International Business Machines Corporation

Globalfoundries Inc.

Jean Labonte

Sylvain E Ouimet

Steven Paul Ostrander

Jon Alfred Casey

Sungjun Chun

Brian W Quinlan

Charles L Reynolds

Martin Beaumier

Pascale Gagnon

Stephanie Allard

Jean-Francois Drapeau

David Edward Turnbull

Jean-Francois Bachand

Denis Blanchard

Multicomponent module assembly by identifying a failed site on a laminate comprising a plurality of sites, adding a machine discernible mark associated with the failed site, placing an electrically good element at a successful site; and providing an MCM comprising the laminate, and the electrically good element.

Multicomponent module design and fabrication

A first and second antenna substrate are included in an advanced antenna package. Each antenna substrate includes a respective array of antenna elements disposed on a respective first surface of the substrate. A plurality of stand-off balls disposed between the first surfaces of first and second antenna substrates are bonded to the first surface of the first antenna substrate. A first sub-plurality of the stand-off balls are placed at positions in a peripheral region of the first and second antenna substrates. A second sub-plurality of the stand-off balls are placed at interior positions between antenna elements of the first and second antenna substrates. A plurality of adhesive pillars are disposed between and bond the first surfaces of first and second antenna substrates at a plurality of discrete selected locations. A first location of the discrete selected locations is in a peripheral region. A second location of the discrete selected locations is at an interior position between antenna elements.

Antenna packaging solution

A first and second antenna substrate are included in an advanced antenna package. Each antenna substrate includes a respective array of antenna elements disposed on a respective first surface of the substrate. A plurality of stand-off balls disposed between the first surfaces of first and second antenna substrates are bonded to the first surface of the first antenna substrate. A first sub-plurality of the stand-off balls are placed at positions in a peripheral region of the first and second antenna substrates. A second sub-plurality of the stand-off balls are placed at interior positions between antenna elements of the first and second antenna substrates. A plurality of adhesive pillars are disposed between and bond the first surfaces of first and second antenna substrates at a plurality of discrete selected locations. A first location of the discrete selected locations is in a peripheral region. A second location of the discrete selected locations is at an interior position between antenna elements. A method for fabricating the antenna package is also described.

A clamping apparatus and method for applying a force to a workpiece during processing includes a base defining a work area. The work area is configured to receive a joined structure including a substrate and a die. A component is positionable in the work area and over the joined structure. An adjustable releasable structure is positionable over the component and the joined structure and includes a resilient mechanism having an inner member for contacting the component to apply an inner downward force to the component. The resilient mechanism also includes outer members for applying an outer downward force to opposing distal edge areas of the substrate. An external downward force is applied to the adjustable releasable structure, such that the inner and outer members apply the inner and outer downward forces to the component and the opposing distal edge areas of the substrate, respectively, during processing of the joined structure.

Laminate peripheral clamping to control microelectronic module BSM warpage

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Cowansville, Canada

Jean Labonte