Process for making a magnetic armature of divided structure and armature thus obtained

• US 4,347,449 A
• Filed: 03/06/1980
• Issued: 08/31/1982
• Est. Priority Date: 03/20/1979
• Status: Expired due to Term

• Current Assignee: Aerospatiale Societe Nationale Industrielle
• Original Assignee: Aerospatiale Societe Nationale Industrielle
• Inventors: Beau, Jean-Francois
• Primary Examiner(s): Hall, Carl E.
• Application Number:
  US06/127,830
• Time in Patent Office: 908 Days
• Field of Search: 29/605, 29/598, 29/596, 310/156, 310/261, 310/216, 310/218, 310/43, 310/42, 335/302, 335/297
• US Class Current: 310/216.045
• CPC Class Codes: F16C 32/0461 of stationary parts of the magnetic circuit
• CPC Class Codes: F16C 32/0468 of moving parts of the magnetic circuit, e.g. of the rotor
• CPC Class Codes: F16C 32/0476 with active support of one degree of freedom, e.g. axial magnetic bearings
• CPC Class Codes: H01F 3/06 made from wires
• CPC Class Codes: H01F 41/0206 Manufacturing of magnetic cores by mechanical means magnetic cores per se H01F27/24
• CPC Class Codes: Y10S 174/21 Rotor
• CPC Class Codes: Y10T 29/49012 Rotor

Abstract

The present invention relates to a process for making a magnetic armature of divided structure of annular shape and provided with a concentric annular groove, comprising the steps of winding a filamentary magnetic material on an annular mandrel, impregnating said winding with a hardening material, then cutting said winding along the equatorial plane of said mandrel, after said material has hardened. The invention is more particularly applicable to the production of divided magnetic armatures, especially for magnetic bearings.

Claims

1. A process for forming a magnetic armature having an annular shape and a concentric annular groove defined in part by concentric inner and outer radial rings, said inner ring having a radial thickness greater than that of said outer ring, said process comprising the steps of:

winding a filamentary magnetic material on an annular mandrel having a cross-section on one side of a plane at right angles to the axis of said mandrel, which cross-section corresponds in part to the cross-sectional contour of said groove, to produce a toroidal winding having an outer shape on said side of said plane which at least approximately corresponds to the desired outer shape of said armature;

impregnating said winding with a hardenable material capable when hardened of joining together the turns of said winding;

hardening said material; and

cutting said winding along said plane to form said armature.

2. A process of claim 1 wherein said mandrel varies in thickness, measured in a direction parallel to its axis, being greater at its end adjacent said outer ring than at its edge adjacent said inner ring.

3. A process as claimed in claim 1, wherein the filamentary material comprises a magnetic or non-magnetic, insulating coating.

4. A process as claimed in claim 1, wherein the section of the filamentary material is square, rectangular or hexagonal.

5. A process as claimed in claim 1, wherein the mandrel is symmetrical with respect to its equatorial plane so that each winding gives two identical armatures after impregnation and cutting.

6. A process as claimed in claim 1, wherein the impregnating material is magnetic or non-magnetic, insulating material.

7. The process of claim 5, wherein the impregnating material is a polymerisable resin.

8. A magnetic armature, obtained by carrying out the process as claimed in any one of claims 1, or 2-6.

9. An electromagnetic device and particularly a magnetic bearing, wherein it comprises an armature as claimed in claim 8.