Annular combustor for a gas turbine and gas turbine

摘要

The chamber (4) has a lining unit (10) with stiffening ribs and interlocking units. The interlocking units have a hook width of B on a rear side facing away from a combustor of two edge areas. The lining unit is secured to a related bearing structure (26), so as to release the lining unit from the structure. The lining unit is moved by the extent of the hook width B of the interlocking unit in an axial direction.