发明名称 Blades rotor disc with threepronged blades
摘要 The blade (10) is held into the disc (1) by the interference fit of a triple root (7,8,9) into circumferential grooves (4,5,6) in the disc. The roots are stepped along the periphery of the rotor, each root lying on a different angular radius from the rotational axis of the disc. The roots are of different cross sections, as are the grooves. Each root is held against the outer edge of its groove by a shock-absorbing spring. The clearances between the roots and the grooves allow limited movement of the blades in the grooves, the system being tuned to dampen vibrations.
申请公布号 EP0854268(A1) 申请公布日期 1998.07.22
申请号 EP19980400062 申请日期 1998.01.15
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION, "S.N.E.C.M.A." 发明人 NAUDET, JACKY;POY, CHRISTOPHE
分类号 F01D5/26;F01D5/30;(IPC1-7):F01D5/30 主分类号 F01D5/26
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