发明名称 AIRCRAFT POWER PLANT COMPRISING ENGINE AND ENGINE PYLON
摘要 FIELD: transport. ^ SUBSTANCE: power plant 1 comprises engine 2 and engine pylon 4. Proposed pylon comprises rigid structure 10 including torsion box 24 and mounting assembly 11 arranged between engine and said rigid structure. Mounting assembly comprises engine suspension rear assembly 8. Besides power plant comprises additionally torsion box heat protection system that includes, preferably, blow-off air duct 60 arranged between said torsion box 24 and engine 2 to produce heat barrier. Said air duct extends rearward and beyond engine suspension limits. ^ EFFECT: improved cooling of engine attachment rigid structure. ^ 12 cl, 8 dwg
申请公布号 RU2401222(C2) 申请公布日期 2010.10.10
申请号 RU20080116732 申请日期 2006.09.26
申请人 EHRBJUS FRANS 发明人 LAFON LORAN;ZHURNAD FREDERIK
分类号 B64D27/26 主分类号 B64D27/26
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