公开(公告)号：US10913531B2

公开(公告)日：2021-02-09

申请号：US15328611

申请日：2015-07-21

Applicant: ATMOS UAV B.V.

Inventor： Sander Hulsman ,  Jurjen De Groot ,  Maarten Milis ,  Dirk Lucas Eduard Dokter ,  Joost Leon Bouman ,  Ruud Knoops

IPC: B64C29/02 ,  B64C39/02

Abstract: An aircraft, in particular an unmanned aerial vehicle with wing-borne flight mode and hover flight mode, comprises a wing structure (4) having a left (6), middle (7), and right wing section (8). A support structure extends from the wing structure (4), and has an upper and lower support section. Each one of the left and right wing section (6, 8), and upper and lower support section (18, 20) has a thrust unit (10, 12, 22, 24). Left and right wingtip sections are rotatable relative to a left and right wing base section, respectively, around an axis extending substantially in a lengthwise direction of the wing structure. The thrust units (10,12) of the left and right wing sections(6, 8) are provided at the respective wingtip sections, in particular at the extremities thereof.

公开(公告)号：US20170217585A1

公开(公告)日：2017-08-03

申请号：US15328611

申请日：2015-07-21

Applicant: ATMOS UAV B.V.

Inventor： Sander HULSMAN ,  Jurjen DE GROOT ,  Maarten MILIS ,  Dirk Lucas Eduard DOKTER ,  Joost Leon BOUMAN ,  Ruud KNOOPS

IPC: B64C29/02 ,  B64C39/02

CPC classification number: B64C29/02 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/165

Abstract: An aircraft, in particular an unmanned aerial vehicle with wing-borne flight mode and hover flight mode, comprises a wing structure (4) having a left (6), middle (7), and right wing section (8). A support structure extends from the wing structure (4), and has an upper and lower support section. Each one of the left and right wing section (6, 8), and upper and lower support section (18, 20) has a thrust unit (10, 12, 22, 24). Left and right wingtip sections are rotatable relative to a left and right wing base section, respectively, around an axis extending substantially in a lengthwise direction of the wing structure. The thrust units (10,12) of the left and right wing sections(6, 8) are provided at the respective wingtip sections, in particular at the extremities thereof.