Abstract: A plurality of propellers generate vertical thrust at least some of the time. An attachment sub-system detachably couples to a vertical connector, where a plurality of vertically-stacked multicopters are configured to detachably couple to the vertical connector in order to transport a load at a bottom end of the vertical connector. There is an opening in a vehicle frame that is configured to: (1) receive the vertical connector prior to the attachment sub-system detachably coupling to the vertical connector and (2) hold the vertical connector while the attachment sub-system is detachably coupled to the vertical connector.

Abstract: According to an aspect, an electrochemical cell may include a vessel, at least two instances of an anode assembly, at least two instances of an oxygen evolution electrode (OEE), and a gas diffusion electrode (GDE). In the vessel, the GDE may be disposed between mirrored arrangements of the at least two instances of the OEE and the at least two instances of the anode assembly.

Abstract: According to one aspect, a power storage system may include an enclosure, and one or more modules disposed in the enclosure. Each of the one or more modules may include a plurality of electrochemical cells electrically coupled to one another, each one of the plurality of electrochemical cells including an oxygen evolution electrode (OEE), an anode, a gas diffusion electrode (GDE), an electrolyte, and a vessel and, within the vessel, the OEE, the anode, and the GDE at least partially immersed in the electrolyte.

Abstract: In an embodiment, a system for battery shifting for center of gravity (CG) control includes a battery holder and a controller. The battery holder is adapted to change between a first battery position and a second battery position in a vehicle. The battery holder being in the first position causes the vehicle to have a first CG and the battery holder being in the second position causes the vehicle to have a second CG. The controller is configured to move the battery holder into the first position at least some of the time when the vehicle is flying at a first angle such that the vehicle has a CG in a first vehicle location, and move the battery holder into the second position at least some of the time when the vehicle is flying at a second angle such that the vehicle has a CG in a second vehicle location.