Geared gas turbine engine and a gearbox

Patent metadata

Field	Value
Publication number	US-10364753-B2
Application number	US-201715628767-A
Country	US
Kind code	B2
Filing date	Jun 21, 2017
Priority date	Jul 8, 2016
Publication date	Jul 30, 2019
Grant date	Jul 30, 2019

Abstract

A gas turbine engine comprises a gearbox comprising a sun gear, an annulus gear, a plurality of planet gears and a carrier. The carrier comprises a primary structure and at least one reinforcing structure. The primary structure comprises a first material and the at least one reinforcing structure comprises a second material. The primary structure includes a first ring, a second ring spaced axially from the first ring and a plurality of circumferentially spaced axles extending axially between the first ring and the second ring. Each planet gear is rotatably mounted on a respective one of the axles by a bearing. The reinforcing structure is secured to the primary structure and the reinforcing structure comprises a particulate reinforced material or a fiber reinforced material. The reinforcing structure increases the stiffness of the carrier and reduces the weight of the carrier.

First claim

The invention claimed is:

1. A gas turbine engine comprising a gearbox, the gearbox comprising a sun gear, an annulus gear, a plurality of planet gears and a carrier, the sun gear meshing with the planet gears and the planet gears meshing with the annulus gear, the carrier comprising a primary structure and at least one reinforcing structure, the primary structure comprising a first material and the at least one reinforcing structure comprising a second material, the primary structure comprising a first ring, a second ring spaced axially from the first ring and a plurality of circumferentially spaced axles extending axially between the first ring and the second ring, each planet gear being rotatably mounted on a respective one of the axles, the at least one reinforcing structure being secured to the primary structure, a first reinforcing structure of the at least one reinforcing structure being secured to the first ring, a second reinforcing structure of the at least one reinforcing structure being secured to the second ring, the first reinforcing structure and the second reinforcing structure each comprising an annular member, and the at least one reinforcing structure comprising a reinforced material, the reinforced material being selected from a group consisting essentially of a particulate reinforced material and a fiber reinforced material,
wherein the reinforced material is selected from a group consisting essentially of a polymer matrix composite with long reinforcing fibers, a metal matrix composite with long reinforcing fibers and a ceramic matrix composite with long reinforcing fibers,
wherein the first and second rings have a plurality of circumferentially spaced bosses, each axle locating in a corresponding one of the bosses in the first ring and a corresponding one of the bosses in the second ring, and
wherein the long reinforcing fibers are arranged in a star shape, the long reinforcing fibers in the star shape are wound partially around each boss of the first ring.

2. A gas turbine engine as claimed in claim 1 wherein the first ring is selected from a group consisting essentially of an annular plate and an annular framework.

3. A gas turbine engine as claimed in claim 1 wherein the second ring is selected from a group consisting essentially of an annular plate and an annular framework.

4. A gas turbine engine as claimed in claim 1 wherein the primary structure comprises an unreinforced material.

5. A gas turbine engine as claimed in claim 4 wherein the primary structure comprises a metal selected from a group consisting essentially of steel, titanium, a titanium alloy, nickel, a nickel alloy, aluminum and an aluminum alloy.

6. A gas turbine engine as claimed in claim 1 wherein the primary structure comprises a particulate reinforced material.

7. A gas turbine engine as claimed in claim 6 wherein the particulate reinforced material of the primary structure is selected from a group consisting essentially of a polymer matrix composite, a metal matrix composite and a ceramic matrix composite.

8. A gas turbine engine as claimed in claim 1 wherein the first and second reinforcing structures are coaxial with the planet gear carrier.

9. A gas turbine engine as claimed in claim 1 wherein the first and second reinforcing structures each have a plurality of circumferentially spaced apertures.

10. A gearbox, the gearbox comprising a sun gear, an annulus gear, a plurality of planet gears and a carrier, the sun gear meshing with the planet gears and the planet gears meshing with the annulus gear, the carrier comprising a primary structure and at least one reinforcing structure, the primary structure comprising a first material and the at least one reinforcing structure comprising a second material, the primary structure comprising a first ring, a second ring spaced axially from the first ring and a plurality of circumferentially spaced axles extending axially between the first ring and the second ring, each planet gear being rotatably mounted on a respective one of the axles, the at least one reinforcing structure being secured to the primary structure, and the at least one reinforcing structure comprising a reinforced material, the reinforced material being selected from a group consisting essentially of a particulate reinforced material and a fiber reinforced material, a first reinforcing structure of the at least one reinforcing structure being secured to the first ring, a second reinforcing structure of the at least one reinforcing structure being secured to the second ring, the first reinforcing structure and the second reinforcing structure each comprising an annular member,
wherein the reinforced material is selected from a group consisting essentially of a polymer matrix composite with long reinforcing fibers, a metal matrix composite with long reinforcing fibers and a ceramic matrix composite with long reinforcing fibers,
wherein the first and second rings have a plurality of circumferentially spaced bosses, each axle locating in a corresponding one of the bosses in the first ring and a corresponding one of the bosses in the second ring, and
wherein the long reinforcing fibers are arranged in a star shape, the long reinforcing fibers in the star shape are wound partially around each boss of the first ring.

11. A gas turbine engine comprising a gearbox, the gearbox comprising a sun gear, an annulus gear, a plurality of planet gears and a carrier, the sun gear meshing with the planet gears and the planet gears meshing with the annulus gear, the carrier comprising a primary structure and at least one reinforcing structure, the primary structure comprising a first material and the at least one reinforcing structure comprising a second material, the primary structure comprising a first ring, a second ring spaced axially from the first ring and a plurality of circumferentially spaced axles extending axially between the first ring and the second ring, each planet gear being rotatably mounted on a respective one of the axles, the at least one reinforcing structure being secured to the primary structure, a first reinforcing structure of the at least one reinforcing structure being secured to the first ring, a second reinforcing structure of the at least one reinforcing structure being secured to the second ring, the first reinforcing structure and the second reinforcing structure each comprising an annular member, and the at least one reinforcing structure comprising a reinforced material, the reinforced material being selected from a group consisting essentially of a particulate reinforced material and a fiber reinforced material,
wherein the reinforced material is selected from a group consisting essentially of a polymer matrix composite with long reinforcing fibers, a metal matrix composite with long reinforcing fibers and a ceramic matrix composite with long reinforcing fibers,
wherein the first and second rings have a plurality of circumferentially spaced bosses, each axle locating in a corresponding one of the bosses in the first ring and a corresponding one of the bosses in the second ring, and
wherein the long reinforcing fibers are arranged into at least one continuous loop arranged at a diameter greater than the diameter at which the bosses are arranged.

12. A gas turbine engine comprising a gearbox, the gearbox comprising a sun gear, an annulus gear, a plurality of planet gears and a carrier, the sun gear meshing with the planet gears and the planet gears meshing with the annulus gear, the carrier comprising a primary structure and at least one reinforcing structure, the primary structure comprising a first material and the at least one reinforcing structure comprising a

Assignees

• Rolls Royce Plc

Inventors

• Madge Jason J

Classifications

• F05D2260/53

  using gears · CPC title

• F05D2300/6032

  Metal matrix composites [MMC] · CPC title

• F02C7/36 Primary

  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

• Y02T50/672

  Cross-Sectional Technologies · mapped topic

• F05D2260/40311

  of the epicyclical, planetary or differential type · CPC title