Combustion chamber of a gas turbine

摘要

A combustion chamber of a gas turbine with an outer combustion chamber wall and with tiles attached to the inner side of said wall or to a combustion chamber of the single-wall design, wherein the combustion chamber has in a center area, relative to the flow direction, a slot extending around the circumference of the combustion chamber and dividing the outer combustion chamber wall and the tiles for the supply of mixing air.

主权项

1. A combustion chamber of a gas turbine comprising:
an outer combustion chamber wall; tiles attached to an inner side of the outer combustion chamber wall; a slot positioned in a center area of the combustion chamber relative to a flow direction and extending around an entire circumference of the combustion chamber, the slot physically separating the outer combustion chamber wall and the tiles into a front part and a separate rear part for supplying mixing air, the front part and the rear part being separately mounted to the gas turbine, the slot including an outlet, the outlet opening toward a radial center of the combustion chamber, a flow path of the slot at the outlet being directed toward the radial center of the combustion chamber to direct the mixing air from the outlet toward the radial center of the combustion chamber; a plurality of combustion chamber arms separately mounting the front part of the combustion chamber and the rear part of the combustion chamber, the combustion chamber arms having through-flow openings, wherein a through-flow opening most adjacent to a combustion chamber head provides the slot with at least a portion of the mixing air.