An airborne platform vehicle comprising an aircraft with a platform affixed to the top side providing for a multipurpose airborne platform is disclosed. The airborne platform vehicle comprising a platform affixed to the top side of an aircraft or airship providing accessibility to the platform from either inside or outside the aircraft. The aircraft itself being able to float or fly by virtue of the lighter than air gas inside the body of the aircraft or with assisted lift from wings, being propelled by a ducted fan, propeller drive system, or otherwise and having a power source from which to power the drive system. The airborne platform vehicle being capable of movement and remaining upright through the use of ballast, propellers, ducted fans, vector thrusters, wings, fins, and/or rudders. The airborne platform vehicle itself being able to take-off and land as well as stay afloat for long durations in a stationary or non-stationary position.

An airborne platform vehicle comprising an aircraft with a platform affixed to the top side providing for a multipurpose airborne platform is disclosed. The airborne platform vehicle comprising a platform affixed to the top side of an aircraft or airship providing accessibility to the platform from either inside or outside the aircraft. The aircraft itself being able to float or fly by virtue of the lighter than air gas inside the body of the aircraft or with assisted lift from wings, being propelled by a ducted fan, propeller drive system, or otherwise and having a power source from which to power the drive system. The airborne platform vehicle being capable of movement and remaining upright through the use of ballast, propellers, ducted fans, vector thrusters, wings, fins, and/or rudders. The airborne platform vehicle itself being able to take-off and land as well as stay afloat for long durations in a stationary or non-stationary position.

The present invention ensures that when condensation forms in a container for a flying object, water from the condensation does not adversely affect an object in the container. Container 12 is a cabin of a gas balloon and comprises Main Body 121, which is an airtight container for accommodating Crew Member H1 and is filled with Air 122, Condensation Promoting Member 123 is made of a material that has a high thermal conductivity, such as aluminum, and is partly exposed to the inside of Main Body 121 and partly exposed to the outside of Main Body 121. Water Collecting Vessel 124 is positioned below the portion of Condensation Promoting Member 123 exposed to the inside of Main Body 121 and collects water from condensation formed on Condensation Promoting Member 123. Conduit 125 directs water collected by Water Collecting Vessel 124 to Water Collection Container 126. Condensation forms on Condensation Promoting Member 123, a temperature of which is lower than that in Main Body 121, and thus condensation does not form on Main Body 121.

The present invention ensures that when condensation forms in a container for a flying object, water from the condensation does not adversely affect an object in the container. Container 12 is a cabin of a gas balloon and comprises Main Body 121, which is an airtight container for accommodating Crew Member H1 and is filled with Air 122, Condensation Promoting Member 123 is made of a material that has a high thermal conductivity, such as aluminum, and is partly exposed to the inside of Main Body 121 and partly exposed to the outside of Main Body 121. Water Collecting Vessel 124 is positioned below the portion of Condensation Promoting Member 123 exposed to the inside of Main Body 121 and collects water from condensation formed on Condensation Promoting Member 123. Conduit 125 directs water collected by Water Collecting Vessel 124 to Water Collection Container 126. Condensation forms on Condensation Promoting Member 123, a temperature of which is lower than that in Main Body 121, and thus condensation does not form on Main Body 121.

A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability. A vehicle comprising a first lift device capable of providing hydrostatic lift; a second lift device capable of providing dynamic lift through movement; and a system structured to generate thrust coupled to the second lift device, the second lift device and the thrust generation system capable of rotating together about an axis that is lateral to a longitudinal axis of the vehicle at angles at least in the range of 90 degrees to and including 180 degrees.

A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability. A vehicle comprising a first lift device capable of providing hydrostatic lift; a second lift device capable of providing dynamic lift through movement; and a system structured to generate thrust coupled to the second lift device, the second lift device and the thrust generation system capable of rotating together about an axis that is lateral to a longitudinal axis of the vehicle at angles at least in the range of 90 degrees to and including 180 degrees.

The method for transporting a payload to a target location, comprises the following steps of providing a hybrid airship comprises a buoyancy enclosure, a gondola carried by the buoyancy enclosure and a payload carrier, and at least one propeller; flying the hybrid airship carrying the payload to a target location, flying the hybrid airship carrying the payload comprising generating a lift force with the at least one propeller. Flying the hybrid airship carrying the payload comprises tilting the longitudinal axis of the buoyancy enclosure to a positive pitch to generate an aerodynamic lift force when the hybrid airship carrying the payload moves longitudinally.

The method for transporting a payload to a target location, comprises the following steps of providing a hybrid airship comprises a buoyancy enclosure, a gondola carried by the buoyancy enclosure and a payload carrier, and at least one propeller; flying the hybrid airship carrying the payload to a target location, flying the hybrid airship carrying the payload comprising generating a lift force with the at least one propeller. Flying the hybrid airship carrying the payload comprises tilting the longitudinal axis of the buoyancy enclosure to a positive pitch to generate an aerodynamic lift force when the hybrid airship carrying the payload moves longitudinally.

The present invention concerns hybrid airship comprising at least one buoyancy enclosure containing a gas lighter than air, a gondola attached below the buoyancy enclosure, the gondola extending along a longitudinal axis, at least one propeller configured to propel the hybrid airship, the at least one propeller being attached to the buoyancy enclosure, at least one generator, configured to provide power to the propeller, the generator being connected to the gondola. The hybrid airship comprises an arm protruding from the gondola and connecting the generator to the gondola.

The present invention concerns hybrid airship comprising at least one buoyancy enclosure containing a gas lighter than air, a gondola attached below the buoyancy enclosure, the gondola extending along a longitudinal axis, at least one propeller configured to propel the hybrid airship, the at least one propeller being attached to the buoyancy enclosure, at least one generator, configured to provide power to the propeller, the generator being connected to the gondola. The hybrid airship comprises an arm protruding from the gondola and connecting the generator to the gondola.