Compact accessory systems for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10731566-B2
Application number	US-201715786733-A
Country	US
Kind code	B2
Filing date	Oct 18, 2017
Priority date	Oct 18, 2017
Publication date	Aug 4, 2020
Grant date	Aug 4, 2020

Abstract

An accessory system for a gas turbine engine having a driveshaft with an axis of rotation is provided. The system includes a towershaft coupled to the driveshaft and rotatable about a towershaft axis of rotation. The towershaft includes a towershaft bevel gear. The system includes a primary shaft including a first bevel gear and a second bevel gear that each revolve about a primary shaft axis of rotation. The first bevel gear is coupled to the towershaft bevel gear. The system includes a secondary shaft including a third bevel gear and a fourth bevel gear that each revolve about a secondary shaft axis of rotation. The third bevel gear is coupled to the second bevel gear. The system includes a tertiary shaft including a fifth bevel gear that revolves about a tertiary shaft axis of rotation. The fifth bevel gear is coupled to the fourth bevel gear.

First claim

What is claimed is:

1. An accessory system for a gas turbine engine having a driveshaft with an axis of rotation, the accessory system comprising:
a towershaft coupled to the driveshaft and rotatable about a towershaft axis of rotation transverse to the axis of rotation of the gas turbine engine, the towershaft including a towershaft bevel gear at a distal end;
a primary shaft including a first bevel gear and a second bevel gear that each revolve about a primary shaft axis of rotation, the first bevel gear coupled to the towershaft bevel gear to drive the primary shaft;
a secondary shaft including a third bevel gear and a fourth bevel gear that each revolve about a secondary shaft axis of rotation that is substantially transverse to the primary shaft axis of rotation, the third bevel gear coupled to the second bevel gear to drive the secondary shaft;
a tertiary shaft including a fifth bevel gear that revolves about a tertiary shaft axis of rotation that is substantially parallel to the primary shaft axis of rotation, the fifth bevel gear coupled to the fourth bevel gear to drive the tertiary shaft; and
a quaternary shaft including a seventh bevel gear and an eighth bevel gear that each revolve about a quaternary shaft axis of rotation that is substantially transverse to the primary shaft axis of rotation, the seventh bevel gear coupled to the second bevel gear to drive the quaternary shaft.

2. The accessory system of claim 1 , wherein the primary shaft is coupled to a first accessory associated with the gas turbine engine, and the primary shaft includes a bearing housing assembly, the bearing housing assembly comprising:
an accessory mount coupled to the primary shaft and to the accessory, the accessory mount including a lock ring that is movable relative to the accessory mount and the primary shaft to adjust a contact pattern between the towershaft bevel gear and the first bevel gear.

3. The accessory system of claim 1 , wherein the primary shaft is coupled to a first accessory associated with the gas turbine engine, and the primary shaft includes a bearing housing assembly, the bearing housing assembly comprising:
an accessory mount coupled to the primary shaft and to the accessory, the accessory mount including a lock cylinder that is movable relative to the accessory mount and the primary shaft to adjust a contact pattern between the towershaft bevel gear and the first bevel gear.

4. The accessory system of claim 1 , further comprising a second tertiary shaft including a sixth bevel gear that revolves about the tertiary shaft axis of rotation, the sixth bevel gear coupled to the fourth bevel gear to drive the second tertiary shaft.

5. The accessory system of claim 1 , wherein the tertiary shaft drives a second accessory of the accessory system and the second tertiary shaft drives a third accessory of the accessory system.

6. The accessory system of claim 1 , further comprising a quinary shaft including a tenth bevel gear that revolves about a quinary shaft axis of rotation that is substantially transverse to the quaternary shaft axis of rotation, the tenth bevel gear coupled to the eighth bevel gear to drive the quinary shaft.

7. The accessory system of claim 6 , wherein the quaternary shaft includes a ninth bevel gear that revolves about the quaternary shaft axis of rotation.

