首页> 外国专利> GYROPENDULAR ENGINE WITH COMPENSATORY PROPULSION AND COLLIMATION OF MULTIMODAL MULTI-MEDIUM FLUID FLOWING GRADIENT WITH VERTICAL LANDING AND LANDING

GYROPENDULAR ENGINE WITH COMPENSATORY PROPULSION AND COLLIMATION OF MULTIMODAL MULTI-MEDIUM FLUID FLOWING GRADIENT WITH VERTICAL LANDING AND LANDING

机译:垂直推进和多模态多介质流梯度补偿混合的回旋式发动机

摘要

The invention relates to a device (FIG.18) device or gyropendular drone that can evolve in the following physical environments: air, land, sea, underwater or space, takeoff and vertical landing, comprising upper and lower propulsion units , provided with an annular fairing accommodating a certain number of motorizations or propellers wing or gas electronically servo, located in the extension of the axis thereof, mounted on 3D ball joints at the end of a number of telescopic rods, eg distributed at 120 ° at the periphery of the plate and orientable along the three axes according to the flight plan of the multimodal multi-media machine, a vertebral structure as a 3D articulated central body of solid cylindrical shape or hollow performing a function of stabilization, position retention and orientation, then an inertial rotating disk tray provided beneath a cockpit shaped he a spherical extension of the vertebral structure, accommodating a payload or application adapted to different fields of application, eg in the defense or civil security sector, in order to carry out search and rescue functions, exploration, navigation, transport, scene monitoring, and deployment of free-space telecommunications infrastructure.
机译:技术领域本发明涉及一种可以在以下物理环境中演化的装置(图18)装置或双螺旋形无人机:空中,陆地,海洋,水下或太空,起飞和垂直着陆,包括具有环形的上,下推进单元整流罩,可容纳一定数量的机动装置或机翼或气体电子伺服螺旋桨,位于其轴线的延长线上,安装在许多伸缩杆末端的3D球形接头上,例如以120°分布在板的外围并根据多模式多媒体机器的飞行计划沿三个轴定向,椎骨结构为3D铰接的实心圆柱或中空中心体,具有稳定,位置保持和定向的功能,然后是惯性旋转盘托盘设置在座舱下方,其形状为椎骨结构的球形延伸部分,可容纳有效载荷或适用于不同领域的应用应用,例如在国防或民安部门,以执行搜索和救援功能,探索,导航,运输,场景监视以及自由空间电信基础设施的部署。

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