Apparatus and methods for filament crimping and manufacturing

• US 8,113,243 B2
• Filed: 07/01/2010
• Issued: 02/14/2012
• Est. Priority Date: 06/22/2006
• Status: Active Grant

• Current Assignee: Autosplice, Inc. (Autosplice Parent, Inc.)
• Original Assignee: Autosplice, Inc. (Autosplice Parent, Inc.)
• Inventors: Bogursky, Robert, Foshansky, Leonid, Kennedy, Craig, Wood, Darrel, Saunders, Mark
• Primary Examiner(s): EKIERT, TERESA M
• Application Number:
  US12/829,208
• Publication Number:
  US 20110000577A1
• Time in Patent Office: 593 Days
• Field of Search: 140/105, 140/106, 723/06, 723/07, 72381-384
• US Class Current: 140/105
• CPC Class Codes: H01R 4/01 Connections using shape memory materials, e.g. shape memory metal
• CPC Class Codes: H01R 4/188 having an uneven wire-receiving surface to improve the contact
• CPC Class Codes: H01R 43/048 Crimping apparatus or processes H01R43/042 takes precedence
• CPC Class Codes: Y10T 29/49181 by deforming
• CPC Class Codes: Y10T 29/49204 Contact or terminal manufacturing
• CPC Class Codes: Y10T 29/5121 Wire working
• CPC Class Codes: Y10T 428/1241 Nonplanar uniform thickness or nonlinear uniform diameter [e.g., L-shape]

Abstract

Apparatus and methods for filament crimping. In one embodiment, the apparatus comprises a body and a filament crimp element. The filament crimp element comprises a first set of cavities disposed at a spacing which creates a first set of features and a second set of cavities disposed at a spacing which creates a second set of features. The first and second set cavities are substantially opposite one another. The first set of features are adapted to be placed at least partially within the second set of cavities and the second set of features are adapted to be placed at least partially within the first set of cavities. Methods and apparatus for the manufacture of the device are also disclosed. In addition, methods for automated placement and manufacture of assemblies using the crimp elements are also disclosed.

Claims

1. A method of manufacturing a crimping assembly comprising a crimping element and a crimped filament, comprising:

pre-forming said crimping element prior to crimping so as to provide a gap, said pre-formed crimping element comprised of;

a first plurality of cavities, said first plurality of cavities disposed so as to at least partly define a first plurality of features; and

a second plurality of cavities, said second plurality of cavities disposed so as to at least partly define a second plurality of features;

disposing a filament at least partly within said gap and adjacent at least a portion of said first and second plurality of cavities;

placing said filament under tension; and

crimping said crimping element after placing said filament under tension so as to fixedly secure said filament to said crimping element.

2. The method of claim 1, further comprising:

feeding said crimping element into a crimping machine along a given feed direction;

wherein said given feed direction is substantially parallel with said disposed filament.

3. The method of claim 1, wherein said act of crimping causes said first and second pluralities of cavities and features to form a substantially serpentine channel therebetween for said filament.

4. The method of claim 3, wherein when said act of crimping causes a part of said first plurality of features to be received within said second plurality of cavities, and a part of said second plurality of features to be received within said first plurality of cavities, thereby forming said substantially serpentine channel.

5. The method of claim 1, wherein said crimping element is formed from a material which has a hardness less than that of said filament, said lesser hardness of said material at least mitigating deleterious material deformation of said filament by said crimping element during the act of crimping.

6. The method of claim 5, wherein said first features are substantially juxtaposed and coplanar with one another in a first plane, and said second features are substantially juxtaposed and coplanar with one another in a second plane.

7. The method of claim 6, wherein said first and second features each comprise substantially rounded edges, said substantially rounded edges mitigating deleterious material deformation of at least a portion of said filament during crimping.

8. The method of claim 6, wherein said first and second features each comprise filament engagement surfaces having substantially rounded profiles, said substantially rounded profiles mitigating cutting of said filament during crimping.

9. The method of claim 1, wherein said act of placing said filament under tension comprises placing said filament under 15-30 grams-force of tension.