PERFEZIONATA RIENTRANZA DI CARCASSA DI COMPRESSORE PER TURBOMOTORE AGAS
A means for improving the aerodynamic efficiency of the compressor of an axial flow turbomachine is disclosed. The compressor includes an airfoil relatively rotatable with respect to a radially disposed surface which bounds a flowpath for aft moving fluid. The surface has a circumferentially extendi...
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Format: | Patent |
Sprache: | ita |
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