Method of rotor assembly without the hub

• US 7,546,674 B2
• Filed: 10/31/2005
• Issued: 06/16/2009
• Est. Priority Date: 10/31/2005
• Status: Expired due to Fees

• Current Assignee: GM Global Technology Operations LLC (General Motors Company)
• Original Assignee: GM Global Technology Operations Incorporated (Motors Liquidation Co. GUC Trust)
• Inventors: Erfanfar, Mohsen M.
• Primary Examiner(s): TRINH, MINH N
• Application Number:
  US11/263,177
• Publication Number:
  US 20070096584A1
• Time in Patent Office: 1,324 Days
• Field of Search: 29596-598, 297/32, 296/09, 310/216, 310/231, 310/259, 310/269, 164108-110, 164/113
• US Class Current: 29/598
• CPC Class Codes: H02K 1/26 Rotor cores with slots for windings
• CPC Class Codes: H02K 1/30 using intermediate parts, e.g. spiders
• CPC Class Codes: H02K 15/028 for fastening to casing or support, respectively to shaft or hub
• CPC Class Codes: Y10T 29/49012 Rotor

Abstract

A method of assembling a rotor assembly is provided, without the use of a rotor steel hub. The method comprises forming first, second and third lamination stacks by stacking individual rotor laminations together. The first, second and third lamination stacks are cast to lock the individual rotor laminations together. The rotor laminations in the first, second and third lamination stacks have a generally ring-like shape with a variable inner diameter and a substantially common outer diameter. The rotor laminations in the first, second and third lamination stacks have substantially the same outer diameter, whereas the rotor laminations in the second lamination stack have a substantially larger inner diameter than the first and third rotor laminations. The elimination of the hub results in reducing total cost and manufacturing cycle time, and in improved features, performance and efficiency of the rotor assembly.

Claims

1. A method of rotor assembly without a hub comprising:

stacking first rotor laminations sufficiently to form a first lamination stack having an inner diameter of substantially one predetermined size, said first lamination stack having a first end and a second end;

stacking second rotor laminations sufficiently onto said second end of said first lamination stack to form a second lamination stack having an inner diameter of substantially another predetermined size to facilitate the attachment of the rotor assembly without a hub, said second lamination stack having a first end and a second end;

wherein there is no central shaft extending through a center of said rotor assembly to aid construction of the rotor assembly;

stacking third rotor laminations sufficiently onto said second end of said second lamination stack to form a third lamination stack having an inner diameter of said one predetermined size;

wherein said first, second and third rotor laminations have a shape with substantially the same outer diameter; and

wherein said second rotor laminations have a larger inner diameter than said first and third rotor laminations.

2. The method of claim 1 including placing said first and second and third lamination stacks into a casting mold;

and compressing said lamination stacks.

3. The method of claim 1, wherein said shape of said first, second and third rotor laminations is a ring shape, having an outer and inner circumference.

4. The method of claim 3, wherein slots extend along a periphery of said outer circumference of said first, second and third rotor laminations.

5. The method of claim 4, further comprising:

injecting molten metal into said slots extending along said periphery of said outer circumference of said first, second and third rotor laminations, wherein said molten metal is injected from said first end of said first lamination stack to said second end of said third lamination stack; and

applying hydraulic back pressure against said molten metal to avoid air gaps, bubbles or porosity inside said first, second and third lamination stacks.

6. The method of claim 5:

wherein said molten metal solidifies at said first end of said first lamination stack to create a first metal end ring; and

wherein said molten metal through said slots solidifies at said second end of said third lamination stack to create a second metal end ring on an opposite end of said assembly.

7. A method of rotor assembly without a hub comprising:

stacking first rotor laminations sufficiently to form a first lamination stack having an inner diameter of substantially one predetermined size, said first lamination stack having a first end and a second end;

stacking second rotor laminations sufficiently onto said second end of said first lamination stack to form a second lamination stack having an inner diameter of substantially another predetermined size to facilitate the attachment of the rotor assembly without a hub, said second lamination stack having a first end and a second end;

stacking third rotor laminations sufficiently onto said second end of said second lamination stack to form a third lamination stack having an inner diameter of said one predetermined size, said third lamination stack having a first end and a second end;

wherein there is no central shaft extending through a center of said rotor assembly to aid construction of the rotor assembly;

wherein said first, second and third rotor laminations have a shape with substantially the same outer diameter;

wherein said second rotor laminations have a larger inner diameter than said first and third rotor laminations;

wherein said shape of said first, second and third rotor laminations is a ring shape, having an outer and inner circumference;

forming a first bolt hole along a periphery of said inner circumference of said first rotor laminations, said first bolt hole extending from said first end of said first lamination stack to said second end of said first lamination stack;

forming a second bolt hole along a periphery of said inner circumference of said third rotor laminations, said second bolt hole extending from said first end of said third lamination stack to said second end of said third lamination stack; and

wherein no bolt holes are formed through said second rotor laminations.

8. The method of claim 7, further comprising:

attaching a first bolt through said first lamination stack through said first bolt hole, said first bolt including first serrations configured to engage with complementary serrations inside said first bolt hole; and

attaching a second bolt through said third lamination stack through said second bolt hole, said second bolt including second serrations configured to engage with complementary serrations inside said second bolt hole.

9. The method of claim 8, wherein:

said first bolt includes a flat side positioned at said second end of said first lamination stack to lock said first bolt in said first lamination stack; and

said second bolt includes a flat side positioned at said first end of said third lamination stack to lock said second bolt in said third lamination stack.

10. The method of claim 8, further comprising:

attaching a first flange onto said first end of said first lamination stack, said first bolt going through a first flange hole formed in said first flange to orient said first flange;

attaching a second flange onto said second end of said third lamination stack, said second bolt going through a second flange hole formed in said second flange to orient said second flange; and

wherein said first and said second flange transmit power from said rotor assembly.

11. The method of claim 8, further comprising:

placing said first and second and third lamination stacks into a casting mold;

compressing said lamination stacks sufficiently to lock all laminations together;

injecting molten metal into slots extending along a periphery of said outer circumference of said first, second and third rotor laminations, wherein said molten metal is injected from said first end of said first lamination stack to said second end of said third lamination stack; and

applying hydraulic back pressure against said molten metal to avoid air gaps, bubbles or porosity inside said first, second and third lamination stacks.

12. The method of claim 11, wherein:

said molten metal solidifies at said first end of said first lamination stack to create a first metal end ring; and

said molten metal through said slots solidifies at said second end of said third lamination stack to create a second metal end ring on an opposite end of said assembly.