Turbomachine auxiliary lead-through device
AssigneeSafran Aircraft Engines
InventorNicolas Stoliaroff-Pepin
Life of this patent
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AssigneeSafran Aircraft Engines
InventorNicolas Stoliaroff-Pepin
Estimating the term…
Auxiliary lead-through device for a turbomachine, including two coaxial annular shell rings, respectively an inner and an outer one, between which there extend radial arms, through at least one of which auxiliaries (20) are led through. An auxiliary retention unit is housed inside the arm, on one wall, the arm includes an aperture that can be closed off by a cover that is attached and fixed to the arm. The retention unit includes at least one first member fixed to the internal surface of the arm and at least one second member fixed to the internal surface of the cover. The fixing of the cover to the arm causes the auxiliaries to be clamped and retained between the first and second members.
A device for leading through auxiliary systems for a turbine engine, comprising two respectively inner and outer coaxial annular collars, between which radial arms extend, and supports for supporting said auxiliary systems,
A radial arm of a device for leading through auxiliary systems of a turbine engine, wherein said radial arm comprises:
Dependencies are inferred from the claim text.