The cone (28) has honeycomb-structured layer (30) which is arranged inside outer wall (29) extending along inner side of outer wall. An inner wall (31) connected to honeycomb structure has passage recesses connecting area of honeycomb structure to annular ...

The assembly has a metallic fixation ring (60) rigidly connected to an aeronautical engine and an exhaust cone (20) i.e. plug, made of ceramic matrix composite material. The exhaust cone is mounted onto the fixation ring by resiliently flexible mounting lu...

An augmentor (24) includes an insert (108) which reduces thermal stresses caused by hot combustion gases impinging the augmentor. The augmentor also includes a plurality of radial flameholder gutters (74) and at least one outer circumferential flameholder ...