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Small fixed-wing unmanned aerial vehicle empennage quick disassembly and assembly mechanism and using method thereof

A technology of disassembly and assembly mechanism and fixed wing, which is applied to the fuselage, aircraft parts, aircraft control and other directions, can solve the problems of wasting time, complicated operation of the tail of the drone, and the installation is not stable enough, so as to achieve simple operation, stable installation, The effect of quick installation and removal

Active Publication Date: 2021-01-29
湖南浩天翼航空技术有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The existing small fixed-wing UAV tail quick disassembly mechanism is complicated to disassemble the UAV tail, and it takes a lot of time to waste, and the installation is not stable enough. For some special operations of UAVs, time is life, so a kind of Small fixed-wing UAV tail quick disassembly mechanism, and has a high stability mechanism after installation

Method used

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  • Small fixed-wing unmanned aerial vehicle empennage quick disassembly and assembly mechanism and using method thereof
  • Small fixed-wing unmanned aerial vehicle empennage quick disassembly and assembly mechanism and using method thereof
  • Small fixed-wing unmanned aerial vehicle empennage quick disassembly and assembly mechanism and using method thereof

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Embodiment

[0036] like Figure 1-9As shown, a small-sized fixed-wing unmanned aerial vehicle empennage quick disassembly mechanism, comprises body 1, two horizontal empennages 2, vertical empennage 5, two horizontal empennages 2 are respectively located at the both sides of airframe 1, vertical empennage 5 is located at On the top of the body 1, the vertical empennage 5 is located between the two horizontal empennages 2, and both sides of the body 1 are fixedly equipped with a first mounting block 4, and the first mounting block 4 is provided with a third groove 18, and the third groove The inner walls of both sides of 18 are symmetrically provided with draw-in slots 19, and one side of the horizontal stabilizer 2 is fixedly equipped with a fixed block 3, and a second groove 13 is provided on the fixed block 3, and an extruding rod 11 is slidably connected in the second groove 13. One side of the fixed block 3 is fixedly connected with the second mounting block 15, the second mounting bl...

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Abstract

The invention discloses a small fixed-wing unmanned aerial vehicle empennage quick disassembly and assembly mechanism and a use method thereof. The small fixed-wing unmanned aerial vehicle empennage quick disassembly and assembly mechanism comprises a vehicle body, two horizontal empennages and a vertical empennage, wherein the two horizontal empennages are located on the two sides of the vehiclebody correspondingly, and the vertical empennage is located at the top of the vehicle body and located between the two horizontal empennages; first mounting blocks are fixedly mounted on the two sidesof the vehicle body correspondingly, third grooves are formed in the first mounting blocks, clamping grooves are symmetrically formed in the inner walls of the two sides of each third groove, and a fixing block is fixedly mounted on one side of each horizontal empennage. The small fixed-wing unmanned aerial vehicle empennage quick disassembly and assembly mechanism is simple to operate and can quickly assemble and disassemble the unmanned aerial vehicle empennages, solves the problems that an existing unmanned aerial vehicle is complex in installation and needs long installation time, and wins time for special operation of the unmanned aerial vehicle; the installation mode is more stable than an existing installation mode, so that the situation that the normal operation of the unmanned aerial vehicle is affected due to the fact that the empennage loosens during work of the unmanned aerial vehicle is avoided.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a rapid disassembly and assembly mechanism for the tail of a small fixed-wing unmanned aerial vehicle and a method for using the same. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft operated by radio remote control equipment and self-provided program control devices. There is no cockpit on the plane, but it is equipped with autopilot, program control devices and other equipment. The personnel on the ground, on the ship or in the remote control station of the mother machine use radar and other equipment to track, locate, remote control, telemetry and digital transmission. It can take off like an ordinary plane under radio remote control or launch it with a booster rocket, or it can be brought into the air by the mother plane for flight. When it is recovered, it can be automatically landed in the same way as the lan...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C5/06B64C5/02B64C1/26
CPCB64C5/06B64C5/02B64C1/26
Inventor 熊哲刘明星李昌
Owner 湖南浩天翼航空技术有限公司
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