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Rapidly-opened parafoil structure and opening method thereof

A parafoil and fast technology, applied in parachute, emergency equipment, weight reduction, etc., can solve the problems of poor inflation conditions, blocked air chamber inflation, hidden dangers, etc., and achieve the effect of low cost, good safety, and reduced usage

Pending Publication Date: 2022-06-03
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when the parafoil is ready to open after being thrown out from the aircraft cabin, the folded shape hinders the inflation of the air chambers, especially the air chambers on both sides. Because of the constraints of the control ropes, the inflation conditions are worse, which often leads to the parafoil opening time being too long However, if the parafoil cannot be inflated quickly, the parafoil will not be able to fly normally or even stall, which will bring safety hazards

Method used

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  • Rapidly-opened parafoil structure and opening method thereof
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  • Rapidly-opened parafoil structure and opening method thereof

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Embodiment Construction

[0016] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0017] The present invention provides an auxiliary device for quickly opening a parafoil, such as the attached Figure 1-8 As shown, it includes a pressure relief valve 1, a wing rib 2, an umbrella rope 3, a rapid inflation channel 4, a load 5, a rapid inflation device 6, an exhaust pipe 7, a sealing film 8, and a small liquid nitrogen bottle 9.

[0018] The wing rib 2 is a bearing rib, and the lower end is connected with a paracord 3...

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Abstract

The invention provides a parafoil structure capable of being quickly opened and an opening method thereof. The parafoil structure comprises a hollow cavity with the front edge open and the rear edge sealed, the center of the cavity is divided into a plurality of air chambers through wing ribs, vent holes are formed in the wing ribs, and the lower ends of the wing ribs are connected with parafoil cords; the left end and the right end of the cavity are connected with inflation channels in a fully-closed state, the inflation channels are connected with the adjacent air chambers through pressure release valves, and inflation devices and deflation valves are arranged in the inflation channels. The parafoil inflating structure provided by the invention can help the parafoil to quickly form an inflating opening state for normal sliding of the parafoil after the parafoil is thrown out of an aircraft cabin, so that the air-drop safety of the parafoil is ensured.

Description

technical field [0001] The invention relates to the field of parafoil opening devices, in particular to an auxiliary device and an opening method for rapidly opening a parafoil. Background technique [0002] A parafoil is a kind of parachute that can glide and fly in the air. Whether it is for leisure, entertainment, commercial use, long-distance delivery, aerospace, etc., parafoils have been widely used. The airfoil of the commonly used inflatable parafoil is formed by using the initial speed and falling speed of the parafoil after the parafoil is thrown from the aircraft cabin to inflate the air chamber against the wind, and the parafoil canopy becomes a flying wing, thereby Can glide in the air. However, when the parafoil is ready to be opened after being thrown from the aircraft cabin, the folded shape hinders the inflation of the air chambers, especially the air chambers on both sides. Because of the constraints of the control rope, the inflation conditions are worse, ...

Claims

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Application Information

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IPC IPC(8): B64D17/72
CPCB64D17/72Y02T50/40
Inventor 宋佳蓉赵敏姚敏蒋宇鸿冯玲华武意棋
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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