Microfabrica Inc.

Pavel B Lembrikov

Dennis R Smalley

Richard T Chen

Christopher A Bang

Ezekiel J J Kruglick

Michael S Lockard

Uri Frodis

Adam L Cohen

Arun S Veeramani

Heath A Jensen

Christopher G Wiita

Irina Boguslavsky

Vacit Arat

Ezekiel Kruglick

Ananda H Kumar

Gang Zhang

Kieun Kim

Jeffrey A Thompson

Embodiments are directed to the formation micro-scale or millimeter scale structures or methods of making such structures wherein the structures are formed from at least one sheet structural material and may include additional sheet structural materials or deposited structural materials wherein all or a portion of the patterning of the structural materials occurs via laser cutting. In some embodiments, selective deposition is used to provide a portion of the patterning. In some embodiments the structural material or structural materials are bounded from below by a sacrificial bridging material (e.g. a metal) and possibly from above by a sacrificial capping material (e.g. a metal).

Methods of forming parts using laser machining

Embodiments disclosed herein are directed to compliant probe structures for making temporary or permanent contact with electronic circuits and the like. In particular, embodiments are directed to various designs of cantilever-like probe structures. Some embodiments are directed to methods for fabricating such probe or cantilever structures. In some embodiments, for example, cantilever probes have extended base structures, slide in mounting structures, multi-beam configurations, offset bonding locations to allow closer positioning of adjacent probes, compliant elements with tensional configurations, improved over travel, improved compliance, improved scrubbing capability, and/or the like.

Cantilever microprobes for contacting electronic components

Embodiments are directed to the formation micro-scale or millimeter scale structures or method of making such structures wherein the structures are formed from at least one sheet structural material and may include additional sheet structural materials or deposited structural materials wherein all or a portion of the patterning of the structural materials occurs via laser cutting. In some embodiments, selective deposition is used to provide a portion of the patterning. In some embodiments the structural material or structural materials are bounded from below by a sacrificial bridging material (e.g. a metal) and possibly from above by a sacrificial capping material (e.g. a metal).

Embodiments disclosed herein are directed to compliant probe structures for making temporary or permanent contact with electronic circuits and the like. Some embodiments are directed to various designs of cantilever-like probe structures while other embodiments are directed to methods for fabricating probe structures. In some embodiments, methods are used to form probe structures from a plurality of planar multi-material layers wherein each probe structure includes a contact tip and a compliant body wherein a portion of the complaint body is formed, then the contact tip is formed and then finally the rest of the compliant body is formed, wherein the compliant body provides for elastic compression of the probe in a plane of primary motion during use and wherein during formation of the layers a stacking direction of the plurality of layers is perpendicular to the plane of primary motion.

Methods of creating probe structures from a plurality of planar layers

Embodiments disclosed herein are directed to compliant probe structures for making temporary or permanent contact with electronic circuits and the like. Some embodiments are directed to various designs of cantilever-like probe structures while other embodiments are directed to methods for fabricating probe structures. In some embodiments, methods are used to form probe structures from a plurality of planar multi-material layers wherein each probe structure includes a contact tip, a compliant body, and a bonding material that can be used in bonding the probe to a substrate and wherein the compliant body provides for elastic compression of the probe in a plane of primary motion during use and wherein during formation of the layers a stacking direction of the plurality of layers is perpendicular to the plane of primary motion.

Embodiments disclosed herein are directed to compliant probe structures for making temporary or permanent contact with electronic circuits and the like. Some embodiments are directed to various designs of cantilever-like probe structures while other embodiments are directed to methods for fabricating probe structures. In some embodiments, methods of forming probe structures include formation of a plurality of planar multi-material electrodeposited layers wherein each probe structure includes a contact tip and a compliant body, wherein the compliant body is formed from at least one material that is different from the contact tip material and wherein the compliant body provides for elastic compression of the probe in a plane of primary motion during use and wherein during formation of the layers a stacking direction of the plurality of layers is perpendicular to the plane of primary motion.

Embodiments disclosed herein are directed to compliant probe structures for making temporary or permanent contact with electronic circuits and the like. In particular, embodiments are directed to various designs of cantilever-like probe structures. Some embodiments are directed to methods for fabricating such cantilever structures. In some embodiments, methods are used to form probe structures from a plurality of planar multi-material layers wherein the probe structures include a contact tip and a compliant body with the compliant body formed from at least one material that is different from the tip material and wherein compliant body provides for elastic compression of the probe in a plane of primary motion during use and wherein during formation a stacking direction of the plurality of layers is perpendicular to the plane of primary motion.

Probe devices formed from multiple planar layers of structural material with tip regions formed from one or more intermediate planar layers

Embodiments of invention are directed to the formation of microprobes (i.e. compliant electrical or electronic contact elements) on a temporary substrate, dicing individual probe arrays, and then transferring the arrays to space transformers or other permanent substrates. Some embodiments of the invention transfer probes to permanent substrates prior to separating the probes from a temporary substrate on which the probes were formed while other embodiments do the opposite. Some embodiments, remove sacrificial material prior to transfer while other embodiments remove sacrificial material after transfer. Some embodiments are directed to the bonding of first and second electric components together using one or more solder bumps with enhanced aspect ratios (i.e. height to width ratios) obtained as a result of surrounding the bumps at least in part with rings of a retention material. The retention material may act be a solder mask material.

Probe arrays and method for making

Embodiments disclosed herein are directed to compliant probe structures for making temporary or permanent contact with electronic circuits and the like. In particular, embodiments are directed to various designs of cantilever-like probe structures. Some embodiments are directed to methods for fabricating such cantilever structures. In some embodiments, for example, cantilever probes have extended base structures, slide in mounting structures, multi-beam configurations, offset bonding locations to allow closer positioning of adjacent probes, compliant elements with tensional configurations, improved over travel, improved compliance, improved scrubbing capability, and/or the like.

Cantilever microprobes for contacting electronic components and methods for making such probes

Embodiments of the invention provide fabrication processes for the co-fabrication of microprobe arrays along with one or more space transformers wherein the fabrication processes include the forming and adhering of a plurality of layers to previously formed layers and wherein at least a portion of the plurality of layers are formed from at least one structural material and at least one sacrificial material that is at least in part released from the plurality of layers after formation and wherein the space transformer includes a plurality of interconnect elements that connect one side to the array of probes that has a first spacing to another side that has a second spacing where the second spacing is greater than the first spacing. In some embodiments, the fabrication process includes a plurality of electrodeposition operations.

Fabrication process for co-fabricating multilayer probe array and a space transformer

Multi-layer structures are electrochemically formed on porous dielectric substrates. In some embodiments, the substrates have at least one surface which is infiltrated with a sacrificial conductive material, all pores (e.g. openings in between dielectric regions of the substrate) or selected pores near the surface of the substrate are opened, and a structural material is deposited to fill at least a portion of the opened pores. If more pores are opened than have been filled or will be filled by the structural material a sacrificial material may be deposited to fill the additional pores. After completing formation of an initial patterned surface on the substrate, a plurality of layers are formed on the substrate (e.g. via electrodeposition operations) and after layer formation is complete, the conductive sacrificial material filling the pores is removed.

Growing community of inventors

Santa Monica, CA, United States of America

Pavel B Lembrikov