circuit. The reserve tank is connected to the main suction pipe via an outlet pipe and the reserve tank is located above the main suction point so that the lubricating liquid flows through the outlet pipe to the main suction pipe by gravity.

Claims (36)

1. A lubrication system for a mechanical system, the lubrication system comprising:

a main tank containing a lubricating liquid;

a main lubrication circuit comprising a main flow generator as well as devices for spraying the lubricating liquid, the main lubrication circuit comprising a main suction point for drawing in the lubricating liquid located in the main tank, a main suction pipe connecting the main suction point to the main flow generator;

a reserve tank comprising an inlet for receiving a portion of the lubricating liquid from the main tank, wherein the reserve tank is arranged in an environment where an outside pressure is prevailing outside the reserve tank;

an outlet pipe directly connecting the reserve tank to the main suction pipe, wherein the lubricating liquid communicates through the outlet pipe between the reserve tank and the main suction pipe by gravity;

a vent port disposed on the reserve tank, wherein opening the vent port vents the reserve tank to the outside pressure outside of the reserve tank and so that the lubricating liquid can flow through the outlet pipe by gravity, the open vent port acting as an overflow, balancing flows of lubricating liquid entering and exiting the reserve tank; and

at least one spill-proof wall positioned within the reserve tank adjacent to the vent port and the spill-proof wall extends from a side wall upward between the inlet and the vent port to prevent the lubricating liquid from exiting the vent port when the system is tilted.

2. The lubrication system according to claim 1 ,

wherein the outlet pipe is configured so that the lubricating liquid flows through the outlet pipe at an outlet flow rate that is less than a main flow rate of the lubricating liquid flowing in the main lubrication circuit.

3. The lubrication system according to claim 1 , wherein the lubrication system includes an outlet flow rate reducer arranged between the reserve tank and the main suction pipe.

4. The lubrication system according to claim 1 , wherein the lubrication system comprises a supply pipe for supplying the reserve tank with lubricating liquid from the main lubrication circuit, the supply pipe connecting the inlet of the reserve tank to the main lubrication circuit downstream of the main flow generator.

5. The lubrication system according to claim 4 , wherein the lubrication system comprises a filter arranged between the inlet of the reserve tank and the main lubrication circuit.

6. The lubrication system according to claim 4 , wherein the supply pipe of the reserve tank is configured so that the lubricating liquid circulates in the supply pipe at a supply flow rate that is less than a main flow rate of the lubricating liquid circulating in the main lubrication circuit.

7. The lubrication system according to claim 6 , wherein the lubrication system includes a supply flow rate reducer arranged between the main lubrication circuit and the inlet of the reserve tank or at the inlet or indeed at one end of the supply pipe.

8. The lubrication system according to claim 1 , wherein the reserve tank is located in the main tank and is arranged at least partially below the level of the lubricating liquid in the main tank.

9. The lubrication system according to claim 1 , wherein the lubrication system comprises a filter.

10. The lubrication system according to claim 1 , wherein the vent port is positioned along the side wall.

11. The lubrication system according to claim 1 , wherein the lubrication system comprises at least one secondary lubrication circuit.

12. The lubrication system according to claim 1 , wherein the lubrication system includes a level indicator arranged in the reserve tank and configured to emit an image signal of an item of information relating to an amount of lubricating liquid present in the reserve tank.

13. A mechanical system,

wherein the mechanical system is provided with the lubrication system according to claim 1 , the main tank of the lubrication system being constituted by a casing of the mechanical system.

14. The mechanical system according to claim 13 ,

wherein the mechanical system is a main gearbox of a rotary-wing aircraft.

15. A rotary-wing aircraft provided with at least one main gearbox

wherein the main gearbox is provided with the lubrication system according to claim 1 , the main tank of the lubrication system being constituted by a casing of the main gearbox.

16. A lubrication system for a mechanical system, the lubrication system comprising:

a main tank containing a lubricating liquid;

a reserve tank having an inlet for receiving a portion of the lubricating liquid from the main tank;

a main lubrication circuit having a main suction pipe in fluid communication with the main tank, the main lubrication circuit circulating the lubricating liquid to devices for applying the lubricating liquid;

an outlet pipe directly connecting the reserve tank to the main suction pipe, wherein the lubricating liquid communicates through the outlet pipe between the reserve tank and the main suction pipe by gravity;

a vent port disposed on the reserve tank, wherein opening the vent port vents the reserve tank to an outside pressure outside of the reserve tank so the lubricating liquid can flow through the outlet pipe by gravity, the vent port being open and acting as an overflow, balancing flows of lubricating liquid entering and exiting the reserve tank; and

at least one spill-proof wall extending from a side wall upward between the inlet and the vent port within the reserve tank to prevent the lubricating liquid from exiting the reserve tank through the vent port when the system is tilted.

17. The lubrication system according to claim 16 , wherein the outlet pipe is configured so that the lubricating liquid flows through the outlet pipe at an outlet flow rate that is less than a main flow rate of the lubricating liquid flowing in the main lubrication circuit.

18. The lubrication system according to claim 16 , wherein the lubrication system includes an outlet flow rate reducer arranged between the reserve tank and the main suction pipe.

19. The lubrication system according to claim 16 , wherein a supply pipe of the reserve tank is configured so that the lubricating liquid circulates in the supply pipe at a supply flow rate that is less than a main flow rate of the lubricating liquid circulating in the main lubrication circuit.

20. The lubrication system according to claim 16 , wherein the at least one spill-proof wall extends adjacent the vent port.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 6, 2021
From: ZAMPONI, LAURENT; BELMONTE, JEROME; FABRIGAT, ERIC
To: AIRBUS HELICOPTERS
Reel/Frame 058040/0764 →
Priority Claims (1)
FR 2010022 · Oct 1, 2020 · national
Continuity (1)
Related Publication 20220107018A1 · Apr 7, 2022
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