MOBILE AEROENERGOSTAT MODULE Russian patent published in 2021 - IPC F03D9/32 F03D7/00 

FIELD: power engineering.

SUBSTANCE: invention relates to the field of high-altitude air-based wind power. The mobile module of the aeroenergostat has a neutral buoyancy assembly and is additionally equipped in the bow with a removable pair of aircraft motors with invariably vertical axes of rotation of the screws and a pair of non-removable aircraft motors at the stern of the device, placed according to the scheme and operating in the multicopter mode from reversible electric motors connected to the onboard battery. The wind power unit with a radial-blade turbine, leeward relative to the nacelle, is suspended from below, like all other equipment of the module to its composite platform. On top of the platform, a soft cigar-shaped shell filled with light gas is pulled by bandage arcs and ribbons. The suspension of the block consists of two vertical struts, parallel to the plane perpendicular to the wind, with a clearance, which are divided in height by coaxial cylindrical hinges into upper fixed links ending with horizontal hinge axes, and lower movable links hanging from the hinge bushings and ending with fasteners with the wind power unit nacelle, for which they are forcibly rotated towards the stern of the module until they occupy a position in which the turbine blades are located in a horizontal plane under the mentioned platform, rotation is stopped and the mobility of the module is not prevented. Such a turn is carried out by an on-board winch displaced from the suspension of the wind power unit to the bow of the module, at least one steel rope from the winch drum is stretched and captures the top of the horizontal bracket connecting the hinged bushings and curved to the stern of the aeronautical structure. The mobile module can be equipped with a source of energy supply for the process of floating in the atmosphere from a wind turbine with orthogonal blades, at the point of wind energy use, its positive buoyancy can be further increased due to the elasticity of the bottom of the gas-filled shell and the tubular balloon.

EFFECT: providing the aeronautical module of the aeroenergostat with the ability to independently rise into the air, move in the atmosphere and descend to the ground berthing node.

3 cl, 6 dwg