Device for protection axial rotor blades and for eliminating rotor imbalance compressor or axial flow turbines.

摘要

INDICATED AN ELIMINATION OF decompensation ROTOR DEVICE FOR SAFETY PERFORMANCE AXIAL OF PRAISE AND FOR AXIAL COMPRESSOR OR TURBINES powertrains GAS TURBINE IN WHICH Vanes (1) OPERATING WITH ITS BASES (2) anchored in grooves (3) THRUST DISK (4) WHEEL DISTRIBUTED BY THE PERIPHERY; So each axial groove includes a cavity (T) formed between the base of the groove and the end of the base; In each cavity STANDS ONE PIECE (5) FILLING USED ON THE BASIS OF SLOT AND PLATES (6) SAFETY bridging between the end of the base and the filler piece A CRACK (S) PASSING ALONG Cavity, doubling AT BOTH ENDS aLIGNED oppositely and projecting CAVITY FACING THE FRONT SURFACE, DISC WHEEL AND THE BASE OF PRAISE, SO decompensation rOTOR compensated BY WEIGHT THROUGH ONE PIECE OF FILLING.