Low noise fan assembly

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/045 (2006.01)

Patent

CA 2076100

A gas turbine engine rotor assembly such as a fan or compressor includes a plurality of rotor blades spaced axially from a plurality of stator vanes inside an annular duct. The number of vanes is selected for a predetermined number of blades for obtaining substantially equal values of a cut-off ratio for at least two blade passing frequency harmonics for reducing spinning mode noise from the duct.

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