Abstract: The present invention relates to an electronic gear shifter assembly for a dual-mode flying and driving vehicle. The electronic gear shifter assembly may include a lever moveable between a first shifting path that includes at least one drive-related operating position, and a second shifting path that includes at least one flying-related operating position.

Abstract: A combined flying-driving vehicle having a unique hybrid propulsion system architecture that provides a very high level of reliability and functionality to the user.

Abstract: A combined flying-driving vehicle having a unique hybrid propulsion system architecture that provides a very high level of reliability and functionality to the user.

Abstract: A combined flying-driving vehicle having a hybrid propulsion system architecture, foldable wings, and rotatable propulsion devices that is capable of vertical take-off and landing (VTOL), fixed wing cruise, and legally operating one a roadway surface.

Abstract: An integrated transportation system with vertical take-off and landing capabilities utilizes multiple common ground, pod, and flight components to facilitate efficient vertiport operations. Automated system operations, enable individuals and cargo routing between destinations in congested urban environments, as well as in remote locations selectively using the integrated ground vehicles and flight vehicles to deliver the payload pod to the destination.

Abstract: The present invention relates to an electronic gear shifter assembly for a dual-mode flying and driving vehicle. The electronic gear shifter assembly may include a lever moveable between a first shifting path that includes at least one drive-related operating position, and a second shifting path that includes at least one flying-related operating position.

Abstract: A combined flying-driving vehicle having a unique hybrid propulsion system architecture that provides a very high level of reliability and functionality to the user.

Abstract: A centrifugal direct injection engine having an open-ended compartment with a combustion chamber at a closed end thereof and an exhaust nozzle at its open end. The compartment is provided with a narrow portion defining a throat that connects the combustion chamber and the exhaust nozzle. A propellant injection manifold is rotatably mounted within the combustion chamber, the propellant injection manifold being configured for rapid rotation within the combustion chamber. The propellant injection manifold includes an upper disk member, an intermediate disk member and a lower disk member, the disks being joined together to form an integral member with the outer perimeter of the disks being in registration with one another. A fuel is introduced into the combustion chamber through the propellant injection manifold and the nozzles.