Patent ID: 8919693
Filing Date: 2014-12-30
Classification: B64D,E05F,E05Y,F02C,F05D

Abstract:
1. A guide device for a translationally moving part of a turbojet engine nacelle and comprising: a rail mounted fixedly on a part of the nacelle; and a slide attached to the moving part and able to slide along the rail, wherein said guide device is equipped with an in-built retractable system for stopping a translational movement of the slide and said guide device comprising at least one immobilizing means pivotally mounted on the rail such that the immobilizing means move alternately from an engaged position in which the immobilizing means constitutes a translational end stop for the slide to a disengaged position in which the immobilizing means is away from the slide and allows a relative translational movement of the slide beyond a locking system and, the retractable system further comprising at least one control means for controlling the immobilizing means, wherein the control means is returned from an unlocked position to a locked position upon a return of the slide, thereby causing the immobilizing means to return to the engaged position.