公开(公告)号：US20240166384A1

公开(公告)日：2024-05-23

申请号：US18388171

申请日：2023-11-08

Applicant: THALES

Inventor： Marc RIEDINGER ,  Eric GUILLOUET ,  Antoine BONNET ,  Patrick GOUHIER

IPC: B64U20/87 ,  B64U20/70 ,  B64U50/20 ,  G01S13/933

CPC classification number: B64U20/87 ,  B64U20/70 ,  B64U50/20 ,  G01S13/933

Abstract: An unmanned aircraft includes three parallel beams extending in at least one longitudinal direction X from a rear side to a front side of the aircraft, the central beam forming a main fuselage containing a powertrain, with a propeller of diameter D configured to be driven by the powertrain being attached to a front end of the central beam, each side beam being at a distance L/2 from the central beam and each side beam supporting a radar at a front end of the beam.