Invention Grant
US09470151B2 Alignment system and methodology to account for variation in a gas turbine engine 有权
对准系统和方法来解释燃气涡轮发动机的变化

Alignment system and methodology to account for variation in a gas turbine engine
Abstract:
A gas turbine engine includes a bushing that is non-round in cross-section, the bushing receivable within an aperture. A fastener passes through the bushing to retain a second component to a third component with respect to the first component.
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