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High-performance small plateau unmanned reconnaissance aerial vehicle

An unmanned reconnaissance aircraft, high-performance technology, applied in the field of unmanned reconnaissance, can solve the problems of reducing the use efficiency and loss of unmanned aerial vehicles, and achieve the effect of solving plateau use inadaptability, easy portability, and quick disassembly and assembly

Active Publication Date: 2016-08-10
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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  • High-performance small plateau unmanned reconnaissance aerial vehicle
  • High-performance small plateau unmanned reconnaissance aerial vehicle
  • High-performance small plateau unmanned reconnaissance aerial vehicle

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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 aerial vehicle which comprises an airframe. The airframe is provided with a tail rod, a middle wing, a left outer wing, a right outer wing, a horizontal tail, an undercarriage, a reconnaissance device and a parachute cabin cover. The middle wing, the left outer wing and the right outer wing are located on the same horizontal line, a tail rod wing is connected with the airframe in a threaded mode, the wings are high lift airfoils improved based on S1223 airfoils and have a high lift coefficient needed for flight on a plateau, the horizontal tail is connected with the tail rod through a clamping spring, the undercarriage is connected with the airframe through a clamping spring, and the parachute cabin cover is connected with the airframe through a clamping spring. A power supply battery, a flight control system, a reconnaissance system, an image position calculation system, an image data transmission system and a parachute landing system are arranged in the airframe. The high-performance small plateau unmanned reconnaissance aerial vehicle has the advantages that the aerial vehicle can take off and be recycled under limited conditions, and the requirements on quick reconnaissance are met.

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 Applications(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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