发明名称 Variable camber turbomachine blade having resilient articulation
摘要 A variable camber vane for a turbomachine comprises leading and trailing edge parts, at least one of which is pivotable relative to the other, and a resilient joining part inserted into a space provided between the leading and trailing edge parts, the joining part being formed by a block of resilient material which is bonded to the leading and trailing edge parts and which ensures the continuity of the intrados and extrados faces of the vane to permit an even flow of fluid along the vane. The vane may also include means for enabling a cooling or heating fluid to flow in the leading and trailing edge parts, and a plurality of ducts in the resilient joining part establishing communication between the fluid flow means of the leading and trailing edge parts.
申请公布号 US5472314(A) 申请公布日期 1995.12.05
申请号 US19940271634 申请日期 1994.07.07
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" 发明人 DELONGE, JEAN-CLAUDE L.;LOUDET, CLAUDE J. A.;VERMONT, GERARD R. E. R.
分类号 F01D5/14;F01D5/18;F01D17/16;(IPC1-7):F01D9/02;F04D29/56 主分类号 F01D5/14
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