FIELD: thermal insulation.
SUBSTANCE: group of inventions relates to a heat insulating system for an aircraft and to a method for heat insulation of a high-temperature component of an aircraft from a heat-sensitive component of an aircraft during operation aircraft, to a method for assembling a heat insulating system for an aircraft. The system comprises a high temperature component, a heat-sensitive component, a supporting structure, a container, two pluralities of magnets. For heat insulation of a high temperature component, magnetic fields are generated from the first and second pluralities of magnets directed oppositely in order to form a gap between the inner surface of the supporting structure and the outer surface of the container. To assemble the heat insulating system, the first plurality of magnets is connected to the inner surface of the supporting structure, the high-temperature component is thermally connected with the outer surface of the supporting structure, the second plurality of magnets is connected to the outer surface of the container, the heat-sensitive component is thermally connected with the inner surface of the container, the container is placed in the inner space of the supporting structure.
EFFECT: diminished effect of heat on the avionics is ensured.
20 cl, 16 dwg
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Authors
Dates
2021-08-11—Published
2018-02-26—Filed