(57) The invention relates to a blade (10) of a rotor of a ninth phase of a compressor,
which can be defined by coordinates of a discreet combination of points, in a Cartesian
reference system (X,Y,Z), wherein the axis (Z) is a radial axis intersecting the central
axis of the compressor, said blade (10) having a profile which can be identified by
means of a series of closed intersection curves between the profile itself and planes
(X,Y) lying at distances (Z) from the central axis, said blade (10) also comprising
a thickening (30), substantially parallel to a base portion (12) of the blade (10)
itself, fixable to said rotor, said thickening (30) being substantially situated half-way
up the blade (10) and being suitable for shifting the natural resonance frequencies
of the blade (10) itself outside a functioning frequency range of said rotor.
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