The present disclosure relates to a method and a combined-propulsion system for high-speed vehicles, which includes a closed tubular guiding structure and a vehicle designed to move through the inside of the tubular structure. The system includes a vacuum system coupled to the tubular structure to provide a safe atmosphere at low pressure, always above the Armstrong limit; electric propulsion means arranged in an initial section of the structure, to accelerate the vehicle to a determined cruising speed; and compressed-air propulsion means arranged on the vehicle, to maintain the cruising speed.

The present disclosure relates to a power distribution architecture for an off-road vehicle. The power distribution architecture includes a work circuit and a propel circuit and is configured for facilitating bi-directional power exchange between the work circuit and the propel circuit.

The vehicle system can include: a set of vehicle couplings (e.g., a tractor interface, a trailer interface, etc.); a chassis, a battery pack, an electric powertrain, a sensor suite, and a controller. The modular vehicle system can optionally include landing gear, a suspension, and any other suitable set of components. The vehicle system functions to structurally support and/or tow a trailer—such as a Class 8 semi-trailer—and/or to augment/supplement a tractor propulsive capability (e.g., via a diesel/combustion engine) with a supplementary electric drive axle(s).

One example provides a battery pack for an electric vehicle. The battery pack includes a plurality of rechargeable battery modules, an enclosure defining an interior space in which the plurality of rechargeable battery modules are enclosed, and a charging port mounted to the enclosure, the charging port electrically connected within the enclosure to the plurality of rechargeable battery modules, the charging port accessible from an exterior of the enclosure and configured to electrically connect an external electrical charging source to the plurality of rechargeable battery modules.

An aircraft assist system described herein includes an aircraft coupling counterpart attached to a strut of a landing gear of an aircraft, and an assist vehicle. The assist vehicle includes a frame, ground-engaging wheels mounted to the frame, a power source for driving one or more of the ground-engaging wheels, and a vehicle coupling counterpart for engagement with the aircraft coupling counterpart. The aircraft coupling counterpart and the vehicle coupling counterpart define a swivel connection for transferring a propulsive force from the takeoff assist vehicle to the aircraft. The aircraft coupling counterpart is disengageable from the vehicle coupling counterpart by upward movement of the aircraft coupling counterpart relative to the vehicle coupling counterpart.

Systems and methods preventing vehicle runaway of an electric powersport vehicle in an emergency situation are provided. One method comprises receiving, via an emergency shutoff switch of the electric powersport vehicle or via a tether switch of the electric powersport vehicle, a signal indicating an existence of the emergency situation while the electric powersport vehicle is in motion, and in response to the signal, attempting to regulate an operation of an electric motor configured to propel the electric powersport vehicle to cause regenerative braking of the electric motor while the electric powersport vehicle is in motion.

Systems and methods for mitigating wear of electric vehicles are provided. A method of operating an electric powersport vehicle includes receiving an accelerator command and driving an electric motor of the vehicle based on whether or not the accelerator command is accompanied by a braking command. When the accelerator command exists at a same time as the braking command, the output of the electric motor is limited to a lower output torque value than when the accelerator command exists at a different time as the braking command.

A mobile platform comprising: (a) one or more platforms to support one or more cartridges, (b) one or more compartments within the one or more platforms, (c) one or more vertical supports connected to the one or more platforms, (d) a plurality of wheels connected to a bottom of the one or more platforms, and (e) one or more recesses located in the one or more platforms to receive one or more support accessories, wherein the one or more compartments are shaped to receive the one or more cartridges so that the one or more cartridges are secured to the one or more platforms during movement.

Systems and methods for providing locked rotor protection for powertrains of electric vehicles are provided. One method for operating an electric vehicle includes receiving a command for propelling the electric vehicle, driving an electric motor of the powertrain of the electric vehicle, and determining that the powertrain is obstructed. After determining that the powertrain is obstructed, an output is generated to initiate one or more actions intended to protect the powertrain.

A rotor assembly for deployment within a momentum control device that enables near-zero revolutions per minute (RPM) sensing, and method for making same, are provided. The provided rotor assembly utilizes a magnet coupled to the rotor shaft and a stationary sensor element to detect magnetic flux from the magnet and derive reliable near zero RPM therefrom.