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Multi-bin type minitype container quadrotor transporting unmanned aerial vehicle

A container-type, micro-miniature technology, applied in the field of drones, can solve the problems of affecting the flight status of the aircraft, the position of the cargo is not fixed, and the center of gravity of the aircraft is affected, so as to achieve the effect of making full use of the effective space and improving the transportation efficiency

Inactive Publication Date: 2018-01-19
XIAMEN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The cargo compartment of a traditional quadrotor transport drone or the manipulator for fixing cargo is located in the middle and lower part of the fuselage and in the middle of the landing gear. Due to the limited space in the middle of the landing gear, the amount of cargo that can be loaded is limited; and too high The landing gear will increase the instability of the aircraft when it lands, and at the same time affect the flight status of the aircraft; the position of the cargo in the traditional box-type warehouse is not fixed, which affects the center of gravity of the aircraft on the one hand, and on the other hand, the shaking and collision during the flight may cause damaged goods

Method used

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  • Multi-bin type minitype container quadrotor transporting unmanned aerial vehicle
  • Multi-bin type minitype container quadrotor transporting unmanned aerial vehicle
  • Multi-bin type minitype container quadrotor transporting unmanned aerial vehicle

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Embodiment Construction

[0020] The following embodiments will further illustrate the present invention in conjunction with the accompanying drawings.

[0021] see Figure 1~4 The embodiment of the present invention is provided with a fuselage 1, a loading compartment 2, a cross-shaped revolving compartment door 3, a container 6, a steering gear 7, a connecting buckle 8, a battery compartment 9, a card slot 13 and an inner compartment body 14; The fuselage 1 is centrally symmetrical, and 4 adjacent two-to-two connections are installed between the 4 shafts of the fuselage 1 to form a whole detachable loading compartment 2, which is fixed to the middle loading compartment of the fuselage 1. A steering gear 7 below the 2 controls the opening and closing of the 4 cross-shaped revolving doors 3; the container 6 is arranged in the loading compartment 2, and there are 4 loading compartments 2, and 4 adjacent ones are detachable. The loading compartment 2 is connected to form an overall structure; the cross-...

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Abstract

The invention relates to unmanned aerial vehicles, in particular to a multi-bin type minitype container quadrotor transporting unmanned aerial vehicle. By utilizing the characteristic of a quadrotor plane that an enough usable space is left between every two adjacent shafts, four detachable cargo bins which are connected in pairs to form a whole are mounted among four shafts of a vehicle body, andopening and closing of the four bin doors are controlled through a steering engine fixed to the position below a small storage warehouse in the middle of the vehicle body. In this way, the transporting efficiency of the quadrotor transporting plane is improved greatly, the effective space of the plane is utilized sufficiently, and the transporting unmanned aerial vehicle has the characteristic ofbeing stable in structure. Meanwhile, container type transporting is adopted, four minitype containers can be transported through one time flying, and the minitype containers can be loaded with different cargos.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle, in particular to a multi-compartment micro-miniature container-type four-rotor transport unmanned aerial vehicle. Background technique [0002] The cargo compartment of a traditional quadrotor transport drone or the manipulator for fixing cargo is located in the middle and lower part of the fuselage and in the middle of the landing gear. Due to the limited space in the middle of the landing gear, the amount of cargo that can be loaded is limited; and too high The landing gear will increase the instability of the aircraft when it lands, and at the same time affect the flight status of the aircraft; the position of the cargo in the traditional box-type warehouse is not fixed, which affects the center of gravity of the aircraft on the one hand, and on the other hand, the shaking and collision during the flight may cause damaged goods. [0003] Chinese patent CN106275413A discloses a logistics transport...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02B64D1/22
Inventor 郭立军刘珺杨忠琴宁静
Owner XIAMEN UNIV
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