Fixed-wing fuel-cell unmanned aerial vehicle for plant protection

A technology for planting and protecting drones and fuel cells, applied in rotorcraft, unmanned aerial vehicles, wings, etc., can solve the problems of many battery replacements, single power source, insufficient safety performance, etc., to ensure the spraying effect, Optimize the wing structure and spray reasonably and effectively

Active Publication Date: 2017-09-19
HUBEI UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The unmanned aerial vehicle in the prior art includes a fuselage, a rotor and a camera platform. At the same time, a flight control system is also provided inside the fuselage. The unmanned aircraft used for agricultural, forestry and plant protection operations can be controlled by ground remote control or GPS flight control. To realize the spraying operation, but the existing drones are generally powered by lithium batteries, and the battery needs to be replaced every 15 minutes on average. Inefficiency is a major defect in the popularization and application of existing plant protection drones, and further improvement is still needed in actual engineering applications
[0003] Chinese utility model patent application (publication date: August 31, 2016, publication number: CN 205524959U) discloses a fuel cell drone, including a fuel cell system, a frame, a flight lifting component, and a control mechanism. The battery system provides power for the fuel cell UAV, which improves the endurance to a certain extent, and the wind generated by the propeller dissipates heat for the fuel cell system, but the power source is single, only the fuel cell system provides power, and the dynamic response capability is poor , there are problems of slow start, difficulty in meeting the requirements of fast climb and special flight, and insufficient safety performance

Method used

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  • Fixed-wing fuel-cell unmanned aerial vehicle for plant protection
  • Fixed-wing fuel-cell unmanned aerial vehicle for plant protection
  • Fixed-wing fuel-cell unmanned aerial vehicle for plant protection

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Embodiment Construction

[0025] The present invention will be further described in detail below with reference to the drawings and specific embodiments.

[0026] Such as figure 1 and figure 2 As shown, the fixed-wing fuel cell plant protection UAV of the present invention includes a fuselage bottom plate 32, a fuselage 14 mounted on the fuselage bottom plate 32, a nose connected to the fuselage 14, and a lower part of the front section of the fuselage 14. Front frame 4, first wing plate 19 and second wing plate 22 symmetrically installed on both sides of the middle section of fuselage 14, first rear frame 9 and second rear frame 13 symmetrically installed on the lower part of the rear section of fuselage 14 And the tail wing installed at the tail of the fuselage 14, the lower ends of the first wing plate 19 and the second wing plate 22 are both installed with a rotor motor 8. The output shaft of the rotor motor 8 is installed with a rotor 6 and the lower end of the nose 1 passes through a camera bracket ...

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Abstract

The present invention relates to the field of unmanned aerial vehicles, and discloses a fixed-wing fuel-cell unmanned aerial vehicle for plant protection. The fixed-wing fuel-cell unmanned aerial vehicle comprises a fuselage baseplate, a fuselage, a nose, a front frame, wings, a rear frame and empennages. A hydrogen cylinder, a fuel cell, a direct current converter, an electronic governor, an accumulator and a controller are sequentially mounted on the fuselage baseplate. The hydrogen cylinder is fixed to the fuselage baseplate through a hydrogen cylinder base; the fuel cell is connected with the hydrogen cylinder through a hydrogen pipeline, and the output end of the direct current converter is electrically connected with the accumulator, the controller and the electronic governor through a wire after being subjected to voltage conversion by the direct current converter; a pesticide box is arranged below the fuselage and connected with a water pump through a pipeline; and the outlet of the water pump communicates with multiple nozzles through a multi-pass joint and a pipeline. After the fixed-wing fuel-cell unmanned aerial vehicle for plant protection is started, the accumulator is cut off, the fuel cell supplies power for each piece of equipment of the system independently, the flight time is long, the spraying efficiency is high, and cleanness, environmental protection, safety and stability are realized.

Description

Technical field [0001] The invention relates to the field of unmanned aerial vehicles, in particular to a fixed-wing fuel cell plant protection unmanned aerial vehicle. Background technique [0002] The drones in the prior art include a fuselage, a rotor, and a camera pan / tilt. At the same time, the fuselage is also equipped with a flight control system. The drone is used for agricultural, forestry and plant protection operations. It is controlled by ground remote control or GPS. To realize the spraying operation, the existing drones generally use lithium batteries to supply power. The battery needs to be replaced every 15 minutes on average. The battery life is poor, which makes the drones have many battery replacements during the operation and the operation is troublesome, resulting in spraying. Low efficiency is a major defect in the popularization and application of existing plant protection drones, and further improvements are still needed in actual engineering applications....

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D1/18B64D27/24B64D47/08B64C3/28B64C9/00B64C27/22A01M7/00
CPCA01M7/0042A01M7/005A01M7/0089B64C3/28B64C9/00B64C27/22B64D1/18B64D27/24B64D47/08B64C2009/005B64U10/00B64U50/19B64U2101/00Y02T90/40
Inventor 全睿刘光银周未王雷杨光友
Owner HUBEI UNIV OF TECH
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