Invention Application
US20160363050A1 PITCH CHANGE MECHANISM FOR SHROUDED FAN WITH LOW FAN PRESSURE RATIO 有权
用于风扇压力比低的风扇的变更机构(PITCH CHANGE FOR SHROUDED FAN LOW FAN PRESSURE RATIO)

PITCH CHANGE MECHANISM FOR SHROUDED FAN WITH LOW FAN PRESSURE RATIO
Abstract:
A shrouded fan assembly for use with a gas turbine engine includes a central hub and a plurality of variable-pitch fan blades coupled to and extending radially outward from the central hub. Each variable-pitch fan blade includes a radially outer tip is rotatable about a longitudinal axis extending therethrough. A shroud is coupled to each radially outer tip.
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