公开(公告)号：WO2017130137A1

公开(公告)日：2017-08-03

申请号：PCT/IB2017/050422

申请日：2017-01-26

Applicant: OPENSTRATOSPHERE SA

Inventor： BROWN, Dave ,  JOHNSON, Simon ,  TISCHHAUSER, Frederick

IPC: B64C39/02 ,  B64D27/24

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2211/00 ,  B64D27/24 ,  B64D2211/00 ,  Y02T50/44 ,  Y02T50/62

Abstract: A stratospheric drone able to operate at an altitude between 17 km and 23 km(ISA), said stratospheric drone comprising: one fuselage; at least two wings; at least one tail;at least two motors and two corresponding propellers; at least one accumulator in each of said wings, so as to partly compensate the lift force on said wings with the weight of the accumulators in said wings; a payload pod at the front of the fuselage, for housing a removable payload,wherein the structure of the drone is designed and optimized for transporting a payload having a maximal mass between 20 and 50 kg.

Abstract translation: 平流层无人机能够在17公里和23公里之间的高度运行（ISA），所述平流层无人机包括：一个机身; 至少两个翅膀; 至少一个尾部;至少两个电机和两个相应的螺旋桨; 在每个所述机翼中至少有一个蓄能器，以便利用所述机翼中蓄能器的重量部分地补偿所述机翼上的升力; 机身前部的有效载荷舱，用于容纳可移动的有效载荷，其中无人驾驶飞机的结构被设计和优化用于运输最大质量在20和50kg之间的有效载荷。