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Aeroengine fan assembly

机译:航空发动机风扇组件

摘要

A fan assembly of a gas turbine engine, the fan assembly includes an array of radially extending blades defining gaps therebetween and an annulus filler located within at least one gap. The annulus filler includes at least two individual bodies arranged circumferentially adjacent one another with at least one adjacent a blade, one of the bodies includes a flexible wall arranged to centrifuge outwardly against the other body thereby urging both bodies against the blades and securing them during engine operation.
机译:燃气涡轮发动机的风扇组件,该风扇组件包括在其间限定间隙的径向延伸叶片的阵列以及位于至少一个间隙内的环形填料。环形填充器包括至少两个单独的主体,该至少两个单独的主体在周向上彼此相邻布置,并且至少一个邻近叶片,其中一个主体包括柔性壁,该柔性壁布置成靠着另一个主体向外离心,从而将两个主体推向叶片并在发动机期间固定它们操作。

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