8. The accessory system of claim 7 , further comprising a second quinary shaft including an eleventh bevel gear that revolves about the quinary shaft axis of rotation, the eleventh bevel gear coupled to the ninth bevel gear to drive the second quinary shaft.

9. The accessory system of claim 8 , wherein the quinary shaft drives a fourth accessory of the accessory system and the quinary shaft drives a fifth accessory of the accessory system.

10. The accessory system of claim 7 , wherein the quaternary shaft includes a first end opposite a second end, the seventh bevel gear is coupled at the first end, the ninth bevel gear coupled at the second end, and the tenth bevel gear is coupled to the quaternary shaft between the first end and the ninth bevel gear.

11. The accessory system of claim 1 , wherein the secondary shaft axis of rotation and the quaternary shaft axis of rotation intersect each other at a point on the primary shaft axis of rotation.

12. The accessory system of claim 1 , wherein the secondary shaft is coupled to a sixth accessory of the accessory system to drive the sixth accessory.

13. An accessory system for a gas turbine engine having a driveshaft with an axis of rotation, the accessory system comprising:
a towershaft coupled to the driveshaft and rotatable about a towershaft axis of rotation transverse to the axis of rotation of the gas turbine engine, the towershaft including a towershaft bevel gear at a distal end;
a primary shaft including a first bevel gear and a second bevel gear that each revolve about a primary shaft axis of rotation, the first bevel gear coupled to the towershaft bevel gear to drive the primary shaft;
a secondary shaft including a third bevel gear and a fourth bevel gear that each revolve about a secondary shaft axis of rotation that is substantially transverse to the primary shaft axis of rotation, the third bevel gear coupled to the second bevel gear to drive the secondary shaft;
a tertiary shaft including a fifth bevel gear that revolves about a tertiary shaft axis of rotation that is substantially transverse to the secondary shaft axis of rotation, the fifth bevel gear coupled to the fourth bevel gear to drive the tertiary shaft; and
a quaternary shaft including a sixth bevel gear and a seventh bevel gear that each revolve about a quaternary shaft axis of rotation that is substantially transverse to the primary shaft axis of rotation, the sixth bevel gear coupled to the second bevel gear to drive the quaternary shaft.

14. The accessory system of claim 13 , further comprising a second tertiary shaft including an eighth bevel gear that revolves about the tertiary shaft axis of rotation, the eighth bevel gear coupled to the fourth bevel gear to drive the second tertiary shaft.

15. The accessory system of claim 13 , further comprising a quinary shaft including a ninth bevel gear that revolves about a quinary shaft axis of rotation that is substantially transverse to the quaternary shaft axis of rotation, the ninth bevel gear coupled to the seventh bevel gear to drive the quinary shaft.

16. The accessory system of claim 15 , wherein the quaternary shaft includes a tenth bevel gear that revolves about the quaternary shaft axis of rotation.

17. The accessory system of claim 16 , further comprising a second quinary shaft including an eleventh bevel gear that revolves about the quinary shaft axis of rotation, the eleventh bevel gear coupled to the tenth bevel gear to drive the second quinary shaft.

18. The accessory system of claim 13 , wherein the primary shaft is coupled to a first accessory associated with the gas turbine engine, and the primary shaft includes a bearing housing assembly, the bearing housing assembly comprising:
an accessory mount coupled to the primary shaft and to the accessory, the accessory mount including a lock cylinder that is movable relative to the accessory mount and the primary shaft to adjust a contact pattern between the towershaft bevel gear and the first bevel gear.

19. An accessory system for a gas turbine engine having a driveshaft with an axis of rotation, the accessory system comprising:
a towershaft coupled to the driveshaft and rotatable about a towershaft axis of rotation transverse

Assignees

• Honeywell Int Inc

Inventors

• Alstad Shawn
• Dobosz Tomasz
• Felix Rocio Chavez

Classifications

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• F05D2260/4031

  as in toothed gearing · CPC title

• F16H1/222

  with non-parallel axes · CPC title

• F02C7/32 Primary

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

• F05D2240/50

  Bearings · CPC title