Turbomachine casing
A turbomachine casing forming a continuous annular ring extending over 360° around a bladed wheel and serving as a propagation medium for rotating waves, each rotating wave being generated by two standing waves of the same frequency, and the casing including at least one longitudinal stiffener at its outer periphery that is dimensioned and positioned in such a manner as to separate the frequencies of the two standing waves of at least one given rotating wave.
1. A turbomachine casing forming a continuous annular ring extending over 360° around a bladed wheel and serving as a propagation medium for rotating waves, each rotating wave being generated by two standing waves having the same frequency, wherein the casing includes at least one longitudinal stiffener at its outer periphery positioned at an antinode of at least one of the two standing waves of a given rotating wave in order to separate the frequencies of the two standing waves.
2. A casing according to claim 1 , wherein the frequency difference between the standing waves of the rotating wave is greater than or equal to 3%.
3. A casing according to claim 1 , including at least two stiffeners arranged at 90° or 180° relative to each other.
4. A casing according to claim 1 , including a plurality of the above-mentioned stiffeners that are positioned around the axis at mutually differing angular intervals.
5. A casing according to claim 1 , wherein the or each above-mentioned stiffener is/are positioned and dimensioned so as to generate frequency differences between the standing waves of a plurality of given rotating waves.
6. A casing according to claim 5 , wherein the stiffeners are axial ribs.
7. A casing according to claim 6 , wherein the ribs extend over at least a portion of the axial length of the casing.
8. A turbomachine includes a casing according to claim 1 .