Constant speed accessory gearbox for turbine engine

Patent metadata

Field	Value
Publication number	US-12553380-B2
Application number	US-202418421616-A
Country	US
Kind code	B2
Filing date	Jan 24, 2024
Priority date	Jan 24, 2024
Publication date	Feb 17, 2026
Grant date	Feb 17, 2026

Abstract

An accessory drive system for a turbine engine includes a first input shaft that is coupled to a first engine drive shaft, a constant speed drive that is driven at an input speed by the first input shaft that varies, the constant speed drive includes an output that rotates at a constant speed independent of the input speed, an accessory gearbox that includes a first gear system that is driven by the output from the constant speed drive, and a first accessory component that is mounted to the accessory gearbox and driven by the gear system.

First claim

What is claimed is:

1 . An accessory drive system for a turbine engine comprising:
a first input shaft coupled to a first engine drive shaft; a constant speed drive that is driven at an input speed by the first input shaft that varies, wherein the constant speed drive includes an output that rotates at a constant speed independent of the input speed; an accessory gearbox including a first gear system driven by the output from the constant speed drive; and a first accessory component mounted to the accessory gearbox and driven by the first gear system, wherein the constant speed drive is mounted to the accessory gearbox and drives the first gear system, wherein the accessory gearbox includes a second gear system that is driven directly by the first input shaft and separate from the constant speed drive; a controller programmed to operate the constant speed drive to provide the constant speed of the output; and a heat exchanger that transfers heat generated within the constant speed drive into a cooling flow.

2 . The accessory drive system as recited in claim 1 , wherein the first input shaft comprises a first tower shaft and the first engine shaft comprise an outer shaft of a high spool of the turbine engine.

3 . The accessory drive system as recited in claim 2 , further comprising a second tower shaft driven by an inner shaft of a low spool of the turbine engine and an integrated gear system that is coupled to both the first tower shaft and the second tower shaft, wherein the constant speed drive and the integrated gear system are combined into a single integrated gearbox that drives the output.

4 . The accessory drive system as recited in claim 1 , further comprising a starter that is mounted to the accessory gearbox and coupled to drive the input shaft through the second gear system.

5 . The accessory drive system as recited in claim 1 , wherein the first accessory component comprises at least one of a lubrication pump, fuel pump, hydraulic fluid pump and a generator.

6 . A turbine engine assembly comprising:
a fan section including a plurality of blades rotatable about an axis; a high spool including a high pressure compressor and a high pressure turbine coupled through an outer shaft; a low spool including a low pressure turbine coupled to drive the fan section through an inner shaft; a high spool tower shaft coupled to the outer shaft; a low spool tower shaft coupled to the inner shaft; a constant speed drive that is driven at a variable input speed by at least one of the high spool tower shaft and the low spool tower shaft, wherein the constant speed drive includes an output that rotates at a constant speed independent of the variable input speed; an accessory gearbox including a first gear system driven by the output of the constant speed drive and wherein the constant speed drive is mounted to the accessory gearbox; at least one first accessory component that is mounted to the accessory gearbox and driven by the first gear system; wherein the accessory gearbox includes a second gear system that is coupled directly by one of the high spool tower shaft and the low spool tower shaft separate from the constant speed drive and at least one second accessory component is driven by the second gear system; and a heat exchanger that transfers heat generated within the constant speed drive into a cooling flow.

7 . The turbine engine assembly as recited in claim 6 , further comprising a controller programmed to operate the constant speed drive to provide the constant speed of the output.

8 . The turbine engine assembly as recited in claim 6 , further comprising a combination gear system that is coupled to both the high spool tower shaft and the low spool tower shaft, wherein the constant speed drive and the combination gear system are combined into a single integrated gearbox that drives the output.

9 . The turbine engine assembly as recited in claim 6 , further comprising a starter that is mounted to the accessory gearbox and coupled to drive one of the high spool tower shaft and the low spool tower shaft directly coupled to the second gear system.

10 . The turbine engine assembly as recited in claim 6 , wherein the at least one second accessory component comprises at least one of a lubrication pump, and a fuel pump, and the at least one first accessory component comprises at least one of a hydraulic fluid pump and a generator.

11 . A method of powering an accessory component of a turbine engine assembly comprising:
coupling at least one tower shaft that is driven by an engine shaft to a constant speed drive; controlling operation of the constant speed drive to drive an output at a constant speed independent of a speed of the engine shaft; coupling the output of the constant speed drive to a gear system supported within an accessory gearbox; driving at least one accessory component through the gear system; coupling a second gear system within the accessory gearbox to the at least one tower shaft to drive an accessory component directly and separate from the constant speed drive; and cooling the constant speed drive within a heat exchanger in thermal communication with a cooling flow.

Assignees

• Rtx Corp

Inventors

• Breault Andrew E
• Connors Joseph T
• Hoult John

Classifications

• F05D2260/4031

  as in toothed gearing · CPC title

• F02K3/06

  with front fan · 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

• F02C7/32 Primary

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

• F02C7/14

  of fluids in the plant {, e.g. lubricant or fuel (F02C7/185 takes precedence)} · CPC title