The present disclosure relates to an anchoring platform for captive aircraft that addresses one of the main problems when handling captive aerostats, which is the excessive workload required to switch between flying and anchored states. The technology disclosed herein requires only one person to install the structure and the operation can be performed remotely or by a person. Additionally, cords, together with the confluence point, are wound into the anchoring device, the winch. The structure for anchoring the captive aircraft is the cradle which bears the aerostat, while the winch exerts tension to hold same static in the structure.

A tethered aerostat with a ground based deployment, extended duration and recovery system to accommodate a weather vaning deployed aerostat while maintaining a supply of a lift gas by having a rotatable tether pipe and a hollow tether. Included is a rotatable tether pipe device assembly with rotor and stator components disposed in an air tight housing assembly to provide a ground based gas maintenance system. An aerostat deployment buoyancy control maintenance and combined recovery platform is provided. The tethered aerostat systems and method increase deployment duration and allow more systems to be controlled and maintained on the ground without interrupting aerostat operational capabilities.

A tethered aerostat with a ground based deployment, extended duration and recovery system to accommodate a weather vaning deployed aerostat while maintaining a supply of a lift gas by having a rotatable tether pipe and a hollow tether. Included is a rotatable tether pipe device assembly with rotor and stator components disposed in an air tight housing assembly to provide a ground based gas maintenance system. An aerostat deployment buoyancy control maintenance and combined recovery platform is provided. The tethered aerostat systems and method increase deployment duration and allow more systems to be controlled and maintained on the ground without interrupting aerostat operational capabilities.

A tethered aerial system includes an on-board fuel cell for powering on-board electronics and a tether cable is less conductive than air. The tether cable includes a pipe for carrying a flow of gas to the fuel cell and/or maintain the gas level in a lighter-than-air platform, so that the tethered aerial system can remain operational for an extended period of time. The system is particularly applicable for maintaining communication links in remote areas, agriculture and applications in the IoT (Internet of Things), event coverage, interactive marketing, for post-disaster situations in rural areas and at mining sites or construction sites in remote environments. The present invention also is immune to rays.

A tethered aerial system includes an on-board fuel cell for powering on-board electronics and a tether cable is less conductive than air. The tether cable includes a pipe for carrying a flow of gas to the fuel cell and/or maintain the gas level in a lighter-than-air platform, so that the tethered aerial system can remain operational for an extended period of time. The system is particularly applicable for maintaining communication links in remote areas, agriculture and applications in the IoT (Internet of Things), event coverage, interactive marketing, for post-disaster situations in rural areas and at mining sites or construction sites in remote environments. The present invention also is immune to rays.

A surveillance drone is disclosed. The surveillance drone includes a gas-filled container and propellers for aerial mobility. The surveillance drone also includes an electronic surveillance sensing device positioned below the gas-filled container. The gas-filled container may be filled with a lighter than air gas such as, for example, helium.

A surveillance drone is disclosed. The surveillance drone includes a gas-filled container and propellers for aerial mobility. The surveillance drone also includes an electronic surveillance sensing device positioned below the gas-filled container. The gas-filled container may be filled with a lighter than air gas such as, for example, helium.

Provided is a transportation system comprising (a) a ground-based powered tug vehicle, (b) an airborne vehicle, and (c) a towline with end links connecting the ground-based vehicle and the airborne vehicle. Also provided are methods of transportation utilizing the transportation system.

Additionally provided is a transportation system comprising a hybrid vehicle that is propelled on a highway by a linear induction electric motor comprising a stationary motor element (stator) and a moving motor element (rotor), where the stator is incorporated into a groove in the highway and the rotor is incorporated into the hybrid vehicle and protrudes into the groove in the highway; and where the hybrid vehicle further comprises at least one wing that elevates the hybrid vehicle when propelled to a take-off speed on the highway. Methods of transportation utilizing this hybrid vehicle transportation system are further provided.

Provided is a transportation system comprising (a) a ground-based powered tug vehicle, (b) an airborne vehicle, and (c) a towline with end links connecting the ground-based vehicle and the airborne vehicle. Also provided are methods of transportation utilizing the transportation system.

Additionally provided is a transportation system comprising a hybrid vehicle that is propelled on a highway by a linear induction electric motor comprising a stationary motor element (stator) and a moving motor element (rotor), where the stator is incorporated into a groove in the highway and the rotor is incorporated into the hybrid vehicle and protrudes into the groove in the highway; and where the hybrid vehicle further comprises at least one wing that elevates the hybrid vehicle when propelled to a take-off speed on the highway. Methods of transportation utilizing this hybrid vehicle transportation system are further provided.

A lighter-than-air airship has an exoskeleton constructed of spokes and hubs to create a set of connected hexagrams comprised of isosceles triangles wherein the spokes flex and vary in length to produce the slope of said airship's surface. In one embodiment, the exoskeleton connects to a nose cone that includes a cockpit cabin for controlling the airship's operation from a single location that can be physically separated from the exoskeleton in response to catastrophic events and for autonomous and/or remotely piloted operation. An improved means is also provided for landing and unloading cargo, and through use of unmanned aerial vehicles in another embodiment, the airship is configured for remote pickup, transport, delivery and return of payloads such as packages. In yet another embodiment, the airship provides a communications platform for beam form transmission and satellite signal relay, including in combination with the foregoing disclosed attributes.