Patent ID: 8875517
Filing Date: 2014-11-04
Classification: F02C,F04D,F23R,Y02T

Abstract:
1. A turbine engine, comprising: an annular diffuser comprising two annular webs extending inside one another and connected between them by substantially radial vanes, wherein a downstream peripheral edge of at least one of the webs comprises indentations evenly distributed around the longitudinal axis of the diffuser; and an annular combustion chamber arranged downstream of the diffuser and inside an external casing of the turbine engine, the combustion chamber being adapted to be supplied with fuel by injectors arranged between the diffuser and the chamber and extending substantially radially towards an interior from the external casing, the indentations of the downstream peripheral edge of each web of the diffuser being aligned in the axial direction with the injectors to allow for a translation upstream of each injector in an indentation of each web for dismounting of the injector.