发明名称 Leaktight seal of a circular vane stage
摘要 A leaktight seal includes plaquettes that are housed between platforms of "hammer legged" vanes and a periphery of a rotor disc. The plaquettes lie above a throat that receives legs between a collar. The plaquettes are completed with heels that also lie between the legs. Centrifugal forces distort the seal and produce excellent leaktightness between the disc and the platforms.
申请公布号 US6332617(B1) 申请公布日期 2001.12.25
申请号 US19990255023 申请日期 1999.02.22
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION "SNECMA" 发明人 LEVEAUX JACQUES;NAUDET JACKY SERGE
分类号 F01D5/30;F01D11/00;(IPC1-7):F16J15/16 主分类号 F01D5/30
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