Abstract: A multijunction solar cell which includes: an upper first solar subcell having a first band gap; a second solar subcell adjacent to said upper first solar subcell and having a second band gap smaller than said first band gap; a third solar subcell adjacent to said second solar subcell and having a third band gap smaller than said second band gap; a graded interlayer adjacent to said third solar subcell, said graded interlayer having a fourth band gap greater than said third band gap; and a lower fourth solar subcell adjacent to said graded interlayer, said lower fourth solar subcell having a fifth band gap smaller than said third band gap such that said lower fourth solar subcell is lattice mismatched with respect to said third solar subcell.
Abstract: A method of forming a multijunction solar cell including an upper subcell, a middle subcell, and a lower subcell by providing a substrate for the epitaxial growth of semiconductor material; forming a first solar subcell on the substrate having a first band gap; forming a second solar subcell over the first solar subcell having a second band gap smaller than the first band gap; forming a graded interlayer over the second subcell, the graded interlayer having a third band gap greater than the second band gap; forming a third solar subcell over the graded interlayer having a fourth band gap smaller than the second band gap such that the third subcell is lattice mismatched with respect to the second subcell; and forming a contact composed of a sequence of layers over the first subcell at a temperature of 280° C. or less and having a contact resistance of less than 5×10?4 ohms-cm2.
Abstract: A multijunction solar cell which includes: an upper first solar subcell having a first band gap; a second solar subcell adjacent to said upper first solar subcell and having a second band gap smaller than said first band gap; a third solar subcell adjacent to said second solar subcell and having a third band gap smaller than said second band gap; a graded interlayer adjacent to said third solar subcell, said graded interlayer having a fourth band gap greater than said third band gap; and at least a fourth solar subcell adjacent to said graded interlayer, said fourth solar subcell having a fifth band gap smaller than said third band gap such that said lower fourth solar subcell is lattice mismatched with respect to said third solar subcell.
Abstract: A method of bonding solar cell component to a support and the solar cell assembly thus obtained. The method of bonding solar cell component to a support comprises: disposing metallized traces on the support; dispensing bonding adhesive on front of the support or on back of the solar cell component; and laying down the solar cell component on the support and soldering the solar cell component to the metallized traces on the support. The support is a glass support with integrated circuits.
Abstract: 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.
Type:
Application
Filed:
August 19, 2016
Publication date:
January 12, 2017
Applicant:
SolAero Technologies Corp.
Inventors:
Marvin B. Clevenger, Cory Tourino, Benjamin Richards
Abstract: Solar cells are obtained by singulating a non-rectangular solar cell wafer into a plurality of solar cells, in one embodiment a first solar cell having a surface area corresponding to at least 60% of the wafer surface area but less than 90% of the wafer surface area, and at least two second solar cells each having a surface area of less than 10% of the wafer surface area. Such a first solar cell can be connected in parallel with a plurality of the second solar cells, to establish a substantially rectangular subassembly, and such subassemblies can be combined into a larger solar cell assembly, which may be mounted on a support including other electrical components on the backside thereof, and attached to a small satellite (e.g., CubeSat) exterior surface, or deployable wing.
Abstract: A multijunction solar cell assembly which includes a first semiconductor body including: an upper first solar subcell having a first band gap; a second solar subcell adjacent to said upper first solar subcell and having a second band gap smaller than said first band gap; a third solar subcell adjacent to said second solar subcell and having a third band gap smaller than said second band gap; a graded interlayer adjacent to said third solar subcell, said graded interlayer having a fourth band gap greater than said third band gap; and a lower fourth solar subcell adjacent to said graded interlayer, said lower fourth solar subcell having a fifth band gap smaller than said third band gap such that said lower fourth solar subcell is lattice mismatched with respect to said third solar subcell, and a second semiconductor body adjacent to and aligned with the first semiconductor body so that light passes through the first semiconductor body into the second semiconductor body.
Abstract: A solar cell assembly including: a solar cell for generating electric power from sunlight; a cover glass for covering the solar cell; transparent shims, which are disposed between the solar cell and the cover glass at the points were the distance between the solar cell and the cover glass needs to be controlled, and form a space between the solar cell and the cover glass; and a transparent adhesive layer, which fills the space between the solar cell and the cover glass and has the thickness the same as that of the transparent shims.
Type:
Grant
Filed:
May 24, 2016
Date of Patent:
October 18, 2016
Assignee:
SolAero Technologies Corp.
Inventors:
Benjamin C Richards, Charles F Sarver, Maria Naidenkova
Abstract: A solar cell assembly including: a solar cell for generating electric power from sunlight; a cover glass for covering the solar cell; transparent shims, which are disposed between the solar cell and the cover glass at the points were the distance between the solar cell and the cover glass needs to be controlled, and form a space between the solar cell and the cover glass; and a transparent adhesive layer, which fills the space between the solar cell and the cover glass and has the thickness the same as that of the transparent shims.
Type:
Application
Filed:
May 24, 2016
Publication date:
September 15, 2016
Applicant:
SolAero Technologies Corp.
Inventors:
Benjamin C. Richards, Charles F. Sarver, Maria Naidenkova
Abstract: According to an aspect of an embodiment of the present disclosure, there is provided a solar cell panel and a method for manufacturing the same. The solar cell panel comprises: a solar cell for generating electric power from sunlight; a coverglass for covering the solar cell; transparent shims, which are disposed between the solar cell and the coverglass at the points where the distance between the solar cell and the coverglass needs to be controlled, and form a space between the solar cell and the coverglass; and adhesive layer, which fills the space between the solar cell and the coverglass and has the thickness the same as that of the transparent shims.
Type:
Grant
Filed:
March 25, 2014
Date of Patent:
June 28, 2016
Assignee:
SolAero Technologies Corp.
Inventors:
Benjamin C. Richards, Charles F. Sarver, Maria Naidenkova