Invention Application
US20160252103A1 FAN ROTOR WITH INTEGRATED PLATFORM ATTACHMENT 审中-公开
风扇转子与集成平台连接

FAN ROTOR WITH INTEGRATED PLATFORM ATTACHMENT
Abstract:
A fan rotor, for an aircraft engine, including at least one blade root attachment lug, each blade root attachment lug including an attachment lug surface, wherein at least one cavity is disposed on each attachment lug surface.
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