Gas turbine engine geared compressor with first and second input rotors

Patent metadata

Field	Value
Publication number	US-10302018-B2
Application number	US-201816121253-A
Country	US
Kind code	B2
Filing date	Sep 4, 2018
Priority date	Oct 31, 2012
Publication date	May 28, 2019
Grant date	May 28, 2019

Abstract

A booster assembly for a gas turbine engine having a first rotor assembly comprising a low pressure turbine drivingly connected to a fan via a first shaft and a second rotor assembly comprising a second turbine drivingly connected to a high pressure compressor via a second shaft. The first and second rotor assemblies are arranged to undergo relative rotation in use about a common axis. The booster assembly comprises a further compressor arranged to be disposed about said common axis between the fan and high-pressure compressor in a direction of flow and a gearing having first and second input rotors and an output rotor. The first input rotor is arranged to be driven by the first rotor assembly and the second input rotor is arranged to be driven by the second rotor assembly such that the output rotor drives the further compressor in dependence upon the difference in rotational speed between the first and second rotor assemblies.

First claim

What is claimed is:

1. An assembly for a gas turbine engine having a first rotor assembly comprising a low pressure turbine drivingly connected to a fan via a first shaft and a second rotor assembly comprising a second turbine drivingly connected to a high pressure compressor via a second shaft, the first and second rotor assemblies arranged to undergo relative rotation in use about a common axis, the assembly comprising:
a gearing having first and second input rotors and an output rotor, the first input rotor arranged to be driven by the first rotor assembly and the second input rotor arranged to be driven by the second rotor assembly, wherein
the gearing is a mechanical epicyclic gearing comprising at least one mechanical coupling including gears and teeth,
the output rotor is drivingly connected to an electrical machine, such that the gearing drives the electrical machine, and
the first input rotor comprises a ring gear, the second input rotor comprises a sun gear and the output rotor comprises a planet gear carrier member.

2. The assembly according to claim 1 , wherein the first or second input rotor comprises an extension portion of the respective first or second shaft.

3. The assembly according to claim 1 , wherein the first or second input rotor is connected to the respective first or second shaft by an intermediate wall or arm which is angled with respect to the common axis.

4. The assembly according to claim 1 , wherein the electrical machine is driven by the output rotor in a generator mode of operation and/or is arranged to drive the output rotor in a starter motor mode of operation.

5. The assembly according to claim 1 , wherein the output rotor is connected to or integral with a rotor of the electrical machine.

6. The assembly according to claim 5 , wherein the electrical machine rotor comprises one or more magnets.

7. The assembly according to claim 1 , wherein the electrical machine is disposed about the common axis.

8. The assembly according to claim 1 , further comprising a brake for any or any combination of the first rotor assembly, second rotor assembly, the first input rotor and/or the second input rotor.

9. A gas turbine engine comprising:
a first rotor assembly comprising a low pressure turbine drivingly connected to a fan via a first shaft;
a second rotor assembly comprising a second turbine drivingly connected to a high pressure compressor via a second shaft, the first and second rotor assemblies arranged to undergo relative rotation in use about a common axis, and
an assembly having a gearing having first and second input rotors and an output rotor, the first input rotor arranged to be driven by the first rotor assembly and the second input rotor arranged to be driven by the second rotor assembly, wherein
the gearing is a mechanical epicyclic gearing comprising at least one mechanical coupling including gears and teeth,
the output rotor is drivingly connected to an electrical machine, such that the gearing drives the electrical machine, and
the first input rotor comprises a planet gear carrier member, the second input rotor comprises a sun gear, and the output rotor comprises a ring gear.

10. The assembly according to claim 1 , wherein the first rotor assembly and the second rotor assembly are corotating.

11. The assembly according to claim 9 , wherein the first or second input rotor comprises an extension portion of the respective first or second shaft.

12. The assembly according to claim 9 , wherein the first or second input rotor is connected to the respective first or second shaft by an intermediate wall or arm which is angled with respect to the common axis.

13. The assembly according to claim 9 , wherein the electrical machine is driven by the output rotor in a generator mode of operation and/or is arranged to drive the output rotor in a starter motor mode of operation.

14. The assembly according to claim 9 , wherein the output rotor is connected to or integral with a rotor of the electrical machine.

15. The assembly according to claim 14 , wherein the electrical machine rotor comprises one or more magnets.

16. The assembly according to claim 9 , wherein the electrical machine is disposed about the common axis.

17. The assembly according to claim 9 , further comprising a brake for any or any combination of the first rotor assembly, second rotor assembly, the first input rotor and/or the second input rotor.

18. The assembly according to claim 9 , wherein the first rotor assembly and the second rotor assembly are contrarotating.

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Venter Gideon Daniel

Classifications

• F02C7/32

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

• F02K3/04

  the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type · CPC title

• F02K3/06

  with front fan · 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

• F02C3/067

  having counter-rotating rotors (F02C3/073 takes precedence) · CPC title