This invention discloses an integrated, retractable, power-generating, ski-rotor transatmospheric
hybrid-powered airship, belonging to the field of ultra-large-scale airship technology. The entire aircraft is seamlessly integrated externally, with symmetrically arranged internal
airbag compartments on both sides. The central axis is divided into sections for the
crew control room, cargo bay,
fuel tank, and
rocket compartment. Retractable
wind power generation devices are installed on the sides and bottom, extending into the
atmosphere to generate
electricity. A ski-rotor, tilting
magnetic levitation ducted rotor is mounted on the top, dynamically adjusting the center of gravity for vertical
takeoff and landing. The
hull incorporates a global
eddy current stabilization
system with 10 sets of lateral damping and 1 set of central axis main damping.
Isotope power generation devices are symmetrically arranged in the left and right
airbag compartments. This invention employs a tiered power supply scheme combining atmospheric wind energy, transitional airspace
isotope power, and space
solar energy, coupled with a multi-compartment, pipeline-connected
helium circulation storage
system. It utilizes low-altitude rotor
cruise and high-altitude
rocket-assisted transatmospheric propulsion, solving the problems of traditional airships such as structural
fragility and environmentally constrained power supply.