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High-altitude airship

A technology of airship and skin, which is applied in the field of airship and can solve problems such as wrinkles, air bubbles, and adverse effects on the skin performance of high-altitude airships

Active Publication Date: 2014-02-19
LIYANG TECH DEV CENT
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The multi-layers of existing high-altitude airship skins are usually combined with each other by hot-melt coating technology or coating rollers or by film bonding. However, since the thickness of each layer of film is generally very thin, Therefore, the precision requirements for the above-mentioned processes are very high, but defects such as bubbles or wrinkles still often inevitably appear, which also adversely affects the performance of the manufactured high-altitude airship skin

Method used

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Embodiment Construction

[0010] The skin of the high-altitude airship according to the invention comprises a weather-resistant layer, a primer layer, a load-bearing layer, an adhesive layer, a helium-blocking layer and a heat-sealing layer sequentially from outside to inside. The heat-sealing layer is polyurethane film, the helium barrier layer is aluminum-plated polyester (Al-PET) film, the adhesive layer is polycarbonate, the load-bearing layer is PBO plain fabric, and the primer layer is two-component epoxy polyamide. The weather-resistant layer is nano-fluorocarbon coating. Preferably, the thickness of the heat-sealing layer is 15 microns; the helium barrier layer is based on a PET film, and a thin and dense metal aluminum film is deposited on it by a magnetron sputtering process, and the surface density of the substrate PET film is 60g / m 2 , the thickness of the aluminum coating is 70 nanometers, the thickness of the helium barrier layer is 37 microns, the thickness of the bonding layer is 15 m...

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PUM

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Abstract

The invention relates to a high-altitude airship which comprises an airship envelope, wherein the envelope sequentially comprises a weather-resistant layer, a primer layer, a load-bearing layer, a bonding layer, a helium-barrier layer and a heat-sealing layer from outside to inside, wherein the heat-sealing layer is a polyurethane; the helium-barrier layer adopts an aluminized polyester (Al-PET) film; the bonding layer is polycarbonate; the load-bearing layer adopts a PBO plain cloth; the primer layer is double-component epoxy polyamide; and the weather-resistant layer is a nano fluorocarbon paint. The nano fluorocarbon paint enhances the self-cleaning effect, ultraviolet resistance and environmental protection capacity of the weather-resistant layer, and greatly enhances the weather resistance of the airship envelope. The invention also relates to a manufacturing method of the airship envelope.

Description

technical field [0001] The invention relates to an airship, in particular to a high-altitude (stratospheric) airship. Background technique [0002] The high-altitude airship is a new type of near-space multifunctional flying platform developed with the continuous development of science and technology. It is different from airplanes and low-altitude airships flying in the aviation layer, and also different from satellites working in low orbits. It has a very wide range of military and civilian values, such as in missile defense, anti-terrorism, communications, remote sensing, space observation and atmospheric measurement. etc. have great application value. However, the flying altitude of high-altitude airships is generally around 20km. The air in this area is thin, the density is about 1 / 14 of the surface air density, the atmospheric pressure is about 5.5kPa, the average wind speed is 10m / s, and the maximum wind speed can reach 40m / s. It is UV-B, its spectrum ranges from 29...

Claims

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Application Information

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IPC IPC(8): B64C1/12B32B15/09B32B15/095B32B27/12B32B27/20
Inventor 张俊
Owner LIYANG TECH DEV CENT