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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
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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
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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.
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