Granted Patent B2

US 12,326,115 · App. 18/972,172 · Granted Jun 10, 2025

Inventors: Bugra H. Ertas (Niskayuna, NY); Xiaohua Zhang (Glenville, NY); Miriam Manzoni (Rivalta di Torino, IT); Flavia Turi (Bari, IT); Andrea Piazza (Turin, IT); Arthur W. Sibbach (Boxford, MA); Brandon W. Miller (Middletown, OH)

Assignees: GENERAL ELECTRIC COMPANY; GE AVIO S.R.L.

F02C7/06F16H57/0434F16N7/38F05D2260/98F16N2210/02F16N2250/40

Abstract

Claims (49)

1. A gas turbine engine comprising:

a gearbox assembly comprising:

a gearbox having a gearbox volume defined by an outer diameter of the gearbox and a gearbox length of the gearbox; and

a gutter for collecting a gearbox lubricant scavenge flow from the gearbox, the gutter having a gutter volume defined by an inner surface of a gutter wall of the gutter and being characterized by a lubricant extraction volume ratio between 0.01 and 0.3, inclusive of the endpoints, the lubricant extraction volume ratio defined by:

V

G

V

G

⁢

B

,

wherein V G is the gutter volume of the gutter and V GB is the gearbox volume; and

a lubricant flow control system comprising:

a variable flow lubricant pump that generates a pump variable flow of lubricant to the gearbox assembly during operation of the gas turbine engine, the gearbox assembly having a variable consumption demand for delivery of lubricant; and

a lubricant flow controller configured to generate a pump control command for the variable flow lubricant pump to produce the pump variable flow of lubricant based on the variable consumption demand of the gearbox assembly.

2. The gas turbine engine of claim 1 , wherein the lubricant flow control system includes a lubricant tank in fluid communication with the variable flow lubricant pump and a heat exchanger in fluid communication with the variable flow lubricant pump.

3. The gas turbine engine of claim 2 , wherein the heat exchanger is in downstream fluid communication with the variable flow lubricant pump and upstream fluid communication with the gearbox assembly.

4. The gas turbine engine of claim 1 , wherein the lubricant flow control system includes a lubricant flow control valve in fluid communication with the variable flow lubricant pump, the lubricant flow control valve configured to change the pump variable flow of lubricant to a valve variable flow of lubricant through operation of the lubricant flow control valve, and the gearbox assembly is configured to receive the valve variable flow of lubricant.

5. The gas turbine engine of claim 4 , wherein the lubricant flow controller is configured to generate a valve command for the lubricant flow control valve based on the variable consumption demand of the gearbox assembly.

6. The gas turbine engine of claim 5 , wherein the lubricant flow control system includes a flow rate sensor in fluid communication with the gearbox assembly, the flow rate sensor configured to generate flow rate data indicative of the valve variable flow of lubricant to the gearbox assembly.

7. The gas turbine engine of claim 1 , wherein the lubricant flow control system includes a plurality of lubricant consumers including the gearbox assembly.

8. The gas turbine engine of claim 7 , wherein each of the plurality of lubricant consumers including a variable consumption demand, and during operation of the plurality of lubricant consumers, the lubricant flow controller determines the pump control command based on an aggregate of the variable consumption demand of the plurality of lubricant consumers.

9. The gas turbine engine of claim 7 , wherein the plurality of lubricant consumers is arranged in a parallel lubricant flow arrangement with each other.

10. The gas turbine engine of claim 7 , wherein the plurality of lubricant consumers includes at least one of an engine bearing, an accessory, or an electrical generator.

11. The gas turbine engine of claim 1 , wherein the lubricant flow control system includes a first flow rate sensor in fluid communication with the gearbox assembly, the first flow rate sensor configured to generate first flow rate data indicative of a rate of lubricant to the gearbox assembly.

12. The gas turbine engine of claim 11 , wherein the lubricant flow controller is configured to generate the pump control command for the variable flow lubricant pump based on the first flow rate data from the first flow rate sensor.

13. The gas turbine engine of claim 11 , wherein the lubricant flow control system includes a second flow rate sensor positioned downstream of the gearbox assembly configured to generate second flow rate data indicative of a rate of lubricant from the gearbox assembly.

14. The gas turbine engine of claim 13 , wherein the lubricant flow controller is configured to generate the pump control command for the variable flow lubricant pump based on the second flow rate data from the second flow rate sensor.

15. A gas turbine engine comprising:

a gearbox assembly comprising:

a gearbox having a gearbox volume defined by an outer diameter of the gearbox and a gearbox length of the gearbox; and

a gutter for collecting a gearbox lubricant scavenge flow from the gearbox, the gutter having a gutter volume defined by an inner surface of a gutter wall of the gutter and being characterized by a lubricant extraction volume ratio between 0.01 and 0.3, inclusive of the endpoints, the lubricant extraction volume ratio defined by:

V

G

V

G

⁢

B

,

wherein V G is the gutter volume of the gutter and V GB is the gearbox volume; and

a lubricant flow control system comprising:

a variable flow lubricant pump that generates a pump variable flow of lubricant during operation of the gas turbine engine;

a lubricant flow control valve in fluid communication with the variable flow lubricant pump, the lubricant flow control valve configured to change the pump variable flow of lubricant to a valve variable flow of lubricant through operation of the lubricant flow control valve, wherein the gearbox assembly is configured to receive the valve variable flow of lubricant, the gearbox assembly having a variable consumption demand for delivery of the lubricant; and

a lubricant flow controller configured to generate a valve control command for the lubricant flow control valve based on the variable consumption demand of the gearbox assembly.

16. The gas turbine engine of claim 15 , wherein the lubricant flow control system includes a flow rate sensor in fluid communication with the gearbox assembly, the flow rate sensor configured to generate flow rate data indicative of the valve variable flow of lubricant to the gearbox assembly.

17. The gas turbine engine of claim 16 , wherein the lubricant flow controller is configured to generate a pump control command for the variable flow lubricant pump to produce the pump variable flow of lubricant based on the flow rate data from the flow rate sensor.

18. The gas turbine engine of claim 17 , wherein the lubricant flow control system includes a plurality of lubricant consumers including the gearbox assembly, each of the plurality of lubricant consumers including a variable consumption demand, and during operation of the plurality of lubricant consumers, the lubricant flow controller determines the pump control command based on an aggregate of the variable consumption demand of the plurality of lubricant consumers.

19. The gas turbine engine of claim 17 , wherein the flow rate sensor is a first flow rate sensor, and the lubricant flow control system includes a second flow rate sensor positioned downstream of the gearbox assembly configured to generate second flow rate data indicative of a rate of lubricant from the gearbox assembly.

20. The gas turbine engine of claim 19 , wherein the lubricant flow controller is configured to generate the pump control command for the variable flow lubricant pump based on the second flow rate data from the second flow rate sensor.

Assignments (1)

Priority Claims (1)

Continuity (2)

References Cited (96)

Cited By (2)

US 12,553,381 US 12,571,468