CHAMBRE DE COMBUSTION DE TURBOMACHINE

摘要

The chamber has a monoblock annular fairing (53) comprising an upstream annular wall extended towards downstream by cylindrical inner and outer peripheral parts of the fairing. The fairing has another upstream annular wall (55) that forms a bypass surface to deviate solid particles i.e. sand, or liquid particles i.e. water, radially towards an exterior, where the particles are transported by supply air of the chamber. Air intake openings (52) are formed in the outer peripheral part of the fairing. The openings are supplied with portion of the air deviated by the latter annular wall.