Air inlet intended to be connected to a fan casing of a turbine engine by a flange-type assembly and propulsion assembly comprising a turbine engine equipped with such an air inlet
AssigneeSafran Nacelles
InventorsAlexis Yves-Marie LONCLE, Jeremie RABINEAU
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Abstract
An air inlet to be connected to a fan casing of a turbine engine by a flange-type assembly. The air inlet includes an annular structure of longitudinal axis including an inner shroud and an outer shroud, the inner shroud at least partially delimiting a radially outer wall of a flow path for an airflow in the turbine engine in a substantially longitudinal direction. The air inlet includes a flange having a bearing face of a clamping member. The air inlet is arranged such that the bearing face is accessible from the flow path via an access port. A propulsion assembly includes such an air inlet.
Claims10
An air inlet intended to be connected to a fan casing of a turbine engine by a flange-type assembly, the air inlet comprising an annular structure of longitudinal axis comprising an inner shroud and an outer shroud,
- the inner shroud at least partially delimiting a radially outer wall of a flow path of an airflow through the air inlet in a substantially longitudinal direction, the air inlet comprising a flange having a bearing face of a clamping member the air inlet being arranged such that the bearing face is accessible from the flow path via an access port.
Dependencies are inferred from the claim text.