A BLEED STRUCTURE FOR A BLEED PASSAGE IN A GAS TURBINE ENGINE
The invention relates to a bleed structure (17) for a bleed passage in a gas turbine engine. The structure comprises a first wall portion (18) defining a first side of an opening for the passage, and a second wall portion (19) defining a second side, opposite the first side of the opening. The first and second wall portions (18; 19) end at different positions in an extension direction of the opening.