Solar multi-axis unmanned aerial vehicle structure without self-weight energy consumption

A technology of unmanned aerial vehicles and solar energy, applied in the field of unmanned aerial vehicles, can solve the problems of unmanned aerial vehicles such as poor battery life, easy damage, poor controllability, etc., and achieve the effect of large wind resistance operation ability, ensuring safety and reducing costs

Pending Publication Date: 2020-12-15
毛雷杰
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The technical problem to be solved by the present invention is to overcome the defects of the prior art, provide a multi-axis unmanned aerial vehicle structure with solar energy and no self-weight and energy consumption, a

Method used

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  • Solar multi-axis unmanned aerial vehicle structure without self-weight energy consumption
  • Solar multi-axis unmanned aerial vehicle structure without self-weight energy consumption
  • Solar multi-axis unmanned aerial vehicle structure without self-weight energy consumption

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Embodiment 1

[0023] Such as Figure 1-4 As shown, the present invention provides a multi-axis unmanned aerial vehicle structure with no self-weight and energy consumption of solar energy, including an unmanned aerial vehicle structure 1, an airship 2 connected to the top of the unmanned aerial vehicle structure 1, and a fixed connection to the bottom of the unmanned aerial vehicle structure 1. In the equipment compartment 3, a plurality of cantilevers 4 are connected to the outside of the UAV structure 1, a drive motor 5 is fixed at one end of the cantilever 4, a drive shaft 6 is connected to the top of the drive motor 5, and a rotor 7 is connected to the top of the drive shaft 6. 2. A secondary airbag 9 is provided in the center of the interior, and a main airbag 10 is provided on the outside of the secondary airbag 9. A suspension cord 12 is provided on the top surface of the airship 2, and a suspension cable 13 is provided between the suspension cord 12 and the UAV structure 1. , the ce...

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Abstract

The invention discloses a solar multi-axis unmanned aerial vehicle structure without self-weight energy consumption, which comprises an unmanned aerial vehicle structure body. An airship is connectedto the top of the unmanned aerial vehicle structure body, an equipment cabin is fixedly connected to the bottom of the unmanned aerial vehicle structure body, a plurality of cantilevers are connectedto the outer side of the unmanned aerial vehicle structure body, and driving motors are fixed to one ends of the cantilevers. The tops of the driving motors are connected with driving shafts, the topends of the driving shafts are connected with rotor wings, an auxiliary airbag is arranged in the center in the airship, a main airbag is arranged on the outer side of the auxiliary airbag, suspensionwire cord fabric is arranged on the surface of the top end in the airship, and a suspension cable is arranged between the suspension wire cord fabric and the unmanned aerial vehicle structure body. The unmanned aerial vehicle technology and the airship structure are combined, the buoyancy of the airship can counteract the gravity of the unmanned aerial vehicle, solar energy and the airship, a whole aircraft is suspended at the fixed position in air under zero gravity, and the safety of the aircraft is guaranteed.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a multi-axis unmanned aerial vehicle structure with solar energy and no self-weight energy consumption. Background technique [0002] With the rapid development of drone technology, various power and multi-axis drones are equipped with various technical modules, which play a role in military and people's livelihood in various scenarios, but battery life and vulnerability restrict the application and development of drones. Most of the energy of the existing drone technology is consumed against its own weight, which also affects the carrying range of the functional equipment of the drone. If the UAV encounters mechanical failure and battery low temperature loss, it is easy to fall directly and be directly destroyed. No matter what type of existing drones, they all face these two shortcomings. As for the airship or the floating air balloon, the existing technology...

Claims

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Application Information

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IPC IPC(8): B64B1/06B64B1/58B64C27/08B64C27/12B64D27/24
CPCB64B1/06B64B1/58B64C27/08B64C27/12B64D27/24
Inventor 毛雷杰
Owner 毛雷杰
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