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US08925331B2 Annular combustion chamber of a turbomachine 有权
涡轮机的环形燃烧室

Annular combustion chamber of a turbomachine
Abstract:
An annular combustion chamber for a turbomachine presenting an axial direction, a radial direction, and an azimuth direction, the combustion chamber including a first annular wall and a second annular wall, each annular wall defining at least a portion of an enclosure of the combustion chamber. The first annular wall and the second annular wall present complementary assembly mechanisms that co-operate by engagement in azimuth.
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