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Supersonic-speed mute unmanned aerial vehicle pneumatic layout

An aerodynamic layout and UAV technology, applied in the direction of wing adjustment

Active Publication Date: 2018-09-28
CHINA ACAD OF AEROSPACE AERODYNAMICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] From the perspective of the speed development of UAVs, a large number of UAVs successfully developed are concentrated in the low-speed and subsonic ranges, and there are still vacancies for hypersonic UAVs flying in space.

Method used

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  • Supersonic-speed mute unmanned aerial vehicle pneumatic layout
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  • Supersonic-speed mute unmanned aerial vehicle pneumatic layout

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Embodiment Construction

[0029] Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. Although exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided for more thorough understanding of the present disclosure and to fully convey the scope of the present disclosure to those skilled in the art. It should be noted that, in the case of no conflict, the embodiments of the present invention and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0030] figure 1 It is the outline drawing of the supersonic silent UAV provided by the embodiment of the present invention; figure 2 It is the front view o...

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Abstract

The invention discloses a supersonic-speed mute unmanned aerial vehicle pneumatic layout which comprises a nose, two canards, an edge strip, two wings, an air inflow channel, a fuselage and two empennages. The nose is connected with the front end of the fuselage, the nose is a conical-similar hollow barrel, the area near a head peak of the nose is warped upwards, and the whole nose has a downwardinclination angle. The two canards are arranged on the two sides of the nose. The edge strip and the fuselage are fused, and the edge strip is located on the rear portion of the nose. The two wings are arranged on the two sides of the fuselage and located on the rear portion of the edge strip. The air inflow channel is formed in the back face of the fuselage, and the air inflow channel is locatedon the rear portion of the wings. The two empennages are arranged on the two sides of the fuselage and located at the tail end of the fuselage. The problem that an aerospace flight high-supersonic-speed unmanned aerial vehicle is not available is solved.

Description

technical field [0001] The invention belongs to the field of aerodynamic layout design of unmanned aerial vehicles, and in particular relates to an aerodynamic layout of a supersonic silent unmanned aerial vehicle. Background technique [0002] In the Afghan operations from 2001 to 2002, the U.S. Predator UAV carried out the strike mission for the first time, becoming a milestone in the history of UAV development. During the Iraq War in 2003, the U.S. military deployed and used about 90 drones, mainly responsible for tactical reconnaissance, battlefield patrol and special target attack missions. U.S. drones played an important role in the air strikes on Libya. With the rapid development of high-tech military technology, unmanned military equipment has penetrated into almost every field of battlefield space. Unmanned aerial vehicles have become an important and even key force affecting the combat process and have been valued by more and more countries. The military departmen...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/40
CPCB64C3/40
Inventor 王斌孟军郭少杰张旭岳良明
Owner CHINA ACAD OF AEROSPACE AERODYNAMICS