发明名称 Mounting arrangement for fixing a fan blade to a disk of a turbojet engine
摘要 A turbojet engine fan rotor including a rotor disk having a peripheral rim with a plurality of axially extending channels carrying a plurality of fan blades each having a blade root interengaging with the channels of the disk, and a mounting arrangement for securing the blades to the disk. The mounting arrangement includes an annular member having a plurality of radially extending teeth, a plurality of wedges each interposed between one of the blade roots and a corresponding one of the channels and including a radially extending boss provided at one end, and a plurality of radially extending protrusions from the disk. The plurality of teeth and the plurality of protrusions cooperate with one another to secure the annular member with the rotor disk.
申请公布号 US2002090300(A1) 申请公布日期 2002.07.11
申请号 US20020041580 申请日期 2002.01.10
申请人 DOUGUET CHARLES JEAN-PIERRE;JUDET MAURICE GUY;LEJARS CLAUDE ROBERT LOUIS;NITRE THIERRY 发明人 DOUGUET CHARLES JEAN-PIERRE;JUDET MAURICE GUY;LEJARS CLAUDE ROBERT LOUIS;NITRE THIERRY
分类号 F04D29/34;F01D5/30;(IPC1-7):F01D1/00 主分类号 F04D29/34
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