Two-duct propulsion control four-rotor-wing solar butterfly variant airship

Abstract

The invention discloses a two-duct propulsion control four-rotor-wing solar butterfly variant airship which comprises airship cloth, rotor wings and a solar film cell panel. A framework type airship cover is arranged inside the airship cloth, the framework type airship cover is fixedly connected with the airship cloth, the rotor wings are fixed to the outer side of the framework type airship cover, rotary vanes are connected above the rotor wings, and the rotor wings are movably connected with the rotary vanes. The solar film cell panel is arranged above the airship cloth, a airship-carrying platform is connected below the frame-type airship cover, an automatic helium charging and exhausting device and a charging and discharging power supply system are fixed to the top of the airship-carrying platform, and horizontal propulsion control ducts are installed on the outer side of the airship-carrying platform. The two-duct propulsion control four-rotor-wing solar butterfly variant airshipis provided with a connecting rod, a framework type airship cover connecting rod and a framework type airship cover connecting frame rod so that the shape of the airship can be changed, the lifting force of the airship can be improved, and the airship is prevented from falling during use.

Description

technical field [0001] The invention relates to the technical field of aircraft, in particular to a two-duct propulsion control four-rotor solar powered butterfly-shaped modified airship. Background technique [0002] The battery life of traditional pure electric aviation aircraft is too dependent on the battery, which is limited by the bottleneck of current battery technology development. As a result, the current pure electric aircraft generally has the problem of short battery life, which cannot meet the needs of today's flight missions and hinders its use. Further promotion, although the airship has the advantage of long battery life, but the traditional airship has poor wind resistance, inflexible manipulation and other factors limit the use of the airship. [0003] Pure electric aircraft on the market have short battery life, poor crash resistance, and poor wind resistance of airships, which affect the user experience. Therefore, we propose a two-duct propulsion control...

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a two-duct propulsion control four-rotor solar butterfly variant airship, to solve the problem of short battery life, poor crash resistance and poor wind resistance of the pure electric aircraft proposed in the above background technology, which affects users. problems with user experience

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