Gas turbine engine starter reduction gear train with geared rotary actuator

Patent metadata

Field	Value
Publication number	US-10473034-B2
Application number	US-201615201841-A
Country	US
Kind code	B2
Filing date	Jul 5, 2016
Priority date	Jul 5, 2016
Publication date	Nov 12, 2019
Grant date	Nov 12, 2019

Abstract

According to an aspect, a system for a gas turbine engine includes a reduction gear train operable to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine. The reduction gear train includes a starter interface gear that engages the starter gear train and a core-turning clutch operably connected to the starter interface gear. The reduction gear train also includes a geared rotary actuator including a primary planetary gear system, where the geared rotary actuator is operably connected to the core-turning clutch. The reduction gear train further includes a secondary planetary gear system operably connected to the primary planetary gear system and a core-turning input. The system also includes a mounting pad with an interface to couple a core-turning motor to the core-turning input of the reduction gear train.

First claim

What is claimed is:

1. A system for a gas turbine engine comprising:
a reduction gear train operable to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine, the reduction gear train comprising:
a starter interface gear that engages the starter gear train;
a core-turning clutch operably connected to the starter interface gear;
a geared rotary actuator comprising a primary planetary gear system, the geared rotary actuator operably connected to the core-turning clutch; and
a secondary planetary gear system operably connected to the primary planetary gear system and a core-turning input; and

a mounting pad comprising an interface to couple a core-turning motor to the core-turning input of the reduction gear train.

2. The system of claim 1 , wherein the starter interface gear engages a planet gear of the starter gear train, and the starter gear train is operably connected to the accessory gearbox through a starter clutch.

3. The system of claim 1 , wherein the core-turning clutch is an overrunning clutch.

4. The system of claim 1 , wherein the geared rotary actuator further comprises a ring gear driven by a carrier system.

5. The system of claim 4 , wherein the ring gear is operably connected to a splined shaft that interfaces with the core-turning clutch.

6. The system of claim 4 , wherein the primary planetary system comprises a sun gear operably connected to at least one planet gear that is operably connected to the carrier system.

7. The system of claim 6 , wherein each of the at least one planet gear is operably connected to an intermediate gear on a respective intermediate shaft, and the intermediate gear is operably connected to the ring gear.

8. An integrated starter and core-turning system for a gas turbine engine, the integrated starter and core-turning system comprising:
a starter comprising a starter gear train that interfaces to an accessory gearbox of the gas turbine engine; and
a reduction gearbox comprising:
a reduction gear train operable to drive rotation of the starter gear train, the reduction gear train comprising:
a starter interface gear operably connected to the starter gear train;
a core-turning clutch operably connected to the starter interface gear;
a geared rotary actuator comprising a primary planetary gear system, where the geared rotary actuator operably connected to the core-turning clutch; and
a secondary planetary gear system operably connected to the primary planetary gear system and a core-turning input; and

a mounting pad comprising an interface to couple a core-turning motor to the core-turning input of the reduction gear train.

9. The integrated starter and core-turning system of claim 8 , wherein the starter interface gear engages a planet gear of the starter gear train, and the starter gear train is operably connected to the accessory gearbox through a starter clutch.

10. The integrated starter and core-turning system of claim 8 , wherein the core-turning clutch is an overrunning clutch, the starter comprises a turbine that drives the starter gear train, and the core-turning motor is an electric motor.

11. The integrated starter and core-turning system of claim 8 , wherein the geared rotary actuator further comprises a ring gear driven by a carrier system.

12. The integrated starter and core-turning system of claim 11 , wherein the ring gear is operably connected to a splined shaft that interfaces with the core-turning clutch.

13. The integrated starter and core-turning system of claim 11 , wherein the primary planetary system comprises a sun gear operably connected to at least one planet gear that is operably connected to the carrier system.

14. The integrated starter and core-turning system of claim 13 , wherein each of the at least one planet gear is operably connected to an intermediate gear on a respective intermediate shaft, and the intermediate gear is operably connected to the ring gear.

15. The integrated starter and core-turning system of claim 8 , wherein the starter and the reduction gearbox are integrally formed within an outer housing.

16. A method of transmitting torque in a system for a gas turbine engine, the method comprising:
transmitting torque output of a core-turning motor through a core-turning input of a reduction gear train of the system;
transmitting torque at the core-turning input through a secondary planetary gear system and a primary planetary gear system of the reduction gear train, wherein the primary planetary gear system comprises a portion of a geared rotary actuator;
transmitting torque from the geared rotary actuator through a starter interface gear operably connected to a core-turning clutch; and
transmitting torque from the starter interface gear to drive rotation of a starter gear train that interfaces to an accessory gearbox of the gas turbine engine.

17. The method of claim 16 , further comprising:
transmitting torque from a starter turbine through the starter gear train to the accessory gearbox.

18. The method of claim 17 , further comprising:
decoupling, by the core-turning clutch, engagement of the reduction gear train with the starter gear train in response to the torque from the starter turbine.

19. The method of claim 18 , wherein the starter interface gear engages a planet gear of the starter gear train, and the starter gear train is operably connected to the accessory gearbox through a starter clutch.

20. The method of claim 16 , wherein the geared rotary actuator further comprises a ring gear driven by a carrier system, the ring gear is operably connected to a splined shaft that interfaces with the core-turning clutch, the primary planetary system comprises a sun gear operably connected to at least one planet gear that is operably connected to the carrier system, each of the at least one planet gear is operably connected to an intermediate gear on a respective intermediate shaft, and the intermediate gear is operably connected to the ring gear.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Harder Benjamin T
• Mcmasters Brian
• Nguyen James Vandung
• Wilson Dwayne Leon
• Fox Paul F
• Davis Richard Alan
• Hergert Richard R
• Roberts Jeffrey Todd
• Brown Jeff A
• Walker Daniel Richard
• Slayter Matthew Allen
• Sheridan William G

Classifications

• F01D21/12 Primary

  responsive to temperature · CPC title

• F02C7/277

  the starter being a {separate} turbine · CPC title

• F01D25/34

  Turning or inching gear · CPC title

• F02C7/32

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

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title