Gas turbine gearbox

• US 7,144,349 B2
• Filed: 04/06/2004
• Issued: 12/05/2006
• Est. Priority Date: 04/06/2004
• Status: Active Grant

• Current Assignee: Pratt & Whitney Canada Corporation (Rtx Corporation)
• Original Assignee: Pratt & Whitney Canada Corporation (Rtx Corporation)
• Inventors: Mitrovic, Lazar
• Primary Examiner(s): ESTREMSKY, SHERRY LYNN
• Application Number:
  US10/817,857
• Publication Number:
  US 20050221946A1
• Time in Patent Office: 973 Days
• Field of Search: 475/343, 475/331, 746/65.G, 746/65.GA, 746/65.F
• US Class Current: 475/331
• CPC Class Codes: B64D 35/00 Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
• CPC Class Codes: F01D 15/12 Combinations with mechanical gearing driven by multiple engines F01D13/00
• CPC Class Codes: F02C 6/206 the vehicles being airscrew driven
• CPC Class Codes: F02C 7/36 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 Class Codes: F16H 1/06 with parallel axes
• CPC Class Codes: F16H 1/2818 by allowing limited movement of the ring gear relative to the casing or shaft
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 74/19074 Single drive plural driven

Abstract

A gearbox for rotating a propeller in a selected one of a first and second direction is provided. The gearbox includes a many common components, selected irrespective of desired propeller direction, and a few unique components selected based on desired propeller direction.

Claims

1. A gearbox for rotating a propeller of a gas turbine engine in a selected one of a first and second direction, the gearbox comprising:

a casing defining an enclosure;

an output shaft rotating the propeller in the selected one of the first and second directions, the output shaft being partially enclosed in the casing;

a mating gear driving the output shaft through a gear train, the mating gear having a first position within the casing;

an input shaft receiving power from a turbine and rotating in the first direction, the input shalt being partially enclosed in the casing;

an input pinion coupled to the input shaft, the input pinion having a second position within the casing;

a plurality of accessory drive gears each adapted to drive one accessory, the plurality of accessory drive gears each having a third position within the casing;

a multiple member gear rotating in the first direction, each member of the multiple member gear being meshed with at least one of the plurality of accessory drive gears, and the multiple member gear having a fourth position within the casing;

wherein an interaction exists between the input pinion, mating gear and multiple member gear, selected from the group consisting of a first and second configuration with the first, second, third and fourth positions being the same in the first and second configuration, the first configuration consisting of the input pinion being meshed with the mating gear such that the mating gear rotates in the second direction, and the multiple member gear being meshed with a first idler gear which is meshed with an accessory pinion coupled to the input pinion, the first idler gear and the accessory pinion being located within the casing, and the second configuration consisting of the input pinion being meshed with a second idler gear which is meshed with the mating gear such that the mating gear rotates in the first direction, the second idler gear being located within the casing, and the multiple member gear being coupled to the mating gear; and

wherein the selection between the first and second configurations determines the selected one of the first and second directions.

2. The gearbox according to claim 1, wherein the casing is composed of a plurality of detachably connected housings.

3. The gearbox according to claim 1, wherein the mating gear is coaxial with the output shalt.

4. The gearbox according to claim 3, wherein the gear train is composed of a sun gear coaxial with the output shaft and meshed with a plurality of planet gears, a planet carrier rotationally supporting the plurality of planet gears, and a stationary ring gear meshed with the plurality of planet gears, the planet carrier being coupled to the output shaft and the mating gear being coupled to the sun gear.

5. The gearbox according to claim 3, wherein the multiple member gear is coaxial with the output shaft.

6. The gearbox according to claim 1, wherein the plurality of accessory drive gears are identical.

7. The gearbox according to claim 1, wherein one accessory drive gear is meshed with each member of the multiple member gear.

8. The gearbox according to claim 1, wherein the multiple member gear has three members.

9. A kit for providing a single output shaft turboprop gearbox, the output shaft being rotatable in selected single one of two opposite directions, the kit comprising:

the output shaft;

an input shaft;

a second-stage gear set co-operative with the output shaft;

a first first-stage gear set having a first configuration and co-operative with the input shaft and with the second-stage gear set, the first configuration being operable to permit rotation of the output shaft in a first one of the opposite directions through the second-stage gear set; and

a second first-stage gear set having a second configuration and co-operative with the input shaft and with the second-stage gear set, the second configuration being operable to permit rotation of the output shaft in a second one of the opposite directions through the second-stage gear set;

wherein only one of the first and second first-stage gear sets is selected and installed in a gearbox casing in engagement with the input shaft and the second-stage gear set depending on the selected single one of the opposite directions.

10. The kit according to claim 9, wherein at least one of the first and second first-stage gear sets is an offset reduction stage.

11. The kit according to claim 9, wherein the second-stage gear set is an epicyclic reduction stage.

12. The kit according to claim 9, further comprising at least one accessory drive gear driven by the selected one of the first and second first-stage gear sets.

13. The kit according to claim 9, further comprising the gearbox casing, the casing being configured to receive the second-stage gear set and the selected one of the first and second first-stage gear sets.

14. The kit according to claim 9, wherein one of the first and second first-stage gear sets includes at least one idler gear operable to reverse a direction of rotation of a driven gear in the one of the first-stage gear sets relative to a direction of rotation of a corresponding driven gear of the other of said first-stage gear sets.