THERMAL INSULATION SYSTEM
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United States of America Patent
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Issued Date -
Apr 20, 2023
app pub date -
Jun 28, 2022
filing date -
Jun 28, 2022
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Abstract
A thermal insulation system for an aerospace duct through which high temperature fluid, greater than 500 F, passes. The thermal insulation system can experience pressures less than 80 kilopascals and can be included in a turbine engine. The thermal insulation system includes at least a first foil layer confronting the duct, an insulation layer confronting the first foil layer, a second foil layer confronting the insulation layer, and at least one coating applied to any one of the layers.
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