Ringdiffusor für eine Gasturbinen-Brennkammer

摘要

A ring-shaped diffuser (1) for feeding for example the pilot burner and the main burner of a ring-shaped gas turbine combustion chamber has at least two ring-shaped diffuser channels (5a, 5b) that lie substantially next to each other in the radial direction. Seen in the circumferential direction, these diffuser channels (5a, 5b) are subdivided by a plurality of struts (7) into adjacent air outlets (6a, 6b). The struts (7) of the diffuser channels (5a, 5b) that lie next to each other in the radial direction are mutually offset.