Abstract: A preform has a fibrous reinforcement woven in one piece by three-dimensional weaving to create a fan inter-blade platform The platform includes an aerodynamic base and a fixing structure having stiffening elements that extend from the aerodynamic base. The preform includes a first fibrous part configured to form the aerodynamic base, second fibrous part configured to at least partially form the stiffening elements of the inter-blade platform, a first connection zone in which the first and second parts are woven together, and a first disconnection zone delimited by a first disconnection line extending in a transverse direction and in which the first and second parts are separated from one another. The first disconnection zone is adjacent to the first connection zone in a longitudinal direction L.

Abstract: The invention relates to a de-icing device designed to supply de-icing air to a turbomachine separation nozzle extending along a longitudinal axis, the turbomachine comprising:—the separation nozzle which is designed to be positioned downstream from a turbomachine fan and comprises an internal casing and an external casing which form a separation between a primary flow vein for a primary stream and a secondary flow vein for a secondary stream, said streams issuing from the fan, the internal casing and the external casing defining an inter-vein space;—turbomachine guide vanes designed to be secured by screws to the internal casing such that the screws extend into the inter-vein space, the de-icing device being intended to be positioned in the inter-vein space and comprising—an air inlet;—an air outlet;—a plurality of channels extending from the air inlet toward the air outlet; the channels being arranged in relation to one another such that they are designed to extend from the air inlet toward the air outlets,

Abstract: A turbine engine fan having an axis of revolution wherein a fan disk having an upstream face and a radial face is configured to receive a series of fan blades. An inter-blade platform wherein an upstream end, a blocking ferrule, are applied and attached on the one hand to the upstream end of the platform and on the other hand to the upstream face of the fan disk, and an inlet cone. The blocking ferrule includes a radial ring and a lug, extending axially from the radial ring and configured to form a radial abutment for the inlet cone.

Abstract: A fan includes: a fan disc; an inter-blade platform including a base and a radial tab, a second orifice being formed in the tab of the platform; and a lock having a downstream edge configured to bear against the tab of the platform. The one among the downstream edge and the yoke of the fan disc includes a pin, the other includes a first orifice, the pin being configured to enter the first orifice and the second orifice so as to block the platform relative to the fan disc.

Abstract: A turbine engine fan having an axis of revolution wherein a fan disk having an upstream face and a radial face is configured to receive a series of fan blades. An inter-blade platform wherein an upstream end, a blocking ferrule, are applied and attached on the one hand to the upstream end of the platform and on the other hand to the upstream face of the fan disk, and an inlet cone. The blocking ferrule includes a radial ring and a lug, extending axially from the radial ring and configured to form a radial abutment for the inlet cone.

Abstract: A fan includes: a fan disc; an inter-blade platform including a base and a radial tab, a second orifice being formed in the tab of the platform; and a lock having a downstream edge configured to bear against the tab of the platform. The one among the downstream edge and the yoke of the fan disc includes a pin, the other includes a first orifice, the pin being configured to enter the first orifice and the second orifice so as to block the platform relative to the fan disc.

Abstract: The invention relates to an automatic device for installing self-locking binder straps, said device comprising: two handles assembled so as to allow rotation relative to each other; a moving component carried by one of said handles and gripping the end of the strap in such a way that the relative movement of the handles tightens the strap; a cutter blade carried by one of said handles and operating when the strap is tightened to a predetermined extent.

Abstract: The invention relates to an automatic method for obtaining directly a moulded finished product provided with nails, e.g. clips for tubes or electric cables. The method comprises successively at a first station an injection phase in a mould defined by a fixed half-mould and a movable half-mould, a transfer phase to a second station of the movable half-mould bearing the moulded clips, a phase in which said clips are provided with nails at said second station and a phase in which the moulded clips, provided with nails are ejected, the cycle of the phases being resumed after the transfer of the movable half-mould to said first station.