Tool for balancing a turbine engine module comprising a cantilevered stator
AssigneeSafran Aircraft Engines
InventorsAlain Roland Luinaud, Alain Decocq
Life of this patent
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AssigneeSafran Aircraft Engines
InventorsAlain Roland Luinaud, Alain Decocq
Estimating the term…
A tool for balancing a turbine engine module in a balancer, the module including a stator, a rotor and a shaft, the balancer including at least one power drive unit and a table equipped with two support of the shaft of the module. The tool includes at least: one stator support, fixed on the table of the balancer behind the supports, a tubular false bearing, configured to support a bearing for guiding the rotor in the stator and protruding outside of the stator, a guiding sleeve of the shaft, confining a support of the false bearing, and received on the supports of the balancer, a rear support plate of the stator, fixed to the support of the stator, and immobilising the rotor with respect to the stator, a front support plate of the stator, fixed to the stator support, and immobilising and centring the false bearing.
Tool for balancing a turbine engine module in a balancer, said module comprising at least one stator and one rotor comprising a shaft of longitudinal axis A configured to be guided by a guiding bearing inside the stator and at least one blades stage which is connected to a longitudinal end portion of said shaft and which is surrounded by said stator, and said balancer comprising at least, from the front to the rear, a power drive unit and a table provided with two front and rear supports for maintaining the shaft of the module, wherein said tool comprises at least:
Dependencies are inferred from the claim text.