Vertical take-off and landing aircraft
AssigneeObshchestvo S Ogranichennoj Otvetstvennostyu “Avianovatsii”
InventorsSergei Evgenievich Tovkach, Aleksei Viktorovich Shanin, Igor Chudakov
Life of this patent
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Abstract
The present technology relates to the field of aircraft construction, and more specifically to vertical take-off and landing aircraft. The aircraft includes a bearing frame of a spatial structure, a seat, controls, moto-units, a control system, and a remote control system. The bearing frame is designed with a central portion and with at least two peripheral clusters. The central portion and the peripheral clusters of the frame are designed as a spatial structure. Each peripheral cluster is designed as a truss structure of at least three segments of the same type, which are interconnected. Inside each segment there is a moto-unit, which has at least one motor and at least one horizontal-rotation propeller.
Claims20
A vertical take-off and landing aerial vehicle comprising:
- a base frame, the base frame including a central portion and at least two peripheral clusters, the central portion and the at least two peripheral clusters being implemented as a spacious construction, each peripheral cluster of the at least two peripheral clusters including at least three segments connected to each other;
- a seat mounted within the base frame;
- a control system for controlling operations of at least a portion of the vertical take-off and landing aerial vehicle;
- and
- a respective motor installation located in each segment of the at least three segments, the respective motor installation containing:
- at least one engine;
- at least one horizontal rotation propeller;
- an individual power supply source, having been installed within the respective motor installation, for powering on the at least one engine of the respective motor installation;
- and
- an individual engine controller having been installed within the respective motor installation, and being configured, by the control system, to control the at least one engine of the respective motor installation.
Dependencies are inferred from the claim text.