Gas turbine engine nacelle with sound damping means in the fan intake area

The housing (29) has a honeycomb structural layer arranged in a region of an inflow-side air inlet (11) at the housing arranged upstream of a fan (12). Sound proofing elements arranged at radially outside the honeycomb structural layer that extends in axial direction. The sound damping elements are arranged annularly adjacent to one another in circumferential direction. Each sound-damping element comprises a hollow chamber extending in axial direction through recesses in communication with the honeycomb structural layer.