发明名称 AXIAL FLOW TURBOMACHINE ROTOR
摘要 An axial flow turbomachine rotor comprises a disc having a plurality of annular flanges extending outwardly from its periphery, a plurality of blades secured to the disc and extending radially outwardly from the periphery thereof, each of the blades having its root notched to define heels which are received in the grooves formed between the annular flanges of the disc, and a plurality of separate platforms which are secured to the disc and are disposed between the blades to define the inner boundary of the fluid flow path through the rotor, the blades each being fixed to the disc by two parallel pins which are equidistance from the axis of the disc and are received in corresponding bores passing through the annular flanges and the heels of the blade, the pins also serving to secure the platforms to the disc.
申请公布号 US5145319(A) 申请公布日期 1992.09.08
申请号 US19900616594 申请日期 1990.11.21
申请人 SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATIONS S.N.E.M.C.A. 发明人 GLOWACKI, PIERRE A.
分类号 F01D5/30 主分类号 F01D5/30
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