FIELD: aviation.
SUBSTANCE: invention relates to aeronautical engineering. Hybrid airship comprises a shell filled with a carrier gas, having the form of a body of revolution relative to the vertical axis of the shell, power rings of the poles of the shell, having a mechanical connection, a power ring of mid-section, vertical thrust engines with equal angular pitch are arranged on power ring of shell midship section, horizontal thrust engines with variable thrust vector in horizontal plane. Along the vertical axis of the shell there is a central power beam which crosses the shell in the upper and lower poles and is movably connected by means of axial movable radial thrust supports and power rings with the housing of the hybrid airship in the plane of power rings of the midship section of the shell and poles of the shell. Locking brakes are installed on power rings. Horizontal thrust engines are located above the upper pole of the shell and under the lower pole of the shell, attached to the central power beam and can be located symmetrically relative to the axis of the central power beam on the traverse, fixed to the central power beam, to the lower part of which the quick-detachable modules of the on-board systems and the attachment unit of the payload module are attached.
EFFECT: airship design with high manoeuvrability and possibility of accurate positioning.
2 cl, 7 dwg
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Authors
Dates
2025-04-17—Published
2024-04-01—Filed