THERMALLY MATCHED COMPOSITE SLEEVE

• US 20100019600A1
• Filed: 07/01/2009
• Published: 01/28/2010
• Est. Priority Date: 07/28/2008
• Status: Active Grant

• Current Assignee: FMC Technologies Incorporated (TechnipFMC, plc)
• Original Assignee: Direct Drive Systems Inc. (TechnipFMC, plc)
• Inventors: Saban, Daniel M., Guedes-Pinto, Paulo
• Granted Patent: US 8,237,320 B2
• Time in Patent Office: Days
• US Class Current: 310/156.270
• CPC Class Codes: H02K 1/02 characterised by the magnetic material
• CPC Class Codes: H02K 1/165 Shape, form or location of the slots
• CPC Class Codes: H02K 1/278 Surface mounted magnets; Inset magnets
• CPC Class Codes: H02K 15/12 Impregnating, heating or drying of windings, stators, rotors or machines
• CPC Class Codes: H02K 3/12 arranged in slots
• CPC Class Codes: H02K 3/24 with channels or ducts for cooling medium between the conductors
• CPC Class Codes: H02K 3/28 Layout of windings or of connections between windings windings for pole-changing H02K17/06, H02K17/14, H02K19/12, H02K19/32
• CPC Class Codes: H02K 3/487 Slot-closing devices
• CPC Class Codes: H02K 3/50 Fastening of winding heads, equalising connectors, or connections thereto
• CPC Class Codes: H02K 5/1285 of the submersible type
• CPC Class Codes: Y10T 29/49009 Dynamoelectric machine
• CPC Class Codes: Y10T 29/49012 Rotor

Abstract

A sleeve about an electric machine rotor core and the plurality of permanent magnets has a fiber-reinforced composite layer about the rotor core and the plurality of permanent magnets. At least a portion of the sleeve about the rotor core and the permanent magnets has a coefficient of thermal expansion that is substantially equal to the aggregate coefficient of thermal expansion of the rotor core and the plurality of permanent magnets.

Claims

1. A rotor for an electrical machine comprising:

a rotor core substantially comprised of a first material;

a plurality of permanent magnets carried on the rotor core, the plurality of permanent magnets substantially comprised of a second material that is different from the first material; and

a sleeve about the rotor core and the plurality of permanent magnets and comprising a fiber-reinforced composite layer about the rotor core and the plurality of permanent magnets, at least a portion of the sleeve about the rotor core and the permanent magnets having a coefficient of thermal expansion that is substantially equal to the coefficient of thermal expansion of the plurality of permanent magnets.

2. The rotor of claim 1, wherein the fiber-reinforced composite layer comprises a plurality of elongate fibers, a polymer binder, and an additional material, an aggregate effective coefficient of thermal expansion of the elongate fibers and the polymer binder being desperate from the aggregate effective coefficient of thermal expansion of the plurality of permanent magnets.

3. The rotor of claim 2, wherein the additional material comprises at least one of at least one of ceramic or glass fillers in the form of at least one of fibers or powder.

4. The rotor of claim 1, wherein the fiber-reinforced composite layer comprises a plurality of elongate fibers and a polymer binder, and the fibers comprise at least one of ceramic, glass, or polymeric fibers.

5. The rotor of claim 1, wherein the at least a portion of the sleeve about the rotor core and the permanent magnets is substantially comprised of fiber-reinforced composite.

6. The rotor of claim 5, wherein the rotor core is substantially comprised of metal.

7. The rotor of claim 1, wherein the sleeve provides a majority of the support retaining the plurality of permanent magnets to the rotor core.

8. A rotor for an electrical machine comprising:

a rotor core substantially comprised of a first material;

a plurality of permanent magnets carried on the rotor core, the plurality of permanent magnets substantially comprised of a second material that is different from the first material; and

a sleeve about the rotor core and the plurality of permanent magnets and comprising a fiber-reinforced composite layer about the rotor core and the plurality of permanent magnets, at least a portion of the sleeve about the rotor core and the permanent magnets having a coefficient of thermal expansion that is substantially equal to the aggregate coefficient of thermal expansion of the rotor core and the plurality of permanent magnets.

9. The rotor of claim 8, wherein the fiber-reinforced composite layer comprises a plurality of elongate fibers, a polymer binder, and an additional material, an aggregate effective coefficient of thermal expansion of the elongate fibers and the polymer binder being desperate from the aggregate coefficient of thermal expansion of the rotor core and the plurality of permanent magnets.

10. The rotor of claim 9, wherein the additional material comprises at least one of ceramic or glass fillers in the form of at least one of fibers or powder.

11. The rotor of claim 8, wherein the fiber-reinforced composite layer comprises a plurality of elongate fibers and a polymer binder, and the fibers comprise at least one of ceramic, glass, or polymeric fibers.

12. The rotor of claim 8, wherein the at least a portion of the sleeve about the rotor core and the permanent magnets is substantially comprised of carbon fiber-reinforced composite.

13. The rotor of claim 12, wherein the rotor core is substantially comprised of metal.

18. The method of claim 13, wherein the core substantially comprises metal.

14. A method of retaining elements of an elongate electric machine rotor, the method comprising:

retaining a plurality of permanent magnets to a core of the rotor with a sleeve comprising a fiber-reinforced composite layer, the fiber-reinforced composite layer having a coefficient of thermal expansion that is substantially equal to the coefficient of thermal expansion of the permanent magnets; and

expanding the fiber-reinforced composite layer substantially along the length of the core of the rotor in response to a change in temperature in approximately the same amount as the permanent magnets expand along the length of the core of the rotor in response to the change temperature.

15. The method of claim 14, wherein the fiber-reinforced composite layer comprises a plurality of elongate fibers, a polymer binder, and an additional material, an aggregate effective coefficient of thermal expansion of the elongate fibers and the polymer binder being desperate from the aggregate effective coefficient of thermal expansion of the plurality of permanent magnets.

16. The method of claim 15, wherein the additional material comprises at least one of ceramic or glass fillers in the form of at least one of fibers or powder.

17. The method of claim 14, wherein the fiber-reinforced composite layer comprises a plurality of elongate fibers and a polymer binder, and the fibers comprise at least one of ceramic, glass, or polymeric fibers.