发明名称 Multiflow turbojet engine fan and turbojet engine fitted with such a fan
摘要 <p>The fan comprises a fan disk able to be rotationally driven about a longitudinal axis and provided at the periphery with radial blades each comprising a root slideably engaged in a groove of the disk and, on the outside thereof, a vane, platforms surrounding the disk being interposed between the radial blades. Advantageously, the fan additionally comprises shock-absorbing wedges which are arranged tangentially at the exterior periphery of said disk underneath the platforms and between two roots of adjacent radial blades, each wedge being in tangential contact with the two adjacent blades.</p>
申请公布号 GB201515665(D0) 申请公布日期 2015.10.21
申请号 GB20150015665 申请日期 2014.03.04
申请人 SNECMA 发明人
分类号 主分类号
代理机构 代理人
主权项
地址