A kind of low-temperature anti-fog method for glass

An anti-fog, low-temperature technology, applied in aircraft accessories and other directions, can solve problems such as affecting the driver's sight, and achieve the effect of preventing fog

Active Publication Date: 2016-02-24
中国航空工业集团有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] During the flight of the aircraft, the external temperature will be lower than 0°C at high altitude. At this time, water droplets will condense on the internal glass plate to form fog, which will affect the driver's sight.

Method used

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  • A kind of low-temperature anti-fog method for glass
  • A kind of low-temperature anti-fog method for glass

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Embodiment Construction

[0018] The following structural examples describe technical solution of the present invention in further detail

[0019] see figure 1 , 2 Shown, the step of this kind glass plate low-temperature anti-fog method is:

[0020] The first step, processing anti-fog glass plate

[0021] The thickness of the anti-fog glass plate 2 is m=2mm~4mm, the length L1 of the anti-fog glass plate 2 is equal to the length of the anti-fog glass plate 1, and the width L2 of the anti-fog glass plate 2 is equal to the width of the anti-fog glass plate 1;

[0022] The second step, paste the double-sided tape

[0023] The double-sided adhesive strip is composed of two long-side double-sided adhesive strips 3 and two wide-side double-sided adhesive strips 4. The thickness t of the side double-sided adhesive strip 3 and the wide-side double-sided adhesive strip 4 is 20 mm to 30 mm;

[0024] First bond two long-side double-sided adhesive tapes 3 to the long side of the anti-fog glass plate 1, and the...

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Abstract

The invention provides a mist preventing method for a glass plate at a low temperature. The mist preventing method comprises steps of processing a mist preventing glass plate, sticking a double-sided adhesive tape, binding the mist preventing glass plate and coating glass plate glue. According to the invention, the mist preventing glass plate is stuck to a common glass plate; the thickness of the double-sided adhesive tapes as well as the sealing and binding function of the glass plate glue are utilized, so as to form a closed air cavity between the common glass plate and the mist preventing glass plate; the low temperature of the outside world is unlikely to be transmitted to the inner surface of the mist preventing glass plate, so that the surface temperature of the mist preventing glass plate is maintained and the generation of the mist is prevented. Devices processed through adopting the mist preventing method improves the temperature insulating capability between the glass plate and the outside world; the glass plate on the inner surface is not subject to the influences of the external low temperature, so that the temperature of the glass plate on the inner surface is increased and the generation of the mist on the inner surface is reduced.

Description

technical field [0001] The invention relates to a low-temperature anti-fog method for glass, which is used for internal anti-fog of a glass plate at low temperature. Background technique [0002] When the aircraft is flying at high altitude, the outside temperature will be lower than 0°C. At this time, water droplets will condense on the internal glass plate to form fog, which affects the driver's sight. Contents of the invention [0003] The present invention is designed to address the above situation and provides a low-temperature anti-fog method for glass, the purpose of which is to prevent the glass plate from generating fog in a low-temperature environment. [0004] Technical solution of the present invention is: [0005] The steps of this glass plate low temperature anti-fog method are: [0006] The first step, processing anti-fog glass plate [0007] The thickness of the anti-fog glass plate (2) m=2mm~4mm, the length L1 of the anti-fog glass plate (2) is equal to...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64C1/14
Inventor 高晓颖李广伟金永生刘艳伟
Owner 中国航空工业集团有限公司
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