A propulsion system for an electric vehicle comprising a high voltage battery unit having a first high voltage battery connected in series with a second high voltage battery, which may also be referred to as a first and second battery bank, and one or more power inverters arranged to connect the battery banks to one or more electric machines. The one or more power inverters and the one or more electric machines are configured to form a first and a second three-phase system. The described architecture incorporating dual battery banks, and dual and/or multiphase inverters and electric machines can provide enhanced redundancy and limp home functionality in cases where a fault or error occurs in the inverter and/or in the electric machine so that a faulty three-phase system can be operated in a safe-state mode.

An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, a line having one end coupled to the chassis and an opposite free end, wherein the free end is positioned below the chassis, and a severing mechanism operable to sever the line under control of the control system.

A method for determining whether an electric insulation of a conductor is sufficient, comprising switching on or off a resistive load between the conductor and ground, measuring a first voltage value u, of a resulting voltage U.sub.m between the conductor and ground at a first point in time t, after switching on or off the load, determining if the first voltage value u, fulfils a first condition, and/or determining an initial rate of change of the resulting voltage U.sub.m between the conductor and ground based on the first voltage value ui, and determining if the initial rate of change fulfils a second condition, determining that the electric insulation is sufficient when at least one of the first and second conditions is fulfilled.

A battery enclosure for a personal watercraft is provided. Different configurations of the battery enclosure are disclosed, as well as different arrangements of the battery enclosure within the personal watercraft and with respect to other features of the personal watercraft. According to one embodiment, a personal watercraft includes a deck and a hull defining an interior volume. An electric motor is housed within the interior volume, the electric motor being operable to rotate a drive shaft. A battery pack having a battery enclosure housing one or more batteries is also positioned within the interior volume. A portion of at least one battery of the one or more batteries is positioned vertically above the drive shaft.

An electric mobility apparatus is disclosed. The electric mobility apparatus may include a mid-frame assembly in which a bracket fastened to at least one component is mounted on an inner side, a front frame assembly having a portion inserted into a front face of the mid-frame assembly so as to be coupled to the mid-frame assembly, and a tail frame assembly having a portion inserted into a rear face of the mid-frame assembly so as to be coupled to the mid-frame assembly, wherein the bracket is fastened to both side faces inside the mid-frame assembly.

The present teachings relate generally to a small remote vehicle having rotatable flippers and a weight of less than about 10 pounds and that can climb a conventional-sized stairs. The present teachings also relate to a small remote vehicle can be thrown or dropped fifteen feet onto a hard/inelastic surface without incurring structural damage that may impede its mission. The present teachings further relate to a small remote vehicle having a weight of less than about 10 pounds and a power source supporting missions of at least 6 hours.

A system for modular dynamically adjustable capacity storage for a vehicle is provided. The system includes a battery pack including a plurality of battery cells, a negative terminal including a chassis ground connection, and a plurality of positive battery pack terminals. The negative terminal and the plurality of positive battery pack terminals are useful for connecting at least one electrical circuit through the battery pack. The system further includes a battery cell switching system, including a plurality of solid-state switches connected to each of the battery cells. The plurality of solid-state switches is operable to selectively connect a portion of the battery cells in parallel, selectively connect the portion of the battery cells in series, and selectively connect one of the plurality of battery cells to one of the plurality of positive battery pack terminals.

A military vehicle including an engine coupled to the chassis for providing mechanical power to the military vehicle, a motor/generator coupled to the engine, and an energy storage system including a battery electrically coupled to the motor/generator. The military vehicle is operable in a silent mobility mode with the engine inactive and the energy storage system providing power to the motor/generator to operate the military vehicle. The motor/generator and the battery are sized such that electrical power generation through engine drive of the motor/generator is greater than the power depletion through operation of the military vehicle in the silent mobility mode. The motor/generator can charge the energy storage system while the military vehicle is driving or stationary.

An electrified vehicle includes a front subframe, a rear subframe, and a body that connects the front subframe to the rear subframe so that forces acting on the front subframe and the rear subframe are transmitted through the body. The vehicle also includes a housing coupled to an underside of the body between the front subframe and the rear subframe. An energy storage system is enclosed in the housing and includes a battery and a battery interface configured to electrically couple the battery to at least one component of the electrified vehicle.

A materials handling vehicle including a battery receiving space, and a removable battery assembly, wherein: the battery receiving space includes opposing pairs of battery guide pins, each opposing pair arranged on opposite sides of the battery receiving space, and each opposing pair includes a latching pin and a guiding pin; the removable battery assembly includes a battery locking mechanism; the battery locking mechanism includes spring-loaded locking pins that are spring-biased in extended positions and are movable from the extended positions to respective retracted positions; the latching pin of each opposing pair of battery guide pins includes a recess forming a battery latch that is positioned to receive a leading portion of one of the spring-loaded locking pins in the extended position.