| 发明名称 | Fan rotor for an airplane turbojet | ||
| 摘要 | A fan rotor for an airplane turbojet including locking blade roots in the respective grooves of an airplane turbojet fan rotor. Each blade root is housed in a groove that is closed by a main latch and by an additional latch that is distinct from the main latch and that is spaced apart therefrom by a predetermined distance. | ||
| 申请公布号 | US8899935(B2) | 申请公布日期 | 2014.12.02 |
| 申请号 | US201013318502 | 申请日期 | 2010.04.19 |
| 申请人 | Snecma | 发明人 | Buisson Herve;Goga Jean-Luc |
| 分类号 | F01D5/30;F04D29/32 | 主分类号 | F01D5/30 |
| 代理机构 | Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P. | 代理人 | Oblon, Spivak, McClelland, Maier & Neustadt, L.L.P. |
| 主权项 | 1. A fan rotor comprising: fan blades attached to a periphery of a wheel, each blade including a blade root engaged in a groove in the wheel and retained therein by a latch engaged in notches formed in a vicinity of and on either side of an upstream end of the corresponding groove to oppose movement of the blade root in an axial direction, each latch, as a main latch, being associated with an additional latch that is distinct from the main latch, wherein the additional latch is spaced apart from the main latch at a predetermined distance, the additional latch being situated between the main latch and an upstream end of the blade root engaged in the groove. | ||
| 地址 | Paris FR | ||