发明名称 TURBOMACHINE STATOR BLADE CIRCULAR SECTOR AND AIRCRAFT TURBOMACHINE
摘要 FIELD: transport.SUBSTANCE: this circular sector has inner shell sector, set of blades and assy that makes the outer shell sector. Blades are secured to said assy making the outer shell sector and to inner shell sector. Said assy making the outer shell sector comprises multiple elementary sectors spaced apart along the assy tangential direction and damping wedges. Every damping wedge is fitted between two elementary sectors arranged directly along said tangential direction. Profile of every damping wedge approximates to that of elementary sectors. Damping wedges extend along inclined position of aforesaid assy. Another invention of this set relates to turbomachine including said blade circular sector.EFFECT: better damping properties.5 cl, 8 dwg
申请公布号 RU2537997(C2) 申请公布日期 2015.01.10
申请号 RU20120107522 申请日期 2010.07.29
申请人 SNEKMA 发明人 DEZUSH LORAN ZHIL';KAPALA PATRIK EHDMON;ZEHDI SAMIR
分类号 F04D29/54;F01D25/04 主分类号 F04D29/54
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