发明名称 |
MULTIFLOW TURBOJET ENGINE FAN AND TURBOJET ENGINE FITTED WITH SUCH A FAN |
摘要 |
<p>The fan (3) comprises a fan disk (8) able to be rotationally driven about a longitudinal axis and provided at the periphery with radial blades (10) each comprising a root (12) slideably engaged in a groove (18) of the disk and, on the outside thereof, a vane (11), platforms (14) surrounding the disk being interposed between the radial blades. Advantageously, the fan additionally comprises shock-absorbing wedges (31) which are arranged tangentially at the exterior periphery (19) of said disk (8) underneath the platforms (14) and between two roots (12) of adjacent radial blades, each wedge (31) being in tangential contact with the two adjacent blades.</p> |
申请公布号 |
WO2014140449(A1) |
申请公布日期 |
2014.09.18 |
申请号 |
WO2014FR50472 |
申请日期 |
2014.03.04 |
申请人 |
SNECMA |
发明人 |
DELAPIERRE, MICHAËL;REGHEZZA, PATRICK, JEAN-LOUIS |
分类号 |
F01D5/22;F01D5/30;F01D5/32;F01D11/00;F04D29/66 |
主分类号 |
F01D5/22 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|