| 摘要 |
The invention relates to a guide vane (10) made from composite material for a gas turbine engine, comprising a fibrous reinforcement densified by a matrix, the fibrous reinforcement being formed as a single component by means of three-dimensional weaving with a blading (12) and at least two attachment flanges (14a, 14b, 24a, 24b, 26a) extending from a radial end (16, 18) of the vane towards opposing side faces (12a, 12b) of the blading, said attachment flanges being axially staggered in relation to each other. The invention also relates to a method for producing such a vane. |
