Tool for handling an inlet cowl of an aircraft turbine engine
OwnerVivien Lucienne, Tony Dehais +1inventors
InventorsVivien Lucienne, Tony Dehais, Francois Bellet
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Abstract
A Tool for handling an aircraft turbine engine cowl comprises an axis, a body and a bar extending longitudinally from the body, the bar being configured to be inserted into a hole located along the axis of the cowl, the tool being configured to allow the bar to rotate relative to the body and about the longitudinal axis of the bar.
Claims10
A tool for handling an aircraft turbomachine cowl, comprising an axis, a body and a bar longitudinally extending from the body, the bar being configured to be inserted into a hole located along the axis of the cowl, the tool being configured to allow the bar to rotate relative to the body and about the longitudinal axis of said bar.
Dependencies are inferred from the claim text.