| 摘要 |
Turbomachine comprising an annular combustion chamber (48) comprising two, a radially inner (24) and a radially outer (26), walls exhibiting symmetry of revolution, which are connected at their upstream ends by an annular chamber end wall (28) equipped with fuel-injection means, which turbomachine comprises suspension means (50) for suspending the upstream end of the combustion chamber (48) from an outer casing (18).
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