Gas turbine engine fuel system

Patent metadata

Field	Value
Publication number	US-10378445-B2
Application number	US-201514694403-A
Country	US
Kind code	B2
Filing date	Apr 23, 2015
Priority date	May 2, 2014
Publication date	Aug 13, 2019
Grant date	Aug 13, 2019

Abstract

The present application discloses a fuel system for a gas turbine engine. The engine includes a main alternating current electrical generator driven by an engine shaft such that the electrical output frequency of the electrical generator varies in dependence on shaft rotational speed. The fuel system includes a variable flow fuel pump for providing a fuel flow to the engine, a frequency and/or voltage controller configured to provide electrical power having at least one of a predetermined output frequency and a predetermined voltage, and a variable speed electric motor configured to drive the fuel pump. The electric motor includes an induction motor having a stator and at least a first rotor, the stator having first and second sets of stator windings. Each set of stator windings is configured to impart a torque on the rotor in use.

First claim

The invention claimed is:

1. A fuel system for a gas turbine engine, the gas turbine engine comprising a combustor having a fuel injector, the gas turbine engine comprising a main alternating current electrical generator driven by an engine shaft such that an electrical output frequency of the electrical generator varies in dependence on engine rotational speed, the fuel system comprising:
a variable flow fuel pump configured to provide a fuel flow to the fuel injector;
a frequency and/or voltage controller configured to provide electrical power having at least one of a predetermined output frequency and a predetermined voltage; and
a variable speed electric motor configured to drive the fuel pump;
the electric motor comprising an induction motor having a stator and at least a first rotor, the stator having first and second sets of stator windings, each set of stator windings being configured to impart a torque on the first rotor to drive the fuel pump in use, the first set of stator windings being supplied only with electrical power from an AC bus powered by the main generator, the electrical power from the AC bus supplied to the first set of stator windings having a same electrical output frequency and voltage as the electrical output frequency and voltage output by the main generator, and the second set of stator windings being supplied only with electrical power output from the frequency and/or voltage controller.

2. The fuel system according to claim 1 , wherein one or each set of stator windings is polyphase, and comprises three electrical phases.

3. The fuel system according to claim 1 , wherein each of the sets of stator windings is arranged around a circumference of the stator.

4. The fuel system according to claim 3 , wherein the first and second sets of stator windings are arranged alternately around the circumference of the stator, such that each stator winding of the first set is located between a stator winding of the second set.

5. The fuel system according to claim 1 , wherein the fuel system comprises a stator controller configured to selectively activate one or more electrical stator windings of the sets of stator windings.

6. The fuel system according to claim 1 , wherein the electric motor comprises a second rotor mechanically coupled to the first rotor, wherein the first rotor is associated with the first set of stator windings, and the second rotor is associated with the second set of stator windings.

7. The fuel system according to claim 6 , wherein the first and second rotors are mounted to a common shaft and arranged co-axially.

8. The fuel system according to claim 1 , wherein the main generator comprises a generator control unit configured to control the voltage of power generated by the main alternating current generator.

9. The fuel system according to claim 1 , wherein the frequency and/or voltage controller is powered by the AC bus.

10. The fuel system according to claim 1 , wherein a plurality of main alternating current electrical generators are provided.

11. The fuel system according to claim 10 , wherein one of the plurality of main alternating current electrical generators is arranged to only provide electrical power to engine loads such as the electric motor configured to drive the fuel pump.

12. A gas turbine engine comprising the fuel system in accordance claim 1 .

13. A method of controlling the fuel system in accordance with claim 1 , the method comprising:
controlling the frequency and/or voltage of the electrical power in the second set of stator windings to adjust the rotational speed of the rotor to thereby operate the fuel pump to match a fuel demand of the engine.

Assignees

• Rolls Royce Plc

Inventors

• Edwards Huw Llewelyn
• Husband Stephen Mark
• Cullen John James Anthony

Classifications

• F04C2270/105

  Controlled or regulated · CPC title

• F04C2210/1044

  Fuel · CPC title

• H02K16/00

  Machines with more than one rotor or stator {(machines for transmitting mechanical power from a driving shaft to a driven shaft and comprising structurally interrelated motor and generator parts H02K51/00; permanent magnet machines with multiple rotors or stators relatively rotated for vectorially combining the excitation fields or the armature voltages H02K21/029)} · CPC title

• F02C9/30

  characterised by variable fuel pump output · CPC title

• H02K16/02

  Machines with one stator and two {or more} rotors · CPC title