Small type fixed-wing unmanned aerial vehicle modularization load cabin device and method

A technology for load compartments and drones, applied in the field of drones, can solve the problems of long replacement cycle, inconvenient installation, and troubles, so as to save task time, facilitate quick installation, and reduce the effect of modified products

Pending Publication Date: 2018-11-23
厦门市汉飞鹰航空科技有限公司
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Problems solved by technology

In addition, the existing loads are generally installed on the body structure, and the mechanical and electrical interfaces of different loads are completely different. If the load needs to be replaced, it will be very troublesome to disassemble it in the load compartment. It is necessary to change the cabl

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  • Small type fixed-wing unmanned aerial vehicle modularization load cabin device and method
  • Small type fixed-wing unmanned aerial vehicle modularization load cabin device and method
  • Small type fixed-wing unmanned aerial vehicle modularization load cabin device and method

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Embodiment Construction

[0016] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted here that the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute conflicts with each other.

[0017] Such as Figure 1 to Figure 3 As shown, what the present invention discloses is a modularized device for a small-sized fixed-wing UAV load cabin, including a fuselage and a wing, and the lower side of its wing 2 is provided with a load cabin 3, and the load cabin 3 is for unmanned It is an independent module connected with the fuselage 1, and the load compartment 3 is modularized so that the load compartment 3 does not participate in the force transmission of the fuselage structure. The load compartment 3 is used as an independent module in conjunction with the fuselage. The structure is closed and complete. ...

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Abstract

The invention discloses a small type fixed-wing unmanned aerial vehicle modularization load cabin device which comprises a vehicle body and wings. The device is characterized in that load cabins are arranged on the lower sides of the wings, the load cabins are independent modules which are connected with the vehicle body of an unmanned aerial vehicle, loads are connected in the load cabins, and gravity centers of the connection between the loads and the load cabins are arranged in a gravity center balance range of the vehicle body of the unmanned aerial vehicle. The invention further disclosesa method based on the small type fixed-wing unmanned aerial vehicle modularization load cabin device. According to the device disclosed by the invention, the load cabins of the fixed-wing unmanned aerial vehicle are modularized, and load replacement and use can be quickly and conveniently achieved under the different situations; furthermore, when the loads are replaced, only the load cabins needto be replaced, and the gravity center positions of the load cabins are prevented from being reconfigured; thus, the device is convenient to use.

Description

technical field [0001] The invention relates to an unmanned aerial vehicle, in particular to a device and a method for modularizing the load cabin of a small fixed-wing unmanned aerial vehicle. Background technique [0002] Fixed drones are particularly sensitive to the position of the center of gravity, so the center of gravity must be recalculated and configured when the drone is reloaded with a mission load. The load platform of the existing small UAV is usually symmetrically arranged on the underside of the two wings and the center of gravity is balanced by moving the airborne equipment and the counterweight. Once the load weight changes, the counterweight needs to be re-balanced. In addition, the existing loads are generally installed on the body structure, and the mechanical and electrical interfaces of different loads are completely different. If the load needs to be replaced, it will be very troublesome to disassemble it in the load compartment. It is necessary to ch...

Claims

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Application Information

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IPC IPC(8): B64C39/02B64D47/00
CPCB64C39/02B64D47/00B64U10/25
Inventor 邓钊周伟汪延鹏
Owner 厦门市汉飞鹰航空科技有限公司
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