CPC F02C 7/24 (2013.01) [G10K 11/168 (2013.01)] | 16 Claims |
1. An acoustic liner for a gas turbine engine, the acoustic liner comprising:
a core comprising a plurality of cells extending between a first side of the core and a second side of the core opposite the first side of the core;
a back skin comprising a light-reflecting layer and a structural layer, the light-reflecting layer comprising a first side and a second side, the first side of the light-reflecting layer attached to the first side of the core, the first side of the light-reflecting layer having a reflectance of greater than fifty percent, the structural layer bonded to the second side of the light-reflecting layer using an adhesive, the structural layer comprising a plurality of thermoplastic layers; and
a face skin, the face skin comprising a first side attached to the second side of the core.
|