WAVY TILTING OF PLATFORMS AT THE ROTOR-STATOR GAPS IN A TURBINE ENGINE COMPRESSOR

A set of compression stage(s) of a turbomachine, forming an annular fluid passage and comprising at least one annular stator platform and/or at least one annular rotor platform having an outer longitudinal profile inclined (ISi/IRi) inwards and upstream with respect to a nominal profile of the fluid...

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Bibliographische Detailangaben
Hauptverfasser: CAVAREC, Mickael, SCHVALLINGER, Michaël, Franck, Antoine
Format: Patent
Sprache:eng ; fre ; ger
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Beschreibung
Zusammenfassung:A set of compression stage(s) of a turbomachine, forming an annular fluid passage and comprising at least one annular stator platform and/or at least one annular rotor platform having an outer longitudinal profile inclined (ISi/IRi) inwards and upstream with respect to a nominal profile of the fluid stream, where the inclination (ISi/IRi) of the outer longitudinal profile of the or each of the annular platforms, relative to the nominal profile of the fluid stream, oscillates along the circumference of the annular platform or platforms, between a maximum value in front of the blades of the annular platform and a minimum value between each pair of adjacent blades of the annular platform.