Unmanned aerial vehicle with high glide ratio fuselage

A technology of drones and fuselages, applied in the field of drones, can solve problems that affect the application of drones and weaken the performance of drones, and achieve the effects of improving gliding efficiency, enhancing performance, and expanding the scope of application

Inactive Publication Date: 2019-04-05
东莞市光点电子科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

UAVs under the existing technical conditions often do not have a fuselage designed with a high glide ratio. The disadvantage of low glide ratio greatly weakens the performance of UAVs and affects the application of UAVs in various industries.

Method used

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  • Unmanned aerial vehicle with high glide ratio fuselage
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  • Unmanned aerial vehicle with high glide ratio fuselage

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Embodiment Construction

[0020] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, a clear and complete description will be made below in conjunction with the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, and Not all examples. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0021] Such as Figure 1-Figure 5 As shown, a UAV with a fuselage with a high glide ratio includes a fuselage 1, and wings 2 are symmetrically fixed on both sides of the fuselage 1, and a beam 5 is arranged in the middle of the wing 2. The structure of the beam 5 is integral, and the beam 5 The length is the sum of the length of the wing 2 and the width of the fuselage 1. The beam 5 is symmetric...

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Abstract

The invention relates to an unmanned aerial vehicle with a high glide ratio fuselage. The unmanned aerial vehicle includes the fuselage, wings are symmetrically fixed on both sides of the fuselage, across beam is arranged in the middles of the wings, the cross beam is symmetrically fixed to the fuselage, the wings are shaped like narrow trapezoids, flanges are arranged at the roots of the wings,the wings are made of carbon fiber, the sections of the wings are shaped like long narrow water drops that are asymmetrical up and down, the insides of the wings are of hollow structures, stiffening rib plates are arranged inside the wings, the wingspan length of the wings is proportional to the width, near the fuselage, of the wings, and the trailing edges of the wings are provided with flaps. The unmanned aerial vehicle with the high glide ratio fuselage has the beneficial effects that the integral cross beam, the wings made of the carbon fiber material and the excellent internal and external structure design are adopted, so that the ratio of the wingspan length of the wings to the width, close to the fuselage, of the wings can be increased, that is, the unmanned aerial vehicle with thehigh glide ratio fuselage structure is obtained, and the glide efficiency of the unmanned aerial vehicle is improved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, and more specifically, relates to an unmanned aerial vehicle with a fuselage with a high glide ratio. Background technique [0002] Unmanned aircraft, referred to as "unmanned aerial vehicle", or "UAV" in English, is an unmanned aircraft that is controlled by radio remote control equipment and its own program control device, or is completely or intermittently operated autonomously by an on-board computer. According to the application field, UAV can be divided into military and civilian. In terms of military use, UAVs are divided into reconnaissance aircraft and target aircraft. In terms of civilian use, the application of UAVs in the industry is the real rigid demand of UAVs. At present, it is widely used in aerial photography, agriculture, plant protection, miniature selfies, express delivery, disaster relief, observation of wild animals, monitoring of infectious diseases, surv...

Claims

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Application Information

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IPC IPC(8): B64C39/02B64C3/14B64C3/18B64C5/02B64C5/06B64C23/06
CPCB64C3/14B64C3/182B64C5/02B64C5/06B64C23/065B64C39/02B64U10/25Y02T50/10
Inventor吴光润
Owner东莞市光点电子科技有限公司