Triple circuit lubrication device with increased reliability for a main power transmission gearbox of an aircraft

• US 9,829,088 B2
• Filed: 10/28/2015
• Issued: 11/28/2017
• Est. Priority Date: 10/31/2014
• Status: Active Grant

• Current Assignee: Airbus Helicopters
• Original Assignee: Airbus Helicopters
• Inventors: Goujet, Damien
• Primary Examiner(s): Riegelman, Michael
• Application Number:
  US14/924,776
• Publication Number:
  US 20160123456A1
• Time in Patent Office: 762 Days
• CPC Class Codes: B64C 27/12 Rotor drives
• CPC Class Codes: B64C 27/14 Direct drive between power plant and rotor hub
• CPC Class Codes: F01M 2011/0075 with a plurality of tubes
• CPC Class Codes: F16H 57/0405 Monitoring quality of lubricant or hydraulic fluids
• CPC Class Codes: F16H 57/0417 Heat exchangers adapted or integrated in the gearing
• CPC Class Codes: F16H 57/0435 Pressure control for supplying lubricant; Circuits or valves therefor
• CPC Class Codes: F16H 57/0436 Pumps
• CPC Class Codes: F16H 57/0438 Pumps of jet type, e.g. jet pumps with means to inject high pressure fluid to the suction area thereby supercharging the pump or means reducing cavitations
• CPC Class Codes: F16H 57/0441 Arrangements of pumps
• CPC Class Codes: F16H 57/0452 Oil pans
• CPC Class Codes: F16H 57/0456 Lubrication by injection; Injection nozzles or tubes therefor oil mist or spray lubrication F16H57/0458
• CPC Class Codes: F16H 57/046 Oil-mist or spray lubrication

Abstract

A triple circuit lubrication device for lubricating a mechanical system, the lubrication device being provided with two independent lubrication circuits, a tank common to both lubrication circuits and containing a lubrication liquid, and a tertiary circuit in which a tertiary liquid flows. Each lubrication circuit comprises pipes, and respective pressure sensors, pumps, heat exchangers, spray nozzles, and suction points for sucking up the lubrication liquid situated in the tank. The second suction point is situated below the high first suction point. The tertiary circuit comprises a third pump, a third pressure sensor, the second heat exchanger, and a third heat exchanger, thus serving to cool the lubrication liquid flowing through the second lubrication circuit.

Claims

1. A triple circuit lubrication device for lubricating a mechanical system, the lubrication device being provided with a tank and two lubrication circuits, the tank containing a lubrication liquid, a first lubrication circuit comprising a first pump, first pipes, a first pressure sensor, a first heat exchanger, first spray nozzles, and a first suction point for sucking up the lubrication liquid, a second lubrication circuit comprising a second pump, second pipes, a second pressure sensor, a second heat exchanger, second spray nozzles, and a second suction point for sucking up the lubrication liquid, the first and second suction points being situated in the tank, each pump acting via the first and second suction points to deliver the lubrication liquid into the first and second pipes respectively, and then into the first and second spray nozzles in order to lubricate the mechanical system, wherein the triple circuit lubrication device includes a tertiary circuit in which a tertiary liquid flows, the tertiary circuit comprising a third pump, third pipes, a third pressure sensor, the second heat exchanger, and a third heat exchanger, the third pump serving to cause the tertiary liquid to flow through the second heat exchanger and through the third heat exchanger, the second suction point being situated below the first suction point.

2. A lubrication device according to claim 1, wherein the tertiary circuit is a closed circuit.

3. A lubrication device according to claim 1, wherein the tertiary circuit includes a tertiary tank and a third suction point, the third suction point being situated in the tertiary tank, the third pump acting via the third suction point to deliver the tertiary liquid into the third pipes and the second and third heat exchangers.

4. A lubrication device according to claim 1, wherein the lubrication liquid flows in the second lubrication circuit at a second pressure P2, the tertiary liquid flows in the tertiary circuit at a third pressure P3, and the second pressure P2 of the lubrication liquid is strictly greater than the third pressure P3 of the tertiary liquid.

5. A lubrication device according to claim 1, wherein the lubrication liquid flows in the second lubrication circuit at a second pressure P2, the tertiary liquid flows in the tertiary circuit at a third pressure P3, and the second pressure P2 of the lubrication liquid is strictly less than the third pressure P3 of the tertiary liquid.

6. A lubrication device according to claim 1, wherein the second heat exchanger is suitable for being situated inside the mechanical system.

7. A lubrication device according to claim 1, wherein the second heat exchanger is suitable for being situated above the tank.

8. A lubrication device according to claim 1, wherein the second heat exchanger is suitable for being situated against a wall of the tank.

9. A lubrication device according to claim 1, wherein the tertiary circuit includes a tertiary valve and third spray nozzles.

10. A lubrication device according to claim 1, wherein the mechanical system is a main power transmission gearbox of a rotary wing aircraft.

11. A main power transmission gearbox for a rotary wing aircraft, wherein the main power transmission gearbox is provided with a lubrication device according to claim 10, the tank being constituted by a casing of the main power transmission gearbox.