发明名称 Compressor rotor blade having a tip with asymmetric lips
摘要 A blade of a compressor rotor has its tip provided with at least one discontinuous sealing lip formed by two half lips arranged on opposite sides of the blade asymmetrically with respect to a transverse sectional plane of the blade tip, either with or without overlap of the half lips in the direction of the chord of the blade.
申请公布号 US4875831(A) 申请公布日期 1989.10.24
申请号 US19880273090 申请日期 1988.11.18
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" 发明人 FETIVEAU, JEAN Y. L.
分类号 F01D5/20 主分类号 F01D5/20
代理机构 代理人
主权项
地址