GAS TURBINE ENGINE COMPRISING MEANS FOR AXIALLY RETAINING A FAN OF THE ENGINE
The invention relates to a gas turbine engine comprising a case (5, 15) in which is mounted at least one shaft (2) for driving a fan (4) solidly connected to a driving drum (6) provided with blades (61) in order to compress an airflow moving from upstream to downstream in the engine. The engine comp...
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Sprache: | eng ; fre |
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