Patent ID: 8882450

Claim:
A device for supporting and fixing equipment to a nacelle fairing or aircraft engine fairing, the device comprising: at least one vibration damper including: a first rigid part configured to be fixed to the fairing through a first fixation, a second rigid part configured to be connected rigidly to the equipment, so as to suspend the equipment on the fairing, the second rigid part being structurally separated from the first rigid part, and an elastically deformable material interposed between the first rigid part and the second rigid part, so that any one of the first rigid part and the second rigid part is movable with respect to the other of the first rigid part and the second rigid part by deforming said elastically deformable material; and a rigid safety device structurally separated from the first and second rigid parts and configured to keep the damper in position on the fairing in an event of a failure or a breakage of at least one of the damper and said first fixation, to ensure support and fixation of the equipment, whereby the rigid safety device is independent of the damper and is mounted crosswise on the damper, whereby the rigid safety device includes a middle rigid part that at least partly caps or covers the damper, and lateral opposite ends configured to be fixed to the fairing through a second fixation, whereby the first fixation is independent of the second fixation.