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Automatic parachute opening device for unmanned aerial vehicle

An unmanned aerial vehicle, automatic technology, applied in the direction of parachute, aircraft parts, transportation and packaging, can solve the problems of complex control mechanism, insensitive response, the umbrella canopy cannot be opened smoothly, etc., to achieve rapid response, simple structure, Easy-to-use effects

Pending Publication Date: 2020-04-07
AEROSPACE SHENZHOU AIRCRAFT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The opening of the traditional umbrella canopy is mostly controlled by the steering gear and the transmission mechanism. The control mechanism is complicated, and it is prone to problems such as insensitive response and the canopy can not be opened smoothly.

Method used

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  • Automatic parachute opening device for unmanned aerial vehicle
  • Automatic parachute opening device for unmanned aerial vehicle
  • Automatic parachute opening device for unmanned aerial vehicle

Examples

Experimental program
Comparison scheme
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Embodiment Construction

[0022] Below, the present invention will be further described in conjunction with the accompanying drawings and specific implementation methods. It should be noted that, under the premise of not conflicting, the various embodiments described below or the technical features can be combined arbitrarily to form new embodiments. .

[0023] refer to figure 1 , figure 2 , image 3 , Figure 4 and Figure 5 . The embodiment of the present invention provides an automatic parachute opening device for unmanned aerial vehicles, which includes an umbrella cabin 1, an umbrella cabin cover 2, a detonator 3 and a ratchet mechanism 4. The ratchet mechanism 4 is installed on the outer wall of the umbrella cabin 1, and the umbrella cabin cover One end of 2 is inserted on the inner wall of umbrella cabin 1, and the other end of umbrella cabin cover 2 is connected with nylon rope 5, and the end of nylon rope 5 is connected with ratchet mechanism 4, and ratchet mechanism 4 is used for tensio...

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PUM

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Abstract

The invention discloses an automatic parachute opening device for an unmanned aerial vehicle. The device comprises a parachute bay, a parachute bay cover, a detonator and a ratchet mechanism, whereinthe ratchet mechanism is installed on the outer wall of the parachute bay, one end of the parachute bay cover is inserted into the inner wall of the parachute bay, the other end of the parachute bay cover is connected with a nylon rope, the tail end of the nylon rope is connected with the ratchet mechanism, the ratchet mechanism is used for tensioning the nylon rope, and the detonator sleeves thenylon rope and is connected with a power supply and a flight control module. The automatic parachute opening device for the unmanned aerial vehicle is sensitive and rapid in response, opening of the parachute bay cover and unfolding of the recovery parachute can be rapidly and reliably achieved, and safe recovery of the unmanned aerial vehicle is guaranteed.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicle accessories, in particular to an automatic parachute opening device for an unmanned aerial vehicle. Background technique [0002] The recovery methods of drones mainly include parachute recovery, air recovery, arresting net recovery, landing gear roll recovery and air cushion landing recovery. Compared with other recovery methods, parachute recovery has the characteristics of wide application range, high cost performance, small size, light weight, and no need for a wide and flat special landing site, so it is widely used in the recovery of drones. Using the parachute recovery method, how to ensure the smooth opening of the parachute becomes the key to the safe recovery of the drone. [0003] The recovery umbrella is located in the umbrella cabin and is covered by the umbrella cabin cover. When the drone is recovered, the umbrella cabin cover is opened, and the guide umbrella is pulled out, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D17/72
CPCB64D17/725
Inventor 龙文彪周洪
Owner AEROSPACE SHENZHOU AIRCRAFT
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