Patent ID: 8448901

Claim:
Aircraft nacelle that comprises: discharge means ( 50 ) linking an inside of the nacelle with an outside of the nacelle; and a junction zone between two superposed panel elements ( 54 , 56 ) at a level of which the two panel elements are superposed, wherein, the two panel elements each have a surface that forms an outside surface of the nacelle on both sides of the junction zone, and said discharge means ( 50 ) comprises a two-part block ( 52 ) comprised of i) a first part ( 58 , 70 , 88 ) that is inserted between the superposed two panel elements and that comprises at least one projecting and/or hollow element to provide a passage between said two panel elements so as to link the inside and the outside of the nacelle, and ii) a second part ( 60 , 72 , 90 ) to one side of a single panel ( 56 ) of the two panel elements, the single panel ( 56 ) arranged inside at the level of the junction zone so as to be protected from an excessive temperature.