| 摘要 |
An inter-vane platform ( 3 ), for a vane support disk ( 1 ) of a turbine engine fan, comprises a central part ( 5 ) of one piece with the support disk ( 1 ) between two adjacent vanes ( 2 ), and two lateral parts ( 8,9 ), forming extensions to two lateral edges ( 6,7 ) of the central part ( 5 ), and each designed in such a way as to deflect under the impact of the vane ( 2 ) opposite which it is located. |
