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US08016561B2 Gas turbine engine fan assembly and method for assembling to same 有权
燃气涡轮发动机风扇组件及其组装方法

Gas turbine engine fan assembly and method for assembling to same
摘要:
A method for operating a turbofan engine includes providing a first fan disk configured to rotate in a first rotational direction, coupling a first fan blade to the first fan disk, the first fan blade including a dovetail, an airfoil coupled to the dovetail, and a plurality of channels extending through the dovetail, and channeling airflow through the at least one fan blade such that the airflow is discharged from the airfoil trailing edge to facilitate reducing the operational noise level of the turbofan engine and improve.
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