Device for fabricating a composite material part

1. A device for fabricating a composite material part by injecting resin into a fiber structure, the device comprising:

a first die configured to support the fiber structure, the first die presenting two adjacent support surfaces defining a reentrant angle between them;

at least one chock presenting first and second adjacent faces together defining a wedge-shaped portion configured to press the fiber structure into the angle; and

a second die that is movable relative to the first die, the first and second dies being configured to clamp on the fiber structure and the chock such that the first die, the second die, and the chock together define, in a closed position, a resin injection space surrounding the fiber structure;

wherein the chock is connected to the second die by at least one link, the link being hinged relative to the second die and to the chock to guide the wedge-shaped portion towards the angle to press the fiber structure into the angle, when the second die approaches the first die, and

wherein the first die is a mandrel around which the fiber structure is wound, the mandrel comprising a central wall and at least one cheekplate, the central wall and the cheekplate defining said adjacent support surfaces.

2. A device according to claim 1 , wherein a third face of the chock presses against the second die in the closed position, the third face being opposite from the first and second faces.

3. A device according to claim 2 , further comprising a gasket arranged between the third face and the second die around the link.

4. A device according to claim 1 , wherein the chock is connected to the second die by at least one pair of mutually parallel links.

5. A device according to claim 1 , wherein the link is hinged to shells configured to be inserted in respective cavities formed in the chock and in the second die.

6. A device according to claim 1 , having a plurality of chocks, wherein each chock is in a form of a ring segment, the chocks being arranged end to end to cover an entire circumference of the mandrel.

7. A method of fabricating a composite material part, comprising:

injecting, resin into a fiber structure using a device, the device including:

a first die configured to support the fiber structure, the first die presenting two adjacent support surfaces defining a reentrant angle between them;

at least one chock presenting first and second adjacent faces together defining a wedge-shaped portion configured to press the fiber structure into the angle; and

a second die that is movable relative to the first die, the first and second dies being configured to clamp on the fiber structure and the chock such that the first die, the second die, and the chock together define, in a closed position, a resin injection space surrounding the fiber structure;

wherein the chock is connected to the second die by at least one link, the being hinged relative to the second die and to the chock to guide the wedge-shaped portion towards the angle to press the fiber structure into the angle, when the second die approaches the first die, and

wherein the first die is a mandrel around which the fiber structure is wound, the mandrel comprising a central wall and at least one cheekplate, the central wall and the cheekplate defining said adjacent support surfaces.

8. A method of fabricating a composite material part according to claim 7 , wherein the part is an aeroengine fan casing, the casing including a main wall and at least one fastener flange, the reentrant angle corresponding to a salient angle formed between the main wall and the fastener flange.