Generator temperature management for throttle loss recovery systems

Patent metadata

Field	Value
Publication number	US-9926807-B2
Application number	US-201514638232-A
Country	US
Kind code	B2
Filing date	Mar 4, 2015
Priority date	Mar 4, 2015
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

Turbine assemblies, loss recovery systems, and related fabrication methods are provided for managing temperatures associated with an electrical generator. One exemplary turbine assembly suitable for use in a loss recovery system includes a wheel configured to rotate in response to a portion of a fluid flow bypassing a flow control valve, a generator including a stator assembly disposed about a rotor coupled to the wheel to rotate in response to rotation of the wheel, a conductive structure in contact with the stator assembly, and an insulating structure radially encompassing the conductive structure and the generator. The conductive structure accesses at least a portion of the fluid flow bypassing the flow control valve and impacting the wheel, thereby providing thermal coupling between the stator assembly and the bypass fluid flow to transfer heat from the stator assembly to the bypass fluid flow via the conductive structure.

First claim

What is claimed is:

1. A turbine assembly comprising:
a wheel configured to rotate in response to a portion of a fluid flow within a volute, the portion of the fluid flow bypassing a flow control valve;
a generator including a stator assembly disposed about a rotor, the rotor being coupled to the wheel to rotate in response to rotation of the wheel;
a metallic structure in contact with the stator assembly, an end portion of the metallic structure defining at least a portion of the volute, wherein the end portion of the metallic structure is exposed to the portion of the fluid flow within the volute; and
an insulating structure radially encompassing the metallic structure and the generator.

2. The turbine assembly of claim 1 , wherein the insulating structure defines at least a portion of the volute for the portion of the fluid flow.

3. The turbine assembly of claim 2 , further comprising one or more guide vanes within the volute to direct the portion of the fluid flow towards the wheel, wherein the metallic structure contacts the one or more guide vanes.

4. The turbine assembly of claim 3 , wherein the one or more guide vanes are integral with the metallic structure.

5. The turbine assembly of claim 2 , further comprising a divider structure within the volute, wherein the metallic structure contacts the divider structure.

6. The turbine assembly of claim 1 , wherein the metallic structure radially circumscribes at least a portion of the stator assembly.

7. The turbine assembly of claim 6 , wherein the insulating structure comprises a thermoplastic molding compound.

8. The turbine assembly of claim 1 , further comprising an electronics assembly including electronics electrically coupled to the stator assembly, wherein the electronics assembly contacts the metallic structure.

9. The turbine assembly of claim 8 , wherein the electronics assembly is mounted on the metallic structure.

10. The turbine assembly of claim 1 , further comprising:
a rotary shaft disposed within the stator assembly, the rotary shaft coupling the rotor to the wheel; and
a bearing assembly to support the rotary shaft disposed between the stator assembly and the wheel, wherein the metallic structure is configured to retain the bearing assembly.

11. The turbine assembly of claim 1 , wherein the portion of the volute comprises a sidewall of the volute.

12. The turbine assembly of claim 1 , wherein the portion of the volute comprises a boundary of the volute.

13. A system comprising:
a turbine including a volute for a portion of a fluid flow and a wheel to rotate in response to the portion of the fluid flow, the portion of the fluid flow bypassing a flow control valve based on an orientation of the flow control valve with respect to the fluid flow;
a generator including a stator assembly radially circumscribing a rotor, the rotor being coupled to the wheel to rotate in response to rotation of the wheel;
a metallic structure in contact with the stator assembly and defining at least a portion of the volute, wherein a portion of the metallic structure is exposed to the portion of the fluid flow within the volute; and
an insulating structure radially circumscribing the metallic structure and the generator.

14. The system of claim 13 , further comprising one or more guide vanes within the volute to direct the portion of the fluid flow towards the wheel, wherein the metallic structure contacts the one or more guide vanes.

15. The system of claim 13 , further comprising a divider structure within the volute, wherein the metallic structure contacts the divider structure.

16. The system of claim 15 , further comprising a turbine housing defining at least a portion of the volute, wherein the divider structure is disposed between the turbine housing and the metallic structure.

17. A method of fabricating a turbine assembly, the method comprising:
forming a metallic structure in contact with a stator assembly of a generator, wherein an end portion of the metallic structure is configured to define a portion of a volute for a portion of a fluid flow, the portion of the fluid flow bypassing a flow control valve based on an orientation of the flow control valve with respect to the fluid flow;
forming an insulating structure about the metallic structure and the stator assembly after forming the metallic structure in contact with the stator assembly; and
mechanically coupling a turbine wheel to a rotor of the generator, the rotor being disposed within the stator assembly, wherein:
the turbine wheel is arranged to rotate in response to the portion of the fluid flow within the volute;
the end portion of the metallic structure is exposed to the portion of the fluid flow within the volute; and
the rotor rotates in response to rotation of the turbine wheel.

18. The method of claim 17 , further comprising providing a bearing assembly within a retaining portion of the metallic structure prior to mechanically coupling the turbine wheel to the rotor, wherein:
the bearing assembly circumscribes a rotary shaft disposed within the stator assembly;
the rotor is coupled to the rotary shaft; and
providing the turbine wheel comprises joining the turbine wheel to a protruding portion of the rotary shaft that extends from the bearing assembly.

19. The method of claim 17 , wherein forming the metallic structure in contact with the stator assembly comprises fitting a metallic sleeve over the stator assembly.

20. The method of claim 19 , wherein forming the insulating structure about the metallic structure and the stator assembly comprises overmolding the metallic sleeve and the stator assembly after fitting the metallic sleeve over the stator assembly.

Assignees

• Honeywell Int Inc

Inventors

• Thompson Glenn F
• Beresewicz Patrick
• Guidry Mike
• Love Andrew

Classifications

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F01D25/145 Primary

  Thermally insulated casings · CPC title

• F01D9/026

  Scrolls for radial machines or engines · CPC title

• F01D17/02

  Arrangement of sensing elements · CPC title

• F02D29/06

  peculiar to engines driving electric generators · CPC title