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COMBUSTION CHAMBER FOR A TURBOMACHINE

机译:涡轮机燃烧室

摘要

The invention relates to a combustion chamber comprising a bottom wall (4) comprising at least one opening (5), at least one sleeve (12) mounted upstream of the bottom wall (4) and fixed to the bottom wall. (4), a closure ring (13) delimiting an annular groove (11) with the sheath (12) and fixed to the sheath (12), at least one system (6) for injecting air and fuel, having an axis (A), mounted in the opening (5) of the bottom wall (4), the injection system (6) comprising an annular flange (10) extending radially relative to said axis (A), mounted in said groove (11) with a radial clearance, a deflector (14) located downstream of the bottom wall (4), fixed to the sheath (12) and / or to the bottom wall (4).
机译:本发明涉及一种燃烧室,该燃烧室包括:底壁(4),其包括至少一个开口(5);至少一个套筒(12),其安装在底壁(4)的上游并固定至底壁。 (4),一个封闭环(13),其与护套(12)界定环形凹槽(11),并固定在护套(12)上,至少一个用于注入空气和燃料的系统(6)具有轴线(A) ),安装在底壁(4)的开口(5)中的注射系统(6)包括相对于所述轴线(A)径向延伸的环形法兰(10),该环形法兰(10)径向安装在所述凹槽(11)中间隙中,位于底壁(4)下游的偏转器(14)固定在护套(12)和/或底壁(4)上。

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