Turbomachine equipped with an embedded electric machine having a segmented and movable stator

Patent metadata

Field	Value
Publication number	US-11894738-B2
Application number	US-202117405147-A
Country	US
Kind code	B2
Filing date	Aug 18, 2021
Priority date	Aug 31, 2020
Publication date	Feb 6, 2024
Grant date	Feb 6, 2024

Abstract

A turbomachine equipped with an embedded electric machine having a segmented and movable stator is provided. In one aspect, a turbomachine defines a radial direction and includes a rotating component, actuators, and an electric machine. The electric machine includes a rotor assembly rotatable with and operatively coupled with the rotating component. The electric machine also includes a stator assembly having a stator split into stator segments. Each one of the stator segments is movable by one of the actuators between a first position and a second position along the radial direction, the stator segments each being closer to the rotor assembly along the radial direction when in the first position than when in the second position.

First claim

What is claimed is:

1. An electric machine defining an axial direction, a radial direction, and a centerline extending along the axial direction, the electric machine comprising:
a rotor assembly rotatable about the centerline;
a stator assembly having a stator split into stator segments, each one of the stator segments having an actuator associated therewith, each of the actuators being operable to move their respective one of the stator segments between a first position and a second position along the radial direction, the stator segments each being closer to the rotor assembly when in the first position than when in the second position;
a plurality of power converters, each of the plurality of power converters being electrically coupled to a respective stator segment of the stator segments; and
a controller operatively coupled with the actuators and being configured to:
receive data from one or more sensors associated with the electric machine;
identify a fault with the electric machine based on the data; and
operate the actuators to move their respective stator segments away from the rotor assembly from their respective first positions to their respective second positions in response to identifying the fault with the electric machine.

2. The electric machine of claim 1 , wherein the first position is an engaged position and the second position is a disengaged position.

3. The electric machine of claim 1 , wherein each one of the stator segments has an associated set of stator windings, and wherein the stator windings of each set are wound only within their respective stator segments.

4. The electric machine of claim 1 , wherein the stator segments are separately movable between their respective first and second positions.

5. The electric machine of claim 1 , wherein the stator segments include at least four stator segments.

6. The electric machine of claim 1 , the stator segments are each movable between their respective first and second positions along the radial direction a distance that is greater than 0.5 inches and less than 10 inches.

7. The electric machine of claim 1 , wherein the controller associated with the electric machine and operatively coupled with the actuators is configured to cause the actuators to move their respective stator segments away from the rotor assembly to respective partial power positions located between their respective first and second positions.

8. The electric machine of claim 1 , wherein each stator segment engages an adjacent one of the stator segments when the stator segments are in their respective first positions and are disengaged from one another in their respective second positions.

9. The electric machine of claim 1 , wherein the rotor assembly includes a plurality of permanent magnets.

10. The electric machine of claim 1 , wherein the stator segments are movable between their respective first and second positions simultaneously.

11. A turbomachine defining a radial direction, the turbomachine comprising:
a rotating component;
actuators;
an electric machine, comprising:
a rotor assembly rotatable with and operatively coupled with the rotating component; and
a stator assembly having a stator split into stator segments, each one of the stator segments having a respective actuator of the actuators associated therewith, each of the actuators being operable to move their respective one of the stator segments between a first position and a second position along the radial direction, the stator segments each being closer to the rotor assembly along the radial direction when in the first position than when in the second position;
a plurality of power converters, each of the plurality of power converters being electrically coupled to a respective stator segment of the stator segments; and

one or more sensors associated with the electric machine; and
a controller associated with the electric machine and communicatively coupled with the actuators and the one or more sensors, the controller being configured to:
receive data from the one or more sensors associated with the electric machine;
identify a fault with the electric machine based on the data; and
cause the actuators to move their respective stator segments away from the rotor assembly along the radial direction in response to identifying the fault with the electric machine.

12. The turbomachine of claim 11 , wherein the controller is further configured to:
receive an electrical power demand that indicates electrical power demanded by one or more electrical loads electrically coupled with the electric machine; and
cause the actuators to move their respective stator segments relative to the rotor assembly along the radial direction in response to receiving the electrical power demand.

13. The turbomachine of claim 11 , wherein the turbomachine is an aviation gas turbine engine, and wherein the rotating component is one of a low pressure shaft and a high pressure shaft of the aviation gas turbine engine.

14. A method, comprising:
operating an electric machine to convert electrical power to rotational power or to convert rotational power to electrical power, the electric machine having a stator assembly and a rotor assembly rotatable with a rotating component of a turbomachine, the stator assembly having a stator split into stator segments, wherein the conversion of electrical power is achieved using a plurality of power converters, each of the plurality of power converters being electrically coupled to a respective stator segment of the stator segments;
receiving data from one or more sensors associated with the electric machine;
identifying a fault with the electric machine based on the data; and
operate the actuators to move their respective stator segments away from the rotor assembly from their respective first positions to their respective second positions in response to identifying the fault condition withing the electric machine;
moving each one of the stator segments away from the rotor assembly along a radial direction defined by the turbomachine in response to identifying the fault condition within the electric machine.

15. The method of claim 14 , wherein the stator segments include a first stator segment and a second stator segment, and wherein moving each one of the stator segments away from the rotor assembly along the radial direction comprises moving the first stator segment and the second stator segment opposite one another along the radial direction.

16. The electric machine of claim 1 , wherein the one or more sensors comprises a temperature sensor and the fault is identified based on a measured temperature of the electric machine.

17. The electric machine of claim 16 , wherein the measured temperature is a stator temperature.

18. The turbomachine of claim 11 , wherein the one or more sensors comprises a temperature sensor and the fault is identified based on a stator temperature of the electric machine.

19. The method of claim 14 , wherein the one or more sensors comprises a temperature sensor and the fault is identified based on a measured temperature of the electric machine.

Assignees

• Gen Electric

Inventors

• Zatorski Darek Tomasz
• Osama Mohamed

Classifications

• H02K21/024 Primary

  Radial air gap machines · CPC title

• F02C7/00

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• H02K7/1823

  structurally associated with turbines or similar engines · CPC title

• H02K11/20

  for measuring, monitoring, testing, protecting or switching (rectifiers H02K11/04; power electronics H02K11/33) · CPC title

• H02K11/30

  Structural association with control circuits or drive circuits · CPC title