The invention relates to a woven laminate which is used, preferably, as a covering for sound absorption of input and output sound absorbers in an auxiliary gas turbine (APU) of an aircraft, in particular, an aeroplane. Said woven laminate comprises at least three superimposed and at least partially soldered together woven layers. One of said layers comprises a relatively large structure in relation to the others, another layer has a fine structure and the remaining woven layer has a structure which is between the large and the fine structure. Said woven layers comprises metallic wires which are wound together or twisted in a non-woven manner.