High-subsonic-speed invisible unmanned aerial vehicle

A subsonic, unmanned aerial vehicle technology, applied in the field of aircraft, can solve the problems of aircraft shape without considering stealth design, unable to meet special combat needs, unable to adapt to cruising speed, etc., to improve battlefield survival rate and flight stability, improve flight The effect of stability and enhanced battery life

Pending Publication Date: 2018-02-13
ZHEJIANG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the wing sweep angle of the UAV is not variable, so it cannot adapt to different cruising speeds, and the shape of the aircraft does not consider the stealth design
The folding-wing UAV disclosed in the invention patent with the application number of 201410303976.6 is in a contracted state when carried and ejected, and the wings are unfolded during flight, providing a portable folding-wing UAV with a simple and compact structure. Propelled by propellers, the flight speed is low, which cannot meet special operational requirements

Method used

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  • High-subsonic-speed invisible unmanned aerial vehicle
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  • High-subsonic-speed invisible unmanned aerial vehicle

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[0036] The present invention will be further elaborated and illustrated below in conjunction with the accompanying drawings and embodiments. The technical features of the various embodiments of the present invention can be combined accordingly without conflict with each other.

[0037] The drone can switch between the folded state and the open state.

[0038] Such as figure 1 with 2 As shown, it is an open state of a high subsonic stealth drone, which includes a body 1, a wing 2, a tail 3, and an air inlet 4. The wing 2, the tail 3 and the air inlet 4 are fixed on the body 1. The drone body adopts a stealth design. Since the radar scattering area (RCS) of the olive is lower than that of an ellipsoid or a sphere, the nose adopts an olive with an angle of 25° to the central axis. The wing 2 and the tail 3 are respectively hinged on the body 1, and the wing 2 adopts an upper single-wing layout to increase the stability of the UAV during cruise. The wing 2 is connected to the fuselage

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Abstract

The invention discloses a high-subsonic-speed invisible unmanned aerial vehicle. The high-subsonic-speed invisible unmanned aerial vehicle comprises an unmanned aerial vehicle body, foldable wings, foldable empennages and a retractable air inlet channel. The unmanned aerial vehicle is in an invisible design; the wings are in upper single wing layout, a folding mode is a rotary folding mode, and the wings are retracted towards the direction of a tail; the empennages are in V-shaped layout, and when folded, the empennages are attached to the side surfaces of the body to rotate towards the direction of the head. In order to adapt to the layouts of the wings and the empennages and facilitate placement and fixation of the wings and the empennages, the body is in integrated design, the back of the body is parallel to the horizontal plane, and dihedral angles of the side surfaces of the body are consistent to dihedral angles of the V-shaped empennages. Before the wings are unfolded, the air inlet channel retracts into the body so as to facilitate transportation and mounting. The high-subsonic-speed invisible unmanned aerial vehicle has excellent invisibility and high-subsonic-speed cruising ability; the shortcoming that a small unmanned aerial vehicle is weak in breaking through defense due to small speed is overcome, and meanwhile, more unmanned aerial vehicle can be loaded in limited carrying space of a mother aircraft.

Description

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Claims

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Application Information

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Owner ZHEJIANG UNIV
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