Thermal insulation for aircraft components
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United States of America Patent
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Dec 3, 2019
Grant Date -
Aug 24, 2017
app pub date -
May 9, 2017
filing date -
Oct 13, 2015
priority date (Note) -
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Abstract
A thermal insulation system for an aircraft is provided. The thermal insulation system includes a carrier and a container. The carrier has an interior surface including a first plurality of magnets that generate a first magnetic field, and an exterior surface that is thermally coupled to at least one high temperature component. The container is surrounded by the interior surface of the carrier, has an exterior surface including a second plurality of magnets that generate a second magnetic field oriented opposite the first magnetic field, and has an interior surface that is thermally coupled to at least one temperature sensitive component. The first magnetic field and the second magnetic field generate a gap between the carrier and the container to reduce a heat transfer from the at least one high temperature component to the at least one temperature sensitive component during operation of the aircraft.
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