A flying robot (10) with projector, including a movable end (100) and a fixed end (200). A distributed working mode is used on the movable end (100) and the fixed end (200). The movable end (100) includes a top (110), a main body (120) and a bottom (130). The top (110) includes a lift system (112) and one or more proximity sensors (114); the main body (120) is a sealed hollow spherical body or spheroid body made of a film material capable of being used as a rear projection screen, and is filled with a gas of which the density is less than that of the air. The bottom (130) includes one or more rear projectors (131), a wireless communication module (132), a microcontroller (133), a battery (134), a direction and steering controlling device (135), a camera device (136), a sound capturing and reproduction device (137), a height sensor (138) and other sensors, etc. The fixed end (200) includes a wireless communication module (220), a control apparatus (240), a charging port (260), and other data interfaces, etc. The flying robot (10) with projector according to the present invention facilitates human-machine interaction and is suitable for being used in both indoor and outdoor environments.

An unmanned hybrid airship for delivering packages, featuring: a forward payload bay counterbalanced by a moveable counterweight; and a gripping mechanism for engaging unconventional mooring structures such as balcony rails and window sills. Other embodiments are described.

A flying robot (10) with projector, including a movable end (100) and a fixed end (200). A distributed working mode is used on the movable end (100) and the fixed end (200). The movable end (100) includes a top (110), a main body (120) and a bottom (130). The top (110) includes a lift system (112) and one or more proximity sensors (114); the main body (120) is a sealed hollow spherical body or spheroid body made of a film material capable of being used as a rear projection screen, and is filled with a gas of which the density is less than that of the air. The bottom (130) includes one or more rear projectors (131), a wireless communication module (132), a microcontroller (133), a battery (134), a direction and steering controlling device (135), a camera device (136), a sound capturing and reproduction device (137), a height sensor (138) and other sensors, etc. The fixed end (200) includes a wireless communication module (220), a control apparatus (240), a charging port (260), and other data interfaces, etc. The flying robot (10) with projector according to the present invention facilitates human-machine interaction and is suitable for being used in both indoor and outdoor environments.

A flying robot (10) with projector, including a movable end (100) and a fixed end (200). A distributed working mode is used on the movable end (100) and the fixed end (200). The movable end (100) includes a top (110), a main body (120) and a bottom (130). The top (110) includes a lift system (112) and one or more proximity sensors (114); the main body (120) is a sealed hollow spherical body or spheroid body made of a film material capable of being used as a rear projection screen, and is filled with a gas of which the density is less than that of the air. The bottom (130) includes one or more rear projectors (131), a wireless communication module (132), a microcontroller (133), a battery (134), a direction and steering controlling device (135), a camera device (136), a sound capturing and reproduction device (137), a height sensor (138) and other sensors, etc. The fixed end (200) includes a wireless communication module (220), a control apparatus (240), a charging port (260), and other data interfaces, etc. The flying robot (10) with projector according to the present invention facilitates human-machine interaction and is suitable for being used in both indoor and outdoor environments.

A blockchain mining platform that comprises an airship utilizing an innovative lift mechanism featuring dynamic and static vacuum chambers. Solar panels power the vast array of computers required for efficient and cost effective blockchain mining. Internet connectivity would be accomplished by communication with satellites or by microwave transmission to ground station. In alternate modes, different types of airships with the ability to stay aloft for extended periods of time could be used.

A blockchain mining platform that comprises an airship utilizing an innovative lift mechanism featuring dynamic and static vacuum chambers. Solar panels power the vast array of computers required for efficient and cost effective blockchain mining. Internet connectivity would be accomplished by communication with satellites or by microwave transmission to ground station. In alternate modes, different types of airships with the ability to stay aloft for extended periods of time could be used.

Aspects of the technology relate to altitude control and lateral propulsion systems in lighter-than-air (LTA) platforms configured to operate in the stratosphere. For instance, an LTA platform may include an envelope filled with lift gas and a payload for providing telecommunication or video services. A fault or failure condition with one or more components of these systems, or with the envelope of the LTA platform itself, can prevent a high altitude platform (HAP) from operating as intended, or otherwise reduce its useful life. Onboard systems are configured to handle adverse conditions, such as a fault or failure of the envelope, an altitude control system component, or the lateral propulsion system. This may be done according to one or more ranked lists of adverse operational conditions. Different conditions may map to different corrective actions, which may be prioritized in importance, for instance to reduce the chance of catastrophic system failure.

A payload lift and positioning system mounted to an airship for precisely positioning a payload being lowered from the airship to the ground. The payload lift and positioning system includes a support beam structure mounted to an underside of the airship, the support beam structure including load hoists and guide cable hoists mounted thereto. A payload supporting structure to carry the payload, the payload supporting structure being connected to support beam structure by the load hoists and guide cable hoists. A guide cable system includes a plurality of guide cables, each extending from the guide cable hoists disposed on the support beam structure. A positioning system includes a guide member that is mounted on the payload supporting structure to control the position of the payload being lowered from the airship to ground.

A payload lift and positioning system mounted to an airship for precisely positioning a payload being lowered from the airship to the ground. The payload lift and positioning system includes a support beam structure mounted to an underside of the airship, the support beam structure including load hoists and guide cable hoists mounted thereto. A payload supporting structure to carry the payload, the payload supporting structure being connected to support beam structure by the load hoists and guide cable hoists. A guide cable system includes a plurality of guide cables, each extending from the guide cable hoists disposed on the support beam structure. A positioning system includes a guide member that is mounted on the payload supporting structure to control the position of the payload being lowered from the airship to ground.

Packages used to deliver items or other payloads via a drone may be customized and 3D printed to house the payload. The package may be customized to minimize the size and/or weight needed to house the payload. The customized packages may include one or more attachment mechanisms adapted to engage with or otherwise be coupled to the drone for delivery. Multiple individual customized packages can be secured together into a composite package for delivery by drone. The customized package may be designed to be aerodynamic given the shape of the payload and the flight characteristics of the drone. The drone itself may be the package, with the payload housed within a portion of the drone. The package and/or a portion of the drone (e.g., fuselage, wing, body, frame, etc.) may be printed at least partially in, on, or around an item or package to be transported by the drone.