IP Library Granted Patent US 11,346,427
Granted Patent B2
US 11,346,427 · App. 16/274,332 · Granted May 31, 2022

Accessory gearbox for gas turbine engine with variable transmission

Inventors: Hung Duong (Unionville, CT); Marc J. Muldoon (Marlborough, CT); Gabriel L. Suciu (Glastonbury, CT)
Assignee: Raytheon Technologies Corporation
F16H3/001F02C7/32F02K3/06F16H3/006F16H3/02F05D2260/4031
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Quick Facts
Patent No.
US 11,346,427
App. No.
16/274,332
Granted
May 31, 2022
Kind
B2
Abstract

An auxiliary gearbox has a low speed input shaft driving a first plurality of accessories. A high speed input shaft drives a second plurality of accessories. The first plurality of accessories rotating about a first set of rotational axes, which are parallel to each other and perpendicular to a first plane. The second plurality of accessories rotating about a second set of rotational axes, which are parallel to each other and perpendicular to a second plane. The first and second planes extending in opposed directions away from a drive input axis of the high speed input shaft and the low speed input shaft. The low speed input shaft drives a variable speed transmission. A gas turbine engine is also disclosed.

Claims (24)

1. A gas turbine engine comprising:

a low speed input shaft from a lower speed spool and a high speed input shaft from a higher speed spool, said low speed input shaft connected to drive a first plurality of accessories, and said high speed input shaft connected to drive a second plurality of accessories, said first plurality of accessories rotating about a first set of rotational axes, which are parallel to each other but spaced along an axial input direction and are perpendicular to a first plane and said second plurality of accessories rotating about a second set of rotational axes, which are parallel to each other and spaced along an axial input direction and perpendicular to a second plane;

said first and second planes extending in opposed directions away from a drive input axis of said high speed input shaft and said low speed input shaft, said first plurality of accessories and said second plurality of accessories together forming a v-shaped gearbox arrangement, with said first and second planes extending away from each other to provide the v-shape; and

said low speed input shaft driving a transmission gear, said transmission gear being an input to a variable speed transmission, and said variable speed transmission varying an input speed to a desired output speed, and said variable speed transmission in turn driving at least some of said first plurality of accessories.

2. The gas turbine engine as set forth in claim 1 , wherein said low speed input shaft and said high speed input shaft are concentric.

3. The gas turbine engine as set forth in claim 2 , wherein said high speed input shaft is hollow and said low speed input shaft is positioned within said high speed input shaft.

4. The gas turbine engine as set forth in claim 3 , wherein each of said low speed and high speed input shafts drives a bevel gear and, in turn, said bevel gears drive first gears to drive said first plurality of accessories and said second plurality of accessories, respectively.

5. The gas turbine engine as set forth in claim 4 , wherein each of said bevel gears drive one of said first gears, which is engaged to drive another gear, and said another gear engaged to drive a third gear.

6. The gas turbine engine as set forth in claim 5 , wherein said low speed and high speed input shafts extend from input gears connected to the lower speed spool and the higher speed spool, with said lower speed spool including a low speed compressor driven by a low speed turbine and said higher speed spool includes a high speed compressor driven by a high speed turbine, and said input gears from said high and low speed spool driving said low speed and said high speed input shafts along concentric axes.

7. The gas turbine engine as set forth in claim 6 , wherein said low speed input shaft and said high speed input shaft each being driven by tower shafts for rotation about a tower shaft drive axis, and said tower shaft drive axis being non-parallel to said low speed and high speed input shafts, and said tower shafts driving said low speed input shaft and said high speed input shaft through input bevel gears.

8. The gas turbine engine as set forth in claim 1 , wherein each of said low speed and high speed input shafts drive a bevel gear and, in turn, said bevel gears drive first gears to drive said first plurality of accessories and said second plurality of accessories, respectively.

9. The gas turbine engine as set forth in claim 8 , wherein each of said bevel gears drive one of said first gears, which is engaged to drive another gear, and said another gear engaged to drive a third gear.

10. The gas turbine engine as set forth in claim 1 , wherein said low speed and high speed input shafts extend from input gears connected to the lower speed spool and the higher speed spool, with said lower speed spool including a low speed compressor driven by a low speed turbine and said higher speed spool includes a high speed compressor driven by a high speed turbine, and said input gears from said high and low speed spool driving said low speed and said high speed input shafts along concentric axes.

11. The gas turbine engine as set forth in claim 1 , wherein the engine is a two spool engine with the lower speed spool also driving a low speed compressor and a fan.

12. An auxiliary gearbox for a gas turbine engine comprising:

a low speed input shaft and a high speed input shaft, said low speed input shaft connected to drive a first plurality of accessories, and said high speed input shaft connected to drive a second plurality of accessories, said first plurality of accessories rotating about a first set of rotational axes, which are parallel to each other but spaced along an axial input direction and are perpendicular to a first plane and said second plurality of accessories rotating about a second set of rotational axes, which are parallel to each other and spaced along an axial input direction and perpendicular to a second plane;

said first and second planes extending in opposed directions away from a drive input axis of said high speed input shaft and said low speed input shaft, said first plurality of accessories and said second plurality of accessories together forming a v-shaped gearbox arrangement, with said first and second planes extending away from each other to provide the v-shape; and

said low speed input shaft driving a transmission gear, said transmission gear being an input to a variable speed transmission, and said variable speed transmission varying an input speed to a desired output speed, and said variable speed transmission in turn driving at least some of said first plurality of accessories.

13. The gearbox as set forth in claim 12 , wherein said low speed input shaft and said high speed input shaft are concentric.

14. The gearbox as set forth in claim 13 , wherein said high speed input shaft is hollow and said low speed input shaft is positioned within said high speed input shaft.

15. The gearbox as set forth in claim 14 , wherein each of said low speed and high speed input shafts drives a bevel gear and, in turn, said bevel gears drive gears to drive said first plurality of accessories and said second plurality of accessories, respectively.

16. The gearbox as set forth in claim 15 , wherein each of said bevel gears drive a gear, which is engaged to drive another gear, and said another gear engaged to drive a third gear.

17. The gearbox as set forth in claim 16 , wherein said low speed and high speed input shafts extend from input gears to be connected to a lower speed spool and a higher speed spool, with the lower speed spool including a low speed compressor driven by a low speed turbine and the higher speed spool includes a high speed compressor driven by a high speed turbine, and said input gears driving said low speed and said high speed input shafts along concentric axes.

18. The gearbox as set forth in claim 17 , wherein said input gears are part of an angle drive having bevel gears.

Assignments (4)
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE SPELLING ON THE ADDRESS 10 FARM SPRINGD ROAD FARMINGTONCONNECTICUT 06032 PREVIOUSLY RECORDED ON REEL 057190 FRAME 0719. ASSIGNOR(S) HEREBY CONFIRMS THE CORRECT SPELLING OF THE ADDRESS 10 FARM SPRINGS ROAD FARMINGTON CONNECTICUT 06032. Recorded Aug 19, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057226/0390 →
CHANGE OF NAME Recorded Aug 16, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 057190/0719 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 13, 2019
From: DUONG, HUNG; MULDOON, MARC J.; SUCIU, GABRIEL L.
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 048316/0022 →