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公开(公告)号：WO2020012430A2
公开(公告)日：2020-01-16
申请号：PCT/IB2019/055959
申请日：2019-07-12
Applicant: SKYPULL SA
Inventor： CATTANO, Aldo , BETTELINI, Alberto , MONA, Nicola
Abstract: Unmanned aircraft, comprising a first wing (11) and a second wing (12), wherein at least one of the first and second wings (11, 12) are made with a multiple element configuration comprising a set of wing profiles (21, 22, 23, 24) which are arranged at least partially in a condition of mutual proximity, said set of wing profiles comprising at least a first wing profile (21) and a second wing profile (22 ) which are mutually positioned one after the other and which define a leading edge and a trailing edge, respectively, wherein said first wing (11) and said second wing (12) are spaced with respect to each other; said aircraft further comprising interconnection supports (13, 14) between said first wing (11) and said second wing (12), holding said first and second wing (11, 12) at a given distance, said unmanned aircraft further comprising at least one aerodynamic container (40) positioned between said first wing (11) and said second wing (12), said aerodynamic container (40) comprising an inner compartment and a casing enclosing said inner compartment and being adapted and configured to carry a load and/or a central motor (50c).
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公开(公告)号：WO2021220148A1
公开(公告)日：2021-11-04
申请号：PCT/IB2021/053449
申请日：2021-04-27
Applicant: SKYPULL SA
Inventor： CATTANO, Aldo
IPC: B64C39/02
Abstract: The present invention relates to an unmanned aircraft (10), comprising at least one upper wing (11), at least one lower wing (12), at least one first and one second side wing (14) each oriented obliquely with respect to the upper wing (11) and the lower wing (12), and at least one engine (19) capable of at least propelling the unmanned aircraft (10) in flight, in which the upper wing (11) and the lower wing (12) are positioned in two substantially parallel planes, wherein the assembly formed by the at least one upper wing (11 ), the at least one lower wing (12) and the at least one first and second lateral wing (14) defines a box structure within which a roll axis (Z) of the unmanned aircraft (10) lies, said roll axis (Z) lying between the first lateral wing (14) and the second lateral wing (14), and in which at least the first and second side wings (14) are self-stabilizing wings.
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公开(公告)号：WO2020012430A3
公开(公告)日：2020-01-16
申请号：PCT/IB2019/055959
申请日：2019-07-12
Applicant: SKYPULL SA
Inventor： CATTANO, Aldo , BETTELINI, Alberto , MONA, Nicola
Abstract: Base for an unmanned aircraft comprising a support platform for said aircraft and a supporting frame adapted to space said support platform from the ground, said supporting frame comprising at least one base element; said base being characterized in that said support platform is movable with respect to said base element.
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