Gas turbine engine dual towershaft accessory gearbox and starter generator assembly

Patent metadata

Field	Value
Publication number	US-10422243-B2
Application number	US-201715410049-A
Country	US
Kind code	B2
Filing date	Jan 19, 2017
Priority date	Jan 19, 2017
Publication date	Sep 24, 2019
Grant date	Sep 24, 2019

Abstract

An exemplary gas turbine engine assembly includes a transmission coupling a starter generator assembly to a first set of gears. The transmission is transitionable between a first mode where the starter generator assembly is driven at a first speed relative to the second towershaft, and a second mode where the starter generator assembly is driven at a different, second speed relative to the second towershaft.

First claim

What is claimed is:

1. A method of operating a gas turbine engine, comprising:
driving a first spool with a starter generator assembly through a first towershaft and a first clutch to start the gas turbine engine;
driving the starter generator assembly through an accessory gearbox through a second clutch with a second towershaft coupled to a second spool once the gas turbine engine is started; and
decoupling the starter generator assembly from the first spool once the first spool reaches an engine idle speed;
driving the starter generator assembly and a hydraulic pump through a transmission in a first mode so that the starter generator assembly and the hydraulic pump are rotated at a first speed relative to the second towershaft, the transmission being driven by a set of gears of the accessory gearbox, the set of gears comprising at least three gears driven by the second towershaft;
transitioning the transmission to a second mode so that the starter generator assembly and the hydraulic pump are rotated at a second speed relative to the second towershaft, wherein the first and second speeds are different from each other;
driving an oil pump with the second towershaft through a gear of the set of gears when the starter generator assembly and the hydraulic pump are driven by the transmission, the oil pump driven at a third speed relative to the second towershaft when the transmission is in the first mode, and the oil pump driven at the third speed relative to the second towershaft when the transmission is in the second mode;
supplying oil from the oil pump to a geared architecture that drives a tan of the gas turbine engine at a lower speed than the second spool;
transitioning the transmission to a third mode;
driving the transmission with the second towershaft through the set of gears to rotate the starter generator assembly and the hydraulic pump at a fourth speed relative to the second towershaft in the third mode; and
wherein the first, second and fourth speeds are different from each other.

2. The method of claim 1 , wherein the decoupling includes rotating the first towershaft at a speed greater than that of the starter generator assembly.

3. The method of claim 1 , further comprising using a shaft of the second spool to drive the geared architecture to drive the fan.

4. The method of claim 1 , wherein the first clutch and the second clutch are one-way mechanical clutch devices.

5. The method of claim 1 , wherein the starter generator assembly comprises a first variable frequency generator and a second variable frequency generator.

6. The method of claim 2 , wherein the first clutch and the second clutch are one-way mechanical clutch devices.

7. The method of claim 6 , wherein the starter generator assembly comprises a first variable frequency generator and a second variable frequency generator.

8. The method of claim 6 , wherein the step of supplying oil from the oil pump to the geared architecture occurs during a windmilling event.

9. A gas turbine engine assembly comprising:
a first spool having a first turbine operatively mounted to a first turbine shaft;
a second spool having a second turbine operatively mounted to a second turbine shaft, the first and second turbines mounted for rotation about a common rotational axis within an engine static structure, the first and second turbine shafts coaxial with one another;
a first towershaft coupled to the first turbine shaft, and a second towershaft coupled to the second turbine shaft;
an accessory drive gearbox with a first set of gears, the first set of gears comprising at least three gears driven by the second towershaft;
a starter generator assembly;
a hydraulic pump;
a first clutch disposed between the first towershaft and the starter generator assembly, the first clutch configured to enable the starter generator assembly to drive the first spool through the accessory drive gearbox;
a second clutch disposed between the second towershaft and the starter generator assembly, the second clutch configured to enable the second spool to drive the starter generator assembly through the accessory drive gearbox;
a transmission coupling the starter generator assembly and the hydraulic Dump to the first set of gears, the transmission driven by the first set of gears and transitionable between a first mode where the starter generator assembly and the hydraulic pump are driven at a first speed relative to the second towershaft in operation, and a second mode where the starter generator assembly and the hydraulic pump area driven at a second speed relative to the second towershaft in operation, and wherein the first and second speeds are different from each other; and
an oil pump driven by a gear of the first set of gears, wherein the starter generator assembly and the hydraulic pump are driven by the second towershaft at a third speed relative to the oil pump when the transmission is in the first mode, and the starter generator assembly and the hydraulic pump are driven by the second towershaft at a fourth speed relative to the oil pump when the transmission is in the second mode, and wherein the third and fourth speeds are different from each other.

10. The gas turbine engine assembly of claim 9 , wherein the first and second turbine shafts are outer and inner shafts, respectively, and the first and second turbines are high and low pressure turbines, respectively.

11. The gas turbine engine assembly of claim 10 , wherein the first towershaft is configured to rotate at a higher speed than the second towershaft.

12. The gas turbine engine assembly of claim 9 , wherein the transmission is further transitionable to a third mode where the starter generator assembly and the hydraulic pump are driven at a fifth speed relative to the second towershaft, and wherein the first, second and fifth speeds are different from each other.

13. The gas turbine engine assembly of claim 12 , wherein the transmission is further transitionable to at least one fourth mode where the starter generator assembly and the hydraulic Dump are driven at a sixth speed relative to the second towershaft, the sixth speed being different than each of the first, second, and fifth speeds.

14. The gas turbine engine assembly of claim 9 , wherein the oil pump is configured to communicate oil to a geared architecture that drives a fan of the gas turbine engine at a lower speed than the second turbine shaft.

15. The gas turbine engine assembly of claim 9 , further comprising a fan driven by a speed reduction device, wherein the speed reduction device is driven by the second turbine shaft.

16. The gas turbine engine assembly of claim 9 , wherein the first clutch and the second clutch are one-way mechanical clutch devices.

17. The gas turbine engine assembly of claim 9 , wherein the starter generator assembly comprises a first variable frequency generator and a second variable frequency generator.

18. The gas turbine engine assembly of claim 9 , wherein the starter generator assembly comprises a first integrated drive generator and a second integrated drive generator.

19. The gas turbine engine assembly of claim 13 , further comprising:
a fan driven by a speed reduction device, wherein the speed reduction device is driven by the second turbine shaft, and the speed reduction device drives the fan at a lower speed than the second turbine shaft;
wherein the first and second turbine shafts are outer and inner shafts, respectively, and the first and second turbines are high and low pressure turbines, respectively, such that the f

Assignees

• United Technologies Corp

Inventors

• Suciu Gabriel L
• Duong Hung
• Zimmitti Jonathan F
• Sheridan William G
• Mccune Michael E
• Merry Brian

Classifications

• F02C7/277 Primary

  the starter being a {separate} turbine · CPC title

• F02C7/32

  Arrangement, mounting, or driving, of auxiliaries · CPC title

• F02C7/36

  Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user ({F02C3/107 - F02C3/13 and} F02C7/32 take precedence; couplings for transmitting rotation F16D; gearing in general F16H) · CPC title

• F05D2260/4023

  through a friction clutch · CPC title

• F16H3/30

  with driving and driven shafts not coaxial · CPC title