Solaero Technologies Corp.

Emcore Solar Power, Inc.

Solaero Technololes Corp.

Solacro Technologies Corp.

Cory Tourino

Benjamin C Richards

Marvin Brad Clevenger

Kenneth Craymer

Daniel Derkacs

Daniel James Aiken

Lei Yang

Philip E Blumenfeld

Anthony Sandoval

Brian Guzie

Dwight Hazlett

Benjamin Cho

Marvin Bradford Clevenger

A method of fabricating a solar cell array module comprising providing a support, providing a face sheet having a top side and an opposite bottom side, mounting the bottom side of the face sheet on the support, providing a pattern of discrete predefined adhesive regions in an automated manner on the top side of the face sheet using machine vision and mounting an array of solar cell assemblies on the adhesive regions in an automated manner on the top side of the face sheet.

Automated assembly and mounting of solar cells on a honeycomb support

A method of fabricating a multijunction solar cell panel by providing a plurality of multijunction solar cells; dispensing out uncured silicone coating on the solar cells using an automated process with visual recognition, and curing the silicone coating on the solar cell to complete the Cell-Interconnect-Cover Glass (CIC) assembly.

Automated assembly and mounting of solar cells on space panels

The present disclosure provides interconnect elements and methods of using interconnect elements. In one embodiment, the interconnect element includes: a first end including at least three members, each member having a pair of parallel gap weld positions for mounting an adjoining first component; a second opposing end including at least two members, each member having a pair of parallel gap weld positions for mounting an adjoining second component; and one or more interconnect connecting portions to attach the first end of the interconnect element to the second end of the interconnect element.

Reliable interconnection of solar cells

The present disclosure provides methods of fabricating a multijunction solar cell panel in which one or more of the steps are performed using an automated process. In some embodiments, the automated process uses machine vision.

The present disclosure provides interconnect elements and methods of using interconnect elements. In one embodiment, the interconnect element includes: a first end including at least three members, each member having a pair of parallel gap apertures for mounting an adjoining first component; a second opposing end including at least two members, each member having a pair of parallel gap apertures for mounting an adjoining second component; and one or more interconnect connecting portions to attach the first end of the interconnect element to the second end of the interconnect element.

Solar cell array assemblies or modules mounted on a space vehicle having discrete predefined pressure sensitive adhesive (PSA) regions thereon. In certain embodiments, the solar cell array modules may be conveniently mounted on the surface of a panel of a space vehicle or satellite with the discrete predefined PSA regions sized and shaped to match portions of the panel.

Assembly and mounting of solar cells on space vehicles or satellites

Solar cell array assemblies or modules and methods of making and using such solar cell array assemblies or modules, having discrete predefined pressure sensitive adhesive (PSA) regions thereon. In certain embodiments, the solar cell array modules may be conveniently mounted on the surface of a panel of a space vehicle or satellite with the discrete predefined PSA regions.

A flexible solar array for a spacecraft or aviation craft including a flexible backing substrate with conductive trace(s) formed thereon; solar cell subassemblies disposed over the flexible backing substrate, each of the solar cell subassemblies at least including a solar cell; and an adhesive layer interposed between the solar cell subassemblies and the flexible backing substrate, with the solar cell attached to the flexible backing substrate. The adhesive layer includes openings for exposing the corresponding conductive traces so that the exposed metal traces are adaptable to interconnect the solar cells of the respective adjacent solar cell subassemblies through the openings.

Flexible solar array

A flexible solar array and a method for fabricating the same is provided. The flexible solar array may include a flexible backing substrate with conductive trace(s) formed thereon; solar cell subassemblies over the flexible backing substrate, each of the solar cell subassemblies at least including a solar cell; and an adhesive layer interposed between the solar cell subassemblies and the flexible backing substrate, and attaching the solar cells to the flexible backing substrate. The adhesive layer includes openings for exposing the corresponding conductive traces so that the exposed metal traces are adaptable to interconnect the solar cells of the respective adjacent solar cell subassemblies through the openings.

Flexible solar array and method for fabricating the same

The present disclosure provides a solar cell array for deployment and use in a space environment, and methods of making same. The array includes a plurality of solar cells having an emissivity coating on the baskside of each, with each coated solar cell being attached to a supporting member.

Emissivity coating for space solar cell arrays

Metal interconnecting member for solar cells

A solar cell assembly and a method of bonding a solar cell component to a flexible support are disclosed. The solar cell assembly comprises a flexible support with a predetermined size, a solar cell component, bonding adhesive between the support and the solar cell component, wherein the support with the predetermined size has substantially uniform borders of 0.003 inches to 0.2 inches in width extending beyond the edges of the solar cell component.

Growing community of inventors

Edgewood, NM, United States of America

Cory Tourino