FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to heat protection with composite materials. Proposed method comprises lining aircraft nose thermally stressed elements with composite heat-isolation material. Surface of lining material in contact with high-temperature gas flow is rough. Roughness Rz is selected from the range of 1·10-4 m ≤ Rz ≤ 5·10-4 m.
EFFECT: higher efficiency.
3 dwg
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Authors
Dates
2013-05-10—Published
2012-01-27—Filed