The invention relates to an unmanned aerodyne with vertical take-off and landing, of the VTOL type, comprising at least one central body (1), at least three arms (2) secured to said central body (1) and uniformly distributed about the central axis of said central body (1), a plurality of propulsion units (3), each propulsion unit (3) being secured to the free end of an arm (2), i.e. to the distal end of an arm (2), and each one comprising at least one pusher propeller (4) and an electric motor (5) that can drive said propeller (4), and an electronic card that is secured to the central body (1) and can control at least the electric motors (5) of the propulsion units (3). Said aerodyne is characterised in that each arm (2) consists of a receiving blade comprising at least three different zones, a so-called capturing zone, a so-called intermediate zone and a so-called motor zone, and in that the central body (1) consists of a long vertical body comprising, from the upper part to the lower part thereof, at least one first so-called upper section (1a) receiving at least one sensor (6) connected to the electronic card, a second so-called hub section (1b) that comprises means (7) for securing the capturing part of each arm (2) and can receive the electronic card, a third so-called navigation section (1c) comprising at least remote measuring means (8), a fourth so-called power supply section (1d) comprising at least one battery powering the at least one sensor (6), the remote measuring means (8) and the electronic card, and a fifth section (1e) comprising at least one sensor and/or means for securing a nacelle.
AERODYNE SANS PILOTE
UNMANNED AERODYNE
UNBEMANNTER FLUGKÖRPER
2020-12-09
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |