Machine Device with Thermosiphon Cooling of Its Superconductive Rotor Winding

• US 20080164782A1
• Filed: 01/18/2006
• Published: 07/10/2008
• Est. Priority Date: 02/02/2005
• Status: Abandoned Application

• Current Assignee: Siemens AG
• Original Assignee: Siemens AG
• Inventors: Gromoll, Bernd
• Application Number:
  US11/883,509
• Publication Number:
  US 20080164782A1
• Time in Patent Office: Days
• US Class Current: 310/261
• CPC Class Codes: F28D 15/0266 with separate evaporating and condensing chambers connected by at least one conduit; Loop-type heat pipes; with multiple or common evaporating or condensing chambers F28D15/043 takes precedence
• CPC Class Codes: F28D 15/046 characterised by the material or the construction of the capillary structure
• CPC Class Codes: H02K 55/04 with rotating field windings
• CPC Class Codes: H02K 9/225 Heat pipes
• CPC Class Codes: Y02E 40/60 Superconducting electric elements or equipment; Power systems integrating superconducting elements or equipment

Abstract

A motor has a rotor, rotating about an axis, with a superconductive winding which is coupled to a central refrigerant cavity of the rotor via a winding support in a thermally conductive manner. The rotor cavity forms a tube system, together with the line sections laterally connected thereto and a condenser chamber of a refrigeration unit, located outside the motor, in which a refrigerant circulates as result of a thermosiphon effect. The refrigerant supply to the central rotor cavity is maintained, even with inclined positions of the rotor, when the rotor cavity is provided with a lining from a porous material, preferably a sintered metal, of high thermal conductivity.

Claims

1-9. -9. (canceled)

10. A machine device, comprising:

a stator;

a rotor mounted so as to be rotatable about a rotation axis extending along an axial direction in a rotor space substantially surrounded by said stator, said rotor including a central cylindrical rotor cavity and at least one rotor winding having superconductive conductors thermally conductively coupled to the central cylindrical rotor cavity which extends in the axial direction and is at least partially provided with a lining, made of a porous material with a thermal conductivity of at least 100 W/(m*K) at an operating temperature of the superconductive conductors, which forms capillary-like structures or cavities accessible to a refrigerant;

a stationary refrigeration unit disposed outside the rotor and enclosing a condenser space; and

tubular line sections extending between the central rotor cavity and the condenser space of said refrigeration unit, where said tubular line sections, the rotor space and the condenser space form a closed one-tube line system in which the refrigerant is circulated by utilizing a thermosiphon effect.

11. The machine device as recited in claim 10, wherein the porous material is a sintered material.

12. The machine device as recited in claim 11, wherein the porous material is a sintered copper material.

13. The machine device as recited in claim 10, wherein the lining is a porous coating.

14. The machine device as recited in claim 13, wherein a porosity of the lining is at least 3%.

15. The machine device as recited in claim 14, wherein a value of the thermal conductivity of the porous material at the operating temperature of the superconductive conductors corresponds to at least that of pure copper.

16. The machine device as recited in claim 15, wherein the superconductive conductors of the rotor winding are formed of a high-T_c superconductor material.

17. A method for producing a machine device as recited in claim 16, wherein the porous lining is press-fitted or shrink-fitted.

18. The machine device as recited in claim 13, wherein the porosity of the lining is at least 10%.