A compact lift generating system is provided. The lift generating system embodies a wind tunnel enclosure extending between an inlet and an outlet. An airflow generator may be fluidly coupled to the enclosure inlet, an intake of a feedback conduit may be fluidly associated with the enclosure outlet, and an airfoil disposed therebetween. Airflow is urged to engage the airfoil, producing lift. The airflow generator may include a fan, an amplifier and an air knife fluidly coupled in series, wherein an output end of the feedback conduit fluidly connects between the airflow generator and the amplifier. A plurality of wind tunnels enclosures may be operatively associated in series. A plurality of airfoils may be provided in a stacked orientation in one wind tunnel enclosure.

Disclosed embodiments include methods of removing carbon dioxide from combustion gas from an engine of a vehicle, systems for removing carbon dioxide from combustion gas from an engine of a vehicle, vehicles, methods of managing carbon dioxide emissions from an engine of a vehicle, and computer software program products for managing carbon dioxide emissions from an engine of a vehicle.

Disclosed embodiments include methods of removing carbon dioxide from combustion gas from an engine of a vehicle, systems for removing carbon dioxide from combustion gas from an engine of a vehicle, vehicles, methods of managing carbon dioxide emissions from an engine of a vehicle, and computer software program products for managing carbon dioxide emissions from an engine of a vehicle.

An Air Platform design is very simple concept as the multi rotor, drone technology with more powerful engines to move heavy objects with precision and speed. It uses the hardware Air Platform and the software to give instruction to the Air Platform. The Multi Rotor AirTrain patent, Ser. No. 14/698,262 design combine with Airtrain, patent Ser. No. 14/173,165 and Symmetrical Airliner, patent pending Ser. No. 14/176,397 contributed in the major source for coming up with this new patent filing of Air Platform. It is multipurpose air platform that can be replace wheels. The wheels of wheel chairs, cars, trucks, buses, trains, airplanes and even ships. Replacing the wheels with the platforms allows all things that move on the surface to glide on the flat surface like an ice puck or fly in and out of ground effects to increase the fuel efficiency with better control. Thus, the Air Platform will increase the safety and reduces the construction and operation costs of all things that is effected by the friction and that reduces different frictions.

An Air Platform design is very simple concept as the multi rotor, drone technology with more powerful engines to move heavy objects with precision and speed. It uses the hardware Air Platform and the software to give instruction to the Air Platform. The Multi Rotor AirTrain patent, Ser. No. 14/698,262 design combine with Airtrain, patent Ser. No. 14/173,165 and Symmetrical Airliner, patent pending Ser. No. 14/176,397 contributed in the major source for coming up with this new patent filing of Air Platform. It is multipurpose air platform that can be replace wheels. The wheels of wheel chairs, cars, trucks, buses, trains, airplanes and even ships. Replacing the wheels with the platforms allows all things that move on the surface to glide on the flat surface like an ice puck or fly in and out of ground effects to increase the fuel efficiency with better control. Thus, the Air Platform will increase the safety and reduces the construction and operation costs of all things that is effected by the friction and that reduces different frictions.

Disclosed embodiments include methods of removing carbon dioxide from combustion gas from an engine of a vehicle, systems for removing carbon dioxide from combustion gas from an engine of a vehicle, vehicles, methods of managing carbon dioxide emissions from an engine of a vehicle, and computer software program products for managing carbon dioxide emissions from an engine of a vehicle.

A hover drone system includes a hull extending from a front end to a rear end and from a first side to a second side; ducted fans integrated into the hull, the ducted fans provide lift and propulsion for the hover drone system, the fans operated by a power source; a first sidewall extending from the first side of the hull; a second sidewall extending from the second side of the hull; and a flexible skirt extending from the front end of the hull and from the first sidewall to the second sidewall; the rear end of the hull is open.

A hover drone system includes a hull extending from a front end to a rear end and from a first side to a second side; ducted fans integrated into the hull, the ducted fans provide lift and propulsion for the hover drone system, the fans operated by a power source; a first sidewall extending from the first side of the hull; a second sidewall extending from the second side of the hull; and a flexible skirt extending from the front end of the hull and from the first sidewall to the second sidewall; the rear end of the hull is open.