发明名称 METHOD OF AIRCRAFT NOSE HEAT PROTECTION
摘要 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 Ris selected from the range of 1·10m ? R? 5·10m.EFFECT: higher efficiency.3 dwg
申请公布号 RU2481239(C1) 申请公布日期 2013.05.10
申请号 RU20120102950 申请日期 2012.01.27
申请人 FEDERAL'NOE GOSUDARSTVENNOE BJUDZHETNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "NATSIONAL'NYJ ISSLEDOVATEL'SKIJ TOMSKIJGOSUDARSTVENNYJ UNIVERSITET" (TGU) 发明人 GOLOVANOV ALEKSANDR NIKOLAEVICH;ZIMA VLADISLAV PAVLOVICH;STEPANOVA EVGENIJA VALER'EVNA
分类号 B64C1/38;B64G1/58;F42B15/00 主分类号 B64C1/38
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