Rotor assembly and method of manufacture for electric machines having multiple magnet lengths

Patent metadata

Field	Value
Publication number	US-9847704-B2
Application number	US-201514932590-A
Country	US
Kind code	B2
Filing date	Nov 4, 2015
Priority date	Feb 19, 2015
Publication date	Dec 19, 2017
Grant date	Dec 19, 2017

Abstract

An improved rotor assembly configured for magnets with differing lengths, and methods and systems for manufacturing the same. The rotor assembly may be created by selectively creating first and second tabs extending into apertures of lamination sheets. The first and second tabs may be selectively removed, depending on the different magnet lengths and the specific lamination sheet, according to one of a first finishing schedule and a second finishing schedule. The lamination sheets are stacked with any remaining first and second tabs, and other features, aligned.

First claim

The invention claimed is:

1. A rotor assembly for an electric machine having a central axis, the rotor assembly comprising:
a plurality of standard lamination sheets;
at least one tab lamination sheet;
a plurality of recess lamination sheets, disposed opposite the tab lamination sheet from the standard lamination sheets;
wherein each of the standard lamination sheets, the tab lamination sheets, and the recess lamination sheets defines an aperture, and
wherein the plurality of lamination sheets are disposed adjacent each other to define a laminated stack, such that the apertures align to define a slot extending substantially parallel with the central axis;

a magnet disposed within the slot;
a first tab formed on the tab lamination sheet, wherein the first tab extends into the slot and into abutting engagement with a proximal surface of the magnet, such that the first tab biases a distal surface of the magnet against the slot to secure the magnet in position relative to the laminated stack;
a first recess groove defined in the recess lamination sheets axially adjacent to the first tab of the tab lamination sheet, wherein the first tab is at least partially disposed within the first recess groove; and
a second tab formed on the tab lamination sheet and extending substantially perpendicularly into the slot relative to the slot, wherein the second tab abuts an end of the magnet but does not bias the magnet against the slot, and wherein the recess lamination sheets do not define a groove adjacent the second tab.

2. A rotor assembly as set forth in claim 1 , wherein the second tab is formed on the standard lamination sheets and the on the recess lamination sheets, such that the second tabs are continuous throughout the slot.

3. A rotor assembly as set forth in claim 2 , further comprising:
a first stop formed on the standard lamination sheets, the tab lamination sheets, and the recess lamination sheets, and extending into the slot, such that the first stops are continuous throughout the slot, wherein the first stop is shorter than the first tab and the second tab.

4. A method of manufacturing rotor assemblies, comprising:
forming a plurality of standard lamination sheets, each having an aperture;
forming a plurality of tab lamination sheets, each having:
an aperture;
a first tab extending into the aperture; and
a second tab extending into the aperture;

forming a plurality of recess lamination sheets, each having:
an aperture;
a first tab extending into the aperture; and
a second tab extending into the aperture;

activating a first finishing schedule, including:
removing the first tabs of the recess lamination sheets and forming a first recess groove on the recess lamination sheets at the location of the first tabs; and
stacking the tab lamination sheets with the recess lamination sheets, such that the first tabs of the tab lamination sheets are axially aligned with the first recess grooves of the recess lamination sheets, and the second tabs of the tab lamination sheets are axially aligned with the second tabs of the recess lamination sheets; and

activating a second finishing schedule, including:
removing the first tabs of the recess lamination sheets and forming a first recess groove on the recess lamination sheets at the location of the first tabs;
removing the second tabs of the recess lamination sheets and forming a second recess groove on the recess lamination sheets at the location of the first tabs; and
stacking the tab lamination sheets with the recess lamination sheets, such that the first tabs of the tab lamination sheets are axially aligned with the first recess grooves of the recess lamination sheets, and the second tabs of the tab lamination sheets are axially aligned with the second recess grooves of the recess lamination sheets.

5. The method of claim 4 , further comprising:
inserting a short magnet after activating the first finishing schedule, such that the first tabs of the tab lamination sheets are deformed into the first recess groove of the recess lamination sheets.

6. The method of claim 5 , further comprising:
inserting a long magnet, which is at least twenty-five percent longer than the short magnet, after activating the second finishing schedule, such that the first tabs of the tab lamination sheets are deformed into the first recess groove of the recess lamination sheet and the second tabs of the tab lamination sheets are deformed into the second recess groove of the recess lamination sheet.

7. The method of claim 6 , further comprising:
forming a first stop on the standard lamination sheets, the tab lamination sheets, and the recess lamination sheets, such that the first stops are continuous throughout the slot, wherein the first stop is shorter than the first tabs and the second tabs.

8. The method of claim 7 , further comprising:
wherein forming the standard lamination sheets includes forming a first tab extending into the aperture and a second tab extending into the aperture;
wherein activating the first finishing schedule includes removing the first tabs of the standard lamination sheets; and
wherein activating the second finishing schedule includes removing the first tabs of the standard lamination sheets and removing the second tabs of the standard lamination sheets.

9. A system for producing a plurality of lamination sheets for a rotor assembly having a central axis, the system comprising:
an aperture punch configured to form an aperture in each of the lamination sheets;
a first tab punch configured to selectively form a first tab in the lamination sheets;
a first recess punch configured to selectively remove the first tab from the lamination sheets and to form a first recess in place of the first tab;
a second tab punch configured to selectively form a second tab in the lamination sheets;
a second recess punch configured to selectively remove the second tab from the lamination sheets and to form a second recess in place of the second tab; and
a stacking mechanism configured to axially align the selectively-formed first tabs and first recesses and to axially align the selectively-formed second tabs and second recesses,
wherein the first recess punch and the second recess punch are configured to operate on different schedules, such that the produced rotor assembly may have consecutive first tabs, intermittent first tabs and first recesses, consecutive second tabs, or intermittent second tabs and second recesses.

Assignees

• Gm Global Tech Operations Llc

Inventors

• Kaiser Edward L
• Savagian Peter J
• Rahman Khwaja M

Classifications

• H02K1/246

  Variable reluctance rotors · CPC title

• H02K15/03 Primary

  having permanent magnets · CPC title

• H02K1/2766

  having a flux concentration effect · CPC title