发明名称 |
Locking mechanism for fan blades |
摘要 |
<p>The rotor has fan blades (15) connected to a rim, where each blade has a blade root (17) engaged in a groove of the rim and retained in the groove by a lock (28). The lock is engaged in notches (34) arranged on both sides of the corresponding groove, near an upstream end of the groove for immobilizing the root in axial direction. The lock has curved plates with concavity directed toward the upstream. The notches (34) are inclined toward the upstream and receive the edges of the plates. An independent claim is also included for a jet engine of an aircraft comprising a fan rotor.</p> |
申请公布号 |
EP1748154(B1) |
申请公布日期 |
2016.01.13 |
申请号 |
EP20060118048 |
申请日期 |
2006.07.28 |
申请人 |
SNECMA |
发明人 |
BUISSON, HERVÉ;GOGA, JEAN-LUC;LEFEBVRE, ERIC |
分类号 |
F01D5/30;F04D29/32 |
主分类号 |
F01D5/30 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|