Patent ID: 8800299
Filing Date: 2014-08-12
Classification: B64D

Abstract:
1. A jet engine nacelle comprising: an air intake forward section; a mid-section intended to surround a fan of the jet engine; an aft section formed from at least two half-shells rotatably mounted such that each of said at least two half-shells is opened out between a working position and a maintenance position under an action of at least one jack and at least one telescopic connecting rod each respectively having a first end fastened on the jet engine and a second end fastened in a corresponding half-shell; and at least one damping member arranged between each of the at least one telescopic connecting rod and said corresponding half-shell, said at least one damping member being be in a prestressed state when the corresponding half-shell is in the working position, said damping member being configured so as to reduce vibrations in the half-shell.