A solar array structure for a spacecraft includes one or a pair of flexible blanket or other foldable solar arrays (such as flexible panels) and a deployable frame structure. The deployable frame structure includes a T-shaped yoke structure, a T-shaped end structure, and one or more rigid beams, the T-shaped yoke structure connectable to the spacecraft. When deployed, the frame structure tensions the flexible blanket solar array or arrays between the T-shaped yoke structure and the T-shaped end structure. When stowed, the flexible blanket solar array or arrays are folded in an accordion manner to form a stowed pack or packs between the cross-member arms of the T-shaped yoke structure and the T-shaped end structure, also stowed in its own Z-fold arrangement. The cross-member arms of the T-shaped end structure can include a solar array that can provide power before deployment while the flexible blanket solar array is stowed.

A deflection pad may include a body including two peaks, and a recess in the body between the two peaks, the recess may be sized to accommodate a fastener such that when deployed, the fastener is below a height of the two peaks within the recess. The deflection pad may include arms projecting in a direction generally opposite the two peaks, the arms biased inward towards the recess. The deflection pad may be included in a system that includes a torsion beam and one or more support racks to which multiple PV modules may be attached, where the support are racks attached to the torsion beam. One or more deflection pads may be positioned on the support racks to be below the PV modules.

Solar trackers that may be advantageously employed on sloped and/or variable terrain to rotate solar panels to track motion of the sun across the sky include bearing assemblies and other mechanical features configured to address mechanical challenges posed by the sloped and/or variable terrain that might otherwise prevent or complicate use of solar trackers on such terrain.

Solar trackers that may be advantageously employed on sloped and/or variable terrain to rotate solar panels to track motion of the sun across the sky include bearing assemblies and other mechanical features configured to address mechanical challenges posed by the sloped and/or variable terrain that might otherwise prevent or complicate use of solar trackers on such terrain.

A solar tracker provides sun tracking to solar panels, and includes several gearboxes for one single motor. In an embodiment, the solar tracker includes a torsion beam. defining a longintudinal direction of rotation and rotating the solar panels; motor, with motor shaft; first gearbox, at torsion beam at first position, and connected to motor shaft for transmitting to torsion beam rotation of motor shaft; second (Tarbox, mounted to torsion beam at second position further from motor than first position; and primary shaft, coaxial to motor shaft, and connected to second gearbox, for transmitting to second gearbox rotation of the motor shaft. Gearboxes define embedments withstanding torsion moment caused by wind loads for restricting rotation of torsion beam. It provides higher resistance to wind loads and allows for longer solar trackers.

A solar tracker provides sun tracking to solar panels, and includes several gearboxes for one single motor. In an embodiment, the solar tracker includes a torsion beam. defining a longintudinal direction of rotation and rotating the solar panels; motor, with motor shaft; first gearbox, at torsion beam at first position, and connected to motor shaft for transmitting to torsion beam rotation of motor shaft; second (Tarbox, mounted to torsion beam at second position further from motor than first position; and primary shaft, coaxial to motor shaft, and connected to second gearbox, for transmitting to second gearbox rotation of the motor shaft. Gearboxes define embedments withstanding torsion moment caused by wind loads for restricting rotation of torsion beam. It provides higher resistance to wind loads and allows for longer solar trackers.

The present invention relates to new energy vehicle field, and more particularly to vehicle-mounted tracking solar power generation system without photoelectric sensor. The current vehicle-mounted thin-film solar power generation device has a low power generation, inductive tracking technology has high cost and large volume, so neither of them can meet the electricity demand of new energy vehicles, therefore, at the moment when the photoelectric conversion rate is difficult to effectively improve in the short term, making the vehicle-mounted photovoltaic power generation system not only able to track but also has practicality, has become a technical problem that needs to be solved urgently in the vehicle-mounted solar charging industry, the present invention provides a solar tracking technology that adopts a combination of the orbital device and the platform, does not require real-time tracking and photoelectric sensors, and solves the above-mentioned technical problems well.

The present invention relates to new energy vehicle field, and more particularly to vehicle-mounted tracking solar power generation system without photoelectric sensor. The current vehicle-mounted thin-film solar power generation device has a low power generation, inductive tracking technology has high cost and large volume, so neither of them can meet the electricity demand of new energy vehicles, therefore, at the moment when the photoelectric conversion rate is difficult to effectively improve in the short term, making the vehicle-mounted photovoltaic power generation system not only able to track but also has practicality, has become a technical problem that needs to be solved urgently in the vehicle-mounted solar charging industry, the present invention provides a solar tracking technology that adopts a combination of the orbital device and the platform, does not require real-time tracking and photoelectric sensors, and solves the above-mentioned technical problems well.

Solar trackers that may be advantageously employed on sloped and/or variable terrain to rotate solar panels to track motion of the sun across the sky include bearing assemblies and other mechanical features configured to address mechanical challenges posed by the sloped and/or variable terrain that might otherwise prevent or complicate use of solar trackers on such terrain.

Solar trackers that may be advantageously employed on sloped and/or variable terrain to rotate solar panels to track motion of the sun across the sky include bearing assemblies and other mechanical features configured to address mechanical challenges posed by the sloped and/or variable terrain that might otherwise prevent or complicate use of solar trackers on such terrain.