Superposition gearbox for engine performance

Patent metadata

Field	Value
Publication number	US-11220960-B2
Application number	US-201916591716-A
Country	US
Kind code	B2
Filing date	Oct 3, 2019
Priority date	Oct 3, 2019
Publication date	Jan 11, 2022
Grant date	Jan 11, 2022

Abstract

A gas turbine engine including a low speed spool including a low pressure compressor, a low speed output gear disposed on the low speed spool, a high speed spool including a high pressure compressor, a high speed output gear disposed on the high speed spool, a first tower shaft engaged to the low speed spool at the low speed output gear, a second tower shaft engaged to the high speed spool at the high speed output gear, and a superposition gearbox. The gas turbine engine further including a ring gear shaft coupled to drive the ring gear, a ring gear shaft drive gear. A low speed spool drive train gear ratio is between 0.5 to 2.0, the low speed spool drive train gear ratio being measured from the low speed output gear to the ring gear shaft drive gear.

First claim

What is claimed is:

1. A gas turbine engine comprising:
a low speed spool including a low pressure compressor;
a low speed output gear disposed on the low speed spool;
a high speed spool including a high pressure compressor;
a high speed output gear disposed on the high speed spool;
a first tower shaft engaged to the low speed spool at the low speed output gear;
a second tower shaft engaged to the high speed spool at the high speed output gear;
a superposition gearbox including a sun gear, a plurality of intermediate gears engaged to the sun gear and supported in a carrier, and a ring gear circumscribing the intermediate gears;
a ring gear shaft coupled to drive the ring gear;
a ring gear shaft drive gear disposed on the ring gear shaft and engaged with the first tower shaft;
a sun gear shaft coupled to drive the sun gear;
a sun gear shaft drive gear disposed on a sun gear shaft and engaged with the second tower shaft,
wherein a low speed spool drive train gear ratio is between 0.5 to 2.0, the low speed spool drive train gear ratio being measured from the low speed output gear to the ring gear shaft drive gear;
a first clutch assembly for selectively coupling the first tower shaft to the ring gear;
a second clutch assembly for selectively coupling the sun gear to the carrier; and
an accessory gearbox driven by an output of the superposition gearbox.

2. The gas turbine engine of claim 1 , wherein the output of the superposition gearbox comprises a lay shaft coupled to the carrier.

3. The gas turbine engine of claim 1 , wherein the first tower shaft and the second tower shaft are concentric about a common axis.

4. The gas turbine engine of claim 1 , wherein the first tower shaft and the second tower shaft are disposed about different axes.

5. The gas turbine engine of claim 1 , wherein the first clutch assembly and the second clutch assembly comprise one-way mechanical clutches.

6. The gas turbine engine of claim 1 , wherein the superposition gearbox is not fixed to a static structure of the engine.

7. The gas turbine engine of claim 1 , wherein a high speed spool drive train gear ratio is between 0.8 to 2.0, the high speed spool drive train gear ratio being measured from the high speed output gear to the sun gear shaft drive gear.

8. The gas turbine engine of claim 1 , wherein an epicycle gear ratio is between 2.5 to 4.5, the epicycle gear ratio being measured from the ring gear to the sun gear.

9. The gas turbine engine of claim 7 , wherein an epicycle gear ratio is between 2.5 to 4.5, the epicycle gear ratio being measured from the ring gear to the sun gear.

10. A gas turbine engine comprising:
a low speed spool including a low pressure compressor;
a low speed output gear disposed on the low speed spool;
a high speed spool including a high pressure compressor;
a high speed output gear disposed on the high speed spool;
a first tower shaft engaged to the low speed spool at the low speed output gear;
a second tower shaft engaged to the high speed spool at the high speed output gear;
a superposition gearbox including a sun gear, a plurality of intermediate gears engaged to the sun gear and supported in a carrier, and a ring gear circumscribing the intermediate gears;
a ring gear shaft coupled to drive the ring gear;
a ring gear shaft drive gear disposed on the ring gear shaft and engaged with the first tower shaft;
a sun gear shaft coupled to drive the sun gear;
a sun gear shaft drive gear disposed on a sun gear shaft and engaged with the second tower shaft,
wherein a high speed spool drive train gear ratio is between 0.8 to 2.0, the high speed spool drive train gear ratio being measured from the high speed output gear to the sun gear shaft drive gear;
a first clutch assembly for selectively coupling the first tower shaft to the ring gear;
a second clutch assembly for selectively coupling the sun gear to the carrier; and
an accessory gearbox driven by an output of the superposition gearbox.

