Method and apparatus for shaping spring elements

• US 6,836,962 B2
• Filed: 12/29/2000
• Issued: 01/04/2005
• Est. Priority Date: 11/16/1993
• Status: Expired due to Fees

• Current Assignee: FormFactor Incorporated
• Original Assignee: FormFactor Incorporated
• Inventors: Mathieu, Gaetan L., Khandros, Igor Y., Dozier, Thomas H., Grube, Gary W.
• Primary Examiner(s): Arbes, Carl J.
• Application Number:
  US09/753,188
• Publication Number:
  US 20010038030A1
• Time in Patent Office: 1,467 Days
• Field of Search: 295/93, 298/25, 298/42, 298/43, 298/54, 298/76, 298/78, 298/79
• US Class Current: 29/844
• CPC Class Codes: B21D 39/00 Application of procedures in order to connect objects or parts, e.g. coating with sheet metal otherwise than by plating joining mitred profiles B21D53/745; riveting B21J; uniting components by forging or pressing to form integral members B21K25/00; welding B23K; press-fitting, force-fitting, or shrinking in general B23P11/00, B21D19/00; by adhesives F16B11/00 ; Connections as such F16L, F16B; Tube expanders
• CPC Class Codes: B23K 31/02 relating to soldering or welding dip or wave soldering in the manufacture of printed circuits H05K3/34
• CPC Class Codes: H01R 9/00 Structural associations of a plurality of mutually-insulated electrical connecting elements, e.g. terminal strips or terminal blocks; Terminals or binding posts mounted upon a base or in a case; Bases therefor
• CPC Class Codes: Y10T 29/49147 Assembling terminal to base
• CPC Class Codes: Y10T 29/49149 by metal fusion bonding
• CPC Class Codes: Y10T 29/49151 by deforming or shaping
• CPC Class Codes: Y10T 29/49208 by assembling plural parts
• CPC Class Codes: Y10T 29/49211 of fused material
• CPC Class Codes: Y10T 29/49213 Metal

Abstract

Interconnection elements for electronic components, exhibiting desirable mechanical characteristic (such as resiliency, for making pressure contacts) are formed by using a shaping tool (512) to shape an elongate core element (502) of a soft material (such as gold or soft copper wire) to have a springable shape (including cantilever beam, S-shape, U-shape), and overcoating the shaped core element with a hard material (such as nickel and its alloys), to impart to desired spring (resilient) characteristic to the resulting composite interconnection element. A final overcoat of a material having superior electrical qualities (e.g., electrical conductivity and/or solderability) may be applied to the composite interconnection element. The resulting interconnection elements may be mounted to a variety of electronic components, including directly to semiconductor dies and wafers (in which case the overcoat material anchors the composite interconnection element to a terminal (or the like) on the electronic component), may be mounted to support substrates for use as interposers and may be mounted to substrates for use as probe cards or probe card inserts. The shaping tool may be an anvil (622) and a die (624), and may nick or sever successive shaped portions of the elongate elements, and the elongate element may be of an inherently hard (springy) material. Methods of fabricating interconnection elements on sacrificial substrates are described. Methods of fabricating tip structures (258) and contact tips at the end of interconnection elements are also described.

Claims

1. Method of mounting an interconnection element to a substrate, comprising:

attaching an elongate element of a first material to a substrate;

shaping the elongate element with a shaping tool; and

overcoating the elongate element with a second material which has a higher yield strength than the first material, in an amount sufficient for imparting a desired resiliency to the interconnection element, whereby the interconnection element after the overcoating step is substantially stiffer than the elongate element prior to the overcoating step.

2. The method of claim 1, wherein the substrate is an electronic component, and the elongate element is attached to a terminal of the electronic component.

3. The method of claim 1, wherein the substrate comprises a lithographically defined part.

4. The method of claim 3, wherein the elongate element is attached to the lithographically defined part.

5. Method, according to claim 2, further comprising:

while overcoating the elongate element, overcoating at least a portion of an exposed surface of the terminal with the second material.