Flow straightener unit comprising a centering and attachment plate
The invention concerns a flow straightener unit ( 1 ) for a fan module of a turbomachine, the straightener unit ( 1 ) comprising a plurality of blades ( 2 ) distributed about an axis of rotation, each blade ( 2 ) is made of a composite material and comprises an aerofoil ( 21 ) and a root ( 22 ) intended to be assembled on a hub ( 4 ) of the turbomachine. The unit ( 1 ) comprises a centring and attachment plate ( 3 ) of the blade ( 2 ) on the turbomachine intended to be attached to the hub ( 4 ) at a determined azimuthal position and to the root ( 22 ) of the blade ( 2 ), the plate ( 3 ) is designed to be screwed to the hub ( 4 ) by screws ( 51 a ) that are longitudinal with respect to the axis of rotation of the unit ( 1 ) and screwed to the root ( 22 ) of the blade ( 2 ) by screws ( 52 ) that are radial with respect to the axis of rotation of the unit ( 1 ).
1. A flow straightener assembly for a fan module of a turbomachine, the flow straightener assembly comprising:
a plurality of blades distributed about an axis of revolution of the flow straightener assembly, each blade of the plurality is made of a composite material, each blade having a vane and a root configured to be assembled to a hub of a turbomachine; and
a centering and fastening plate configured to be fastened to the hub at a determined azimuthal position and to the root of one blade of the plurality of blades, the centering and fastening plate configured to be fastened to the hub by screws extending longitudinally relative to the axis of revolution of the flow straightener assembly and attached to the root by screws extending radially relative to the axis of revolution of the assembly.
2. The flow straightener assembly of claim 1 , wherein the plate has a radial section having a L or S or triangular shape.
3. The flow straightener assembly of claim 1 , wherein the root is fastened to the hub only via the plate.
4. The flow straightener assembly of claim 1 , wherein the root has a leading portion and a trailing portion, the leading portion of the root being fastened directly to the hub and the trailing portion of the root being fastened to the hub via the plate.
5. The flow straightener assembly of claim 1 , wherein the plate is made of metal.
6. The flow straightener assembly of claim 1 , wherein a platform is positioned between the root and the vane, the platform having a conical radial section configured to having a deflector function for an air flow.
7. The flow straightener assembly of claim 6 , wherein the platform is integral with the vane.
8. The flow straightener assembly of claim 6 , wherein the platform is an element separable from the vane, and is fastened to the vane.
9. A turbomachine comprising:
a fan module;
a hub on which the fan module is mounted; and
a flow straightener assembly comprising:
a plurality of blades distributed about an axis of revolution of the flow straightener assembly, each blade having a vane and a root fastened to the hub of the turbomachine, and
a respective centering and fastening plate fastened to the hub at a determined azimuthal position and to the root of each respective blade of the plurality of blades, the centering and fastening plate fastened to the hub by screws extending longitudinally relative to the axis of revolution of the flow straightener assembly and attached to the root by screws extending radially relative to the axis of revolution of the assembly.
10. A method for assembling a flow straightener assembly in a turbomachine, the method comprising:
fastening a centering and fastening plate to a blade of a flow straightener assembly, the blade being made of a composite material, the blade having a vane and a root, the centering and fastening plate fastened to the root of the blade by screws extending radially relative to an axis of revolution of the flow straightener assembly; and
fastening the centering and fastening plate to a hub of a turbomachine at a determined azimuthal position, the centering and fastening plate fastened to the hub by screws extending longitudinally relative to the axis of revolution of the flow straightener assembly.