Abstract:
Systems and methods are presented including solar cells or solar sheets having textured coversheets that provide increased light collection efficiency. Some embodiments include a textured solar coversheet configured for installation on a surface of a space-based vehicle or on a surface of a component of a space-based vehicle. The textured solar sheet includes a plurality of solar cells, a polymer coversheet to which the plurality of solar cells are attached, and an ultraviolet rejection film disposed over the polymer coversheet.
Abstract:
Some embodiments include a kit for increasing endurance of a battery-powered unmanned aerial vehicle (UAV) by incorporating flexible solar cells or applying flexible solar cells on a surface of a UAV or on a surface of a component of a UAV. The kit further include a power conditioning system configured to operate the solar cells within a desired power range and configured to provide power having a voltage compatible with an electrical system of the UAV.
Abstract:
Some embodiments include a high efficiency, lightweight solar sheet. Some embodiments include a solar sheet configured for installation on a surface of a UAV or on a surface of a component of a UAV. The solar sheet includes a plurality of solar cells and a polymer layer to which the plurality of solar cells are attached. Some embodiments include a kit for supplying solar power in a battery-powered or fuel cell powered unmanned aerial vehicle (UAV) by incorporating flexible solar cells into a component of a UAV, affixing flexible solar cells to a surface of a UAV, or affixing flexible solar cells to a surface of a component of a UAV. The kit also includes a power conditioning system configured to operate the solar cells within a desired power range and configured to provide power having a voltage compatible with an electrical system of the UAV.
Abstract:
Some embodiments include a high efficiency, lightweight solar sheet. Some embodiments include a solar sheet configured for installation on a surface of a UAV or on a surface of a component of a UAV. The solar sheet includes a plurality of solar cells and a polymer layer to which the plurality of solar cells are attached. Some embodiments include a kit for supplying solar power in a battery-powered or fuel cell powered unmanned aerial vehicle (UAV) by incorporating flexible solar cells into a component of a UAV, affixing flexible solar cells to a surface of a UAV, or affixing flexible solar cells to a surface of a component of a UAV. The kit also includes a power conditioning system configured to operate the solar cells within a desired power range and configured to provide power having a voltage compatible with an electrical system of the UAV.
Abstract:
Some embodiments include a high efficiency, lightweight solar sheet. Some embodiments include a solar sheet configured for installation on a surface of a UAV or on a surface of a component of a UAV. The solar sheet includes a plurality of solar cells and a polymer layer to which the plurality of solar cells are attached. Some embodiments include a kit for supplying solar power in a battery-powered or fuel cell powered unmanned aerial vehicle (UAV) by incorporating flexible solar cells into a component of a UAV, affixing flexible solar cells to a surface of a UAV, or affixing flexible solar cells to a surface of a component of a UAV. The kit also includes a power conditioning system configured to operate the solar cells within a desired power range and configured to provide power having a voltage compatible with an electrical system of the UAV.
Abstract:
An assembly technique for assembling solar cell arrays is provided. During the fabrication of a solar cell, openings through the semiconductor layer are etched through to a top surface of the backmetal layer. The solar cells include an exposed top surface of the backmetal layer. A plurality of solar cells are assembled into a solar cell array where adjacent cells are interconnected in an electrically serial or parallel fashion solely from the top surface of the solar cells.
Abstract:
Described herein are optoelectronic devices and methods incorporating strain balanced direct bandgap AlxIn1-xP multiple quantum wells. The described devices are strain balanced in that the net strain between the ordered quantum wells and barriers is low, or in some cases zero. Advantageously, the described devices may be specifically designed for higher efficiency than existing AlxIn1-xP and may be grown on commercially available GaAs substrates.
Abstract:
Methods and systems for forming a device structure free of a substrate are described. Exemplary embodiments include a device structure comprising of device layers, a release layer, an etch stop layer, and a substrate. The device structure is exposed to photoenhanced wet etch environments to vertically and laterally etch the release layer to separate the device layers from the substrate. The device structure can include a contact layer, an etch stop layer, or both in some embodiments.
Abstract:
Some embodiments include a kit for supplying solar power in a battery-powered or fuel cell powered unmanned aerial vehicle (UAV) by incorporating flexible solar cells into a component of a UAV, affixing flexible solar cells to a surface of a UAV, or affixing flexible solar cells to a surface of a component of a UAV. The kit also includes a power conditioning system configured to operate the solar cells within a desired power range and configured to provide power having a voltage compatible with an electrical system of the UAV. Another embodiments include a solar sheet configured for installation on a surface of a UAV or on a surface of a component of a UAV. The solar sheet includes a plurality of solar cells and a polymer layer to which the plurality of solar cells are attached.
Abstract:
The method of the invention includes the sequential steps of providing a plurality of solar cells, interconnecting the solar cells using one or more interconnect tabs, attaching the interconnect tabs to a top side of the solar cell to interconnect the plurality of solar cells by coupling an exposed top surface of a first solar cell to a top surface of an adjacent second solar cell, attaching one or more bypass diodes to a top side of the solar cell, then next applying an adhesive to a first film layer, placing the plurality of solar cells onto the first film layer, then next applying an adhesive to a second film layer, placing the plurality of solar cells and first film layer onto the second film layer to form a sheet assembly, and then forming the solar sheet from the sheet assembly.