TURBOMACHINE GUIDE VANES WITH IMPROVED VANE PROFILE
A set of turbomachine guide vanes including plural vanes arranged around an annulus, each vane having a leading edge extending between root and tip ends, the leading edge offset between these two ends being greater than 10% of the blade height. A tangential stacking of the guide vanes towards the suction face side, the curve of tangential stacking, of the position, in the direction tangential to the annulus, of centers of gravity of successive vane cross sections along the vane height, is a curve that increases constantly towards the suction face side. The curve, near the vane tip end, has an accentuated gradient towards the suction face side compared with the rest of the curve, and has a mean gradient near the vane tip end that is greater than at least 1.2 times the mean gradient of the curve over the portion between 30% and 90% of the vane height.
1 - 7 . (canceled)
8 . A straightener of a turbomachine, comprising:
a plurality of vanes arranged around a ring centered on an axis of the turbomachine, each vane including a leading edge and extending between a root end and a tip end,
the leading edge at the root end of each vane being situated upstream of the leading edge at the tip end of the vane, relative to an air flow direction, an offset of the leading edge between these two ends being greater than 10% of the height of the vane, measured in a direction of the axis of the turbomachine,
a tangential stacking curve, of a position, in the tangential direction of a ring of centers of gravity of consecutive vane sections along the height of the vane, is a curve constantly increasing toward an upper surface of the vane,
the curve has, in proximity to the tip end of a vane, an increased slope toward the upper surface compared to a rest of the curve, and the curve has an average slope in proximity to the tip end of the vane greater than at least 1.2 times the average slope of the curve on a portion between 30% and 90% of the vane height.
9 . The turbomachine straightener according to claim 8 , wherein the portion of the slope in proximity to the tip end is between 90% and 100% of the vane height.
10 . The turbomachine straightener according to claim 8 , wherein the leading edge of each vane includes at least one portion located downstream of the position of the leading edge at the tip end of the vane with respect to the direction of the air flow.
11 . The turbomachine straightener according to claim 3 , wherein the portion is included in a region of the leading edge situated between 60% and 100% of the height of the vane.
12 . The turbomachine straightener according to claim 10 , wherein a point of the leading edge positioned in line with the position of the leading edge at the tip end of the vane is situated between 60% and 80% of the vane height.
13 . The turbomachine straightener according to claim 8 , wherein the leading edge at the root end of each vane is situated upstream of the leading edge at the tip end of the vane with respect to the air flow direction by a distance between 10% and 20% of the vane height, or between 12% and 20% of the vane height, the distance being measured in the direction of the axis of the turbomachine.
14 . A turbomachine comprising at least one straightener according to claim 8 .