Rotor asymmetry

摘要

A gas turbine engine (10) has a section, such as a compressor section (14), with at least two spaced apart stator assemblies (28) and an asymmetrical rotor assembly (30') positioned between the spaced apart stator assemblies (28). The asymmetrical rotor assembly (30') has a rotor array which is asymmetric about at least one diameter of the rotor assembly (30').