| 摘要 |
<p>A method of positioning arrays (9, 10, 11) of stages (4, 5) of a turbine (1), particularly for aircraft engines; the turbine (1) having an axis (2) and a first (9), a second (10) and a third (11) array of blades arranged consecutively, and of which the first and third array (9) (11) have a relative velocity about the axis (2) with respect to the second array (10); the method including the steps of determining the paths of wakes (27) moving inside gaps (16) defined by the blades in the second array (10) and towards the third array (11); distinguishing, for each wake (27), a first (31) and at least one second (32) zone differing from each other; selecting one (32) of the first and second zone (31) (32); and regulating the position of the third array (11) with respect to the first array (9) by aligning the leading edges (21) of the blades (14) in the third array (11) with the paths of the selected wake zones (32). <IMAGE></p> |
