Remote control parachute

A parachute and parachute technology, applied in the field of remote control parachutes, can solve problems such as increased economic and property losses, damage to spacecraft, and inability to actively control the parachute's descending trajectory, thereby reducing unnecessary economic losses and improving accuracy.

Active Publication Date: 2017-02-08
DALIAN UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although parachutes have been widely used in various fields, the current application level cannot realize the active control of the parachute descent trajectory, and the accuracy of the parachute drop point cannot be guaranteed
Especially when recovering a spacecraft, if it encounters windy weather, it will directly cause the spacecraft to deviate from the scheduled landing point by dozens or even hundreds of kilometers; if it encounters complex terrain environments, such as jungles, mountains, waters, etc., it may directly Damage to the spacecraft will bring great difficulties to search and recovery, and the resulting economic and property losses will also greatly increase

Method used

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Examples

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Embodiment Construction

[0014] The present invention will be further described below in conjunction with accompanying drawing.

[0015] like figure 1 , 2 , 3, a remote-controlled parachute mainly includes a canopy 2, an umbrella rope 6, a load 7 and a remote control 8, and the inner wall of the canopy 2 is equipped with 4N umbrella ribs 3 evenly and symmetrically distributed, and N is a natural positive integer One end of the 4N umbrella ribs 3 is fixedly connected to one end of the 4N umbrella ropes 6 respectively, and the other end of the 4N umbrella ropes 6 is fixedly connected to the load 7 respectively, and the top of the umbrella cover 2 is equipped with a flight control main board 1 , every N umbrella ribs 3 on the canopy 2 are provided with 4 rectangular holes 4 that are evenly and symmetrically distributed and of the same size, and 4 hard holes 4 with arc shapes that are evenly and symmetrically distributed are arranged on the inner wall of the canopy 2 . The hard flat plate 5 is fixed wit...

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PUM

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Abstract

The invention relates to the technical field of aircraft design, and discloses a remote control parachute. The remote control parachute mainly comprises a load, parachute cords, a parachute canopy and a remote controller, wherein rectangular holes are formed in the parachute canopy. An operator sends out a remote control instruction based on an error between the current position of the parachute and the target landing point of the parachute; a flight control mainboard receives the remote control instruction and sends out a baffle rotation angle instruction to a stepper motor; and then the stepper motor drives a baffle to adjust the opening degree of the holes so as to control the descending trajectory of the parachute. According to the remote control parachute disclosed by the invention, the accuracy of landing points of the parachute can be significantly improved, and unnecessary economic loss caused by the situation that the landing points of traditional parachutes cannot be controlled is reduced; and besides, in the process of changing the descending trajectory of the parachute, only a small-power electric source enabling the stepper motor to drive the baffle needs to be provided, and other power does not need to be used, so that the remote control parachute is both economic and environment-friendly.

Description

technical field [0001] The invention relates to a remote control parachute, which belongs to the technical field of aircraft design. Background technique [0002] The working principle of the parachute is that after the parachute is opened at a certain height, due to the action of the airflow and the inner wall of the canopy, the canopy will open rapidly, and the descending speed will continue to increase. With the continuous increase of air resistance, its descending speed decreases, and gradually reaches the equilibrium speed until a safe landing is achieved. Although parachutes have been widely used in various fields, the current application level cannot realize the active control of the parachute descent trajectory, and the accuracy of the parachute drop point cannot be guaranteed. Especially when recovering a spacecraft, if it encounters windy weather, it will directly cause the spacecraft to deviate from the scheduled landing point by dozens or even hundreds of kilome...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D17/00B64D17/18B64D17/34B64D17/80
CPCB64D17/00B64D17/18B64D17/34B64D17/80
Inventor 周文雅余兴林战俊杰阮政委
Owner DALIAN UNIV OF TECH
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