Thrust reverser
AssigneesSnecma, Aircelle
InventorsHerve Hurlin, Nicolas Dezeustre, Wouter Balk, Bertrand Desjoyeaux
Life of this patent
Estimating the term…
Abstract
A thrust reverser for the nacelle of a turboreactor includes at least one fixed front frame that can be mounted downstream of a fan casing of the turboreactor and directly or indirectly supports at least one flow deviation vanes, in which at least part of the flow deviation vanes can be detached from the front frame and moved in translation independently therefrom when a maintenance operation is being carried out on the reverser.
Claims8
A thrust reverser for a turbojet engine nacelle comprising at least one fixed front frame suitable for being mounted downstream of a fan case of said turbojet engine and directly or indirectly supporting at least one flow deviating means, characterized in that at least part of the flow deviating means is detachable from the front frame to be translated independently therefrom when a maintenance operation is being carried out on said reverser.
Dependencies are inferred from the claim text.