11. The gas turbine engine of claim 10 , wherein the output of the superposition gearbox comprises a lay shaft coupled to the carrier.

12. The gas turbine engine of claim 10 , wherein the first tower shaft and the second tower shaft are concentric about a common axis.

13. The gas turbine engine of claim 10 , wherein the first tower shaft and the second tower shaft are disposed about different axes.

14. The gas turbine engine of claim 10 , wherein the first clutch assembly and the second clutch assembly comprise one-way mechanical clutches.

15. The gas turbine engine of claim 10 , wherein the superposition gearbox is not fixed to a static structure of the engine.

16. The gas turbine engine of claim 10 , wherein an epicycle gear ratio is between 2.5 to 4.5, the epicycle gear ratio being measured from the ring gear to the sun gear.

17. A gas turbine engine comprising:
a low speed spool including a low pressure compressor;
a low speed output gear disposed on the low speed spool;
a high speed spool including a high pressure compressor;
a high speed output gear disposed on the high speed spool;
a first tower shaft engaged to the low speed spool at the low speed output gear;
a second tower shaft engaged to the high speed spool at the high speed output gear;
a superposition gearbox including a sun gear, a plurality of intermediate gears engaged to the sun gear and supported in a carrier, and a ring gear circumscribing the intermediate gears;
a ring gear shaft coupled to drive the ring gear;
a ring gear shaft drive gear disposed on the ring gear shaft and engaged with the first tower shaft;
a sun gear shaft coupled to drive the sun gear;
a sun gear shaft drive gear disposed on a sun gear shaft and engaged with the second tower shaft,
wherein an epicycle gear ratio is between 2.5 to 4.5, the epicycle gear ratio being measured from the ring gear to the sun gear;
a first clutch assembly for selectively coupling the first tower shaft to the ring gear;
a second clutch assembly for selectively coupling the sun gear to the carrier; and
an accessory gearbox driven by an output of the superposition gearbox.

18. A gas turbine engine comprising:
a low speed spool including a low pressure compressor;
a low speed output gear disposed on the low speed spool;
a high speed spool including a high pressure compressor;
a high speed output gear disposed on the high speed spool;
a first tower shaft engaged to the low speed spool at the low speed output gear;
a second tower shaft engaged to the high speed spool at the high speed output gear;
a superposition gearbox including a sun gear, a plurality of intermediate gears engaged to the sun gear and supported in a carrier, and a ring gear circumscribing the intermediate gears;
a ring gear shaft coupled to drive the ring gear;
a ring gear shaft drive gear disposed on the ring gear shaft and engaged with the first tower shaft;
a sun gear shaft coupled to drive the sun gear; and
a sun gear shaft drive gear disposed on a sun gear shaft and engaged with the second tower shaft,
wherein a low speed spool drive train gear ratio is between 0.5 to 2.0, the low speed spool drive train gear ratio being measured from the low speed output gear to the ring gear shaft drive gear, and
wherein the first tower shaft and the second tower shaft are concentric about a common axis.

19. A gas turbine engine comprising:
a low speed spool including a low pressure compressor;
a low speed output gear disposed on the low speed spool;
a high speed spool including a high pre

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Leque Nicholas D
• Polly Joseph H

Classifications

• F05D2260/40311

  of the epicyclical, planetary or differential type · CPC title

• F16H57/02

  Gearboxes; Mounting gearing therein · CPC title

• F05D2240/60

  Shafts · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F16H3/46

  Gearings having only two central gears, connected by orbital gears (F16H3/68 - F16H3/78 take precedence) · CPC title