Thermal protection structure and preparation method thereof

Abstract

The invention provides a thermal protection structure and a preparation method thereof. The thermal protection structure comprises a thermal insulation layer, a cavity layer and a skin which are sequentially arranged, wherein the thermal insulation layer is arranged on the outer surface of the inner cabin of an aircraft, the thermal insulation layer comprises a porous thermal insulation structure, a temperature-sensitive hydrogel arranged in the porous thermal insulation structure and a cooling working medium adsorbed in the temperature-sensitive hydrogel, when the thermal protection structure is not subjected to thermal protection, the temperature-sensitive hydrogel is in a swelling state and is used for adsorbing the cooling working medium into the temperature-sensitive hydrogel in a solid-phase existence form, and when the thermal protection structure carries out thermal protection, the temperature-sensitive hydrogel absorbs heat radiated inwards from the skin and the cavity layer so as to make the temperature-sensitive hydrogel be in a deswelling state, and is used for sequentially converting the existence form of the cooling working medium from a solid phase to a liquid phase and a gas phase, and discharging the gas-phase cooling working medium after being released to the cavity layer. The thermal protection structure provided by the invention has excellent thermal protection performance.

Description

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AI Technical Summary

Benefits of technology

The technical effect of this patented design is that by providing an inner part called the heat insulting protective layers or shells on top of the air conditioner's interior space, they have good thermal barrier capabilities for maintaining optimal temperatures during flight operations. This makes them suitable for reuse when needed without requiring maintenance over time. Additionally, there are also features like coolant supply systems used within the system itself, allowing users to adjust how much liquid crystal material needs to absorb enough cold water from outside sources while still keeping their internal parts warm properly.

Problems solved by technology

This patented describes how current methods of protecting against damage caused during low altitude flights involve adding layers between different parts inside the body of the object being protected. While some previous solutions were able to perform well under certain conditions but could still cause significant issues if applied outside these specific environments where temperature changes frequently occur.

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