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A high-performance small plateau unmanned reconnaissance aircraft

An unmanned reconnaissance aircraft, high-performance technology, applied in the field of unmanned reconnaissance, can solve the problems of loss, reduce the use efficiency of unmanned aerial vehicles, etc., achieve the effect of easy portability, unsuitable use on plateaus, and quick disassembly and assembly

Active Publication Date: 2018-06-08
GUANGZHOU TIAN HAI XIANG AVIATION TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Now, drones are widely used, such as aerial photography, rescue, inspection, monitoring, surveying and mapping, reconnaissance, film and television shooting, news reports, express transportation and other fields, but many drones encounter bad weather. Losing his role will greatly reduce the efficiency of drone use. In order to reduce the occurrence of such things, it is necessary to set up this device

Method used

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  • A high-performance small plateau unmanned reconnaissance aircraft
  • A high-performance small plateau unmanned reconnaissance aircraft
  • A high-performance small plateau unmanned reconnaissance aircraft

Examples

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Embodiment Construction

[0020] The present invention is specifically described below in conjunction with accompanying drawing, as Figure 1-4 Shown, a kind of high-performance small plateau unmanned reconnaissance aircraft comprises aircraft fuselage (1), and described aircraft fuselage (1) is provided with tail boom (2), middle wing (3), left outer wing (4 ), right outer wing (5), horizontal stabilizer (6), landing gear (7), reconnaissance device (8) and canopy cover (9), described center wing (3), left outer wing (4) and right Outer wing (5) is positioned at same horizontal line, and described middle wing (3), left outer wing (4) right outer wing (5) are positioned at tail boom (2) front side, and described horizontal tailplane (6) is positioned at tail boom ( 2) above, the landing gear (7) is located below the aircraft fuselage (1), the detection device (8) is located at the front side of the aircraft fuselage (1), and the tail boom (2) is located at the aircraft fuselage (1) ) rear side, the can...

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Abstract

The invention discloses a high-performance small plateau unmanned reconnaissance aircraft. and the umbrella canopy, the middle wing, the left outer wing and the right outer wing are located on the same horizontal line, the tail boom wing is connected to the aircraft fuselage by threads, and the wing adopts the high-lift airfoil improved from the S1223 airfoil , with a high lift coefficient required for plateau flight, the horizontal tail is connected to the tail boom through a circlip, the landing gear is connected to the aircraft fuselage through a circlip, and the umbrella canopy is connected to the aircraft fuselage through a The airframe is connected by means of a circlip, and the fuselage of the aircraft is equipped with a power supply battery, a flight control system, a reconnaissance system, an image position calculation system, an image data transmission system, and a parachute system. The beneficial effect of the invention is that it can quickly take off and recover under limited conditions, so as to meet the requirements of fast investigation.

Description

technical field [0001] The invention relates to the field of unmanned reconnaissance, in particular to a high-performance small plateau unmanned reconnaissance aircraft. Background technique [0002] Now, drones are widely used, such as aerial photography, rescue, inspection, monitoring, surveying and mapping, reconnaissance, film and television shooting, news reports, express transportation and other fields, but many drones encounter bad weather. Losing his role will greatly reduce the efficiency of the drone. In order to reduce the occurrence of such things, it is necessary to set up this device. Contents of the invention [0003] The purpose of the present invention is in order to solve the problems referred to above, has designed a kind of high-performance small plateau unmanned reconnaissance aircraft. [0004] Achieving the above object The technical solution of the present invention is, a high-performance small plateau unmanned reconnaissance aircraft, comprising a...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/30B64C39/02
CPCB64C1/30B64C39/02B64U10/25B64U2101/30
Inventor 李裕壮王林林
Owner GUANGZHOU TIAN HAI XIANG AVIATION TECH
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