Abstract: There is disclosed a lay-up head for applying elongate fiber reinforcement material to an application surface. The lay-up head comprises a guide eyelet through which elongate fiber reinforcement material is arranged to pass into the lay-up head. The guide eyelet has an eyelet rim forming a discontinuous contact surface over which elongate fiber reinforcement material is arranged to pass.

Abstract: There is disclosed a cutting mechanism for severing elongate fiber reinforcement material in composite material lay-up equipment, the cutting mechanism comprising a cutting element and a counteracting element which cooperate to sever fiber reinforcement material extending through the nip between them, the cutting element being mounted on an elongate arm which is pivotable about a pivot axis A spaced from the nip, to displace the cutting element relatively to the counteracting element to perform a cutting stroke, the mechanism further comprising guide means arranged to guide the fiber reinforcement material through the nip in a feed direction transverse to the pivot axis A, and an actuation device for driving the elongate arm in a cutting stroke, the actuation device acting on the elongate arm at a position away from the cutting element. There is also provided composite material lay-up equipment comprising the cutting mechanism.

Abstract: There is disclosed a method of forming a composite component having a curved body and an integral flange from a pre-form (200) using forming apparatus comprising: a tool (102) comprising a curved body portion (104) having a lay-up surface (110) and a forming assembly (105) comprising a plurality of forming elements (106) each having a lay-up surface (120) and a primary flange-forming surface (122); and a plurality of filler elements (107) each having a secondary flange-forming surface (156).

Abstract: There is disclosed composite material lay-up equipment for applying a plurality of individual lengths of elongate fiber reinforcement material to an article, the equipment comprising: a support head; a cutting mechanism carried by the support head for severing a plurality of individual lengths of elongate fiber reinforcement material. The cutting mechanism comprises a plurality of cutting elements coupled to and moveable with respect to the support head and a cassette removably attached to the support head and having a plurality of corresponding counteracting elements statically mounted thereto. Each cutting element is displaceable relative to the corresponding counteracting element to perform a cutting stroke in which the respective cutting and counteracting elements cooperate to sever a length of elongate fiber reinforcement material extending through the nip formed between them.

Abstract: A containment arrangement for a gas turbine engine comprises: a radially outer annular casing (12); a fan track liner (28) radially within the casing comprising: an impact region (30) comprising a cellular material having a first compressive strength; at least one elongate ridge portion (26) extending through the impact region in a direction having an axial component, the ridge portion having a second compressive strength higher than the first compressive strength; and a gas-washed layer (38) radially within the fan track liner.

Abstract: There is disclosed composite material lay-up equipment 10 for applying a plurality of individual lengths of elongate fiber reinforcement material 14 to an article 12, the equipment 10 comprising: a support head 20; a cutting mechanism 22 carried by the support head 20 for severing a plurality of individual lengths of elongate fiber reinforcement material 14. The cutting mechanism 22 comprises a plurality of cutting elements 60 coupled to and moveable with respect to the support head 20 and a cassette 65 removably attached to the support head 20 and having a plurality of corresponding counteracting elements 76 statically mounted thereto. Each cutting element 60 is displaceable relative to the corresponding counteracting element 76 to perform a cutting stroke in which the respective cutting and counteracting elements 60, 76 cooperate to sever a length of elongate fiber reinforcement 14 material extending through the nip formed between them.

Abstract: There is disclosed a cutting mechanism 22 for severing elongate fiber reinforcement material 14 in composite material lay-up equipment 10, the cutting mechanism 22 comprising a cutting element 60 and a counteracting element 76 which cooperate to sever fiber reinforcement material 14 extending through the nip between them, the cutting element 60 being mounted on an elongate arm 44 which is pivotable about a pivot axis A spaced from the nip, to displace the cutting element 60 relatively to the counteracting element 76 to perform a cutting stroke, the mechanism 22 further comprising guide means 52 arranged to guide the fiber reinforcement material 14 through the nip in a feed direction transverse to the pivot axis A, and an actuation device 84 for driving the elongate arm 44 in a cutting stroke, the actuation device 84 acting on the elongate arm 44 at a position away from the cutting element 60. There is also provided composite material lay-up equipment 10 comprising the cutting mechanism 22.

Abstract: A composite aerofoil, the aerofoil having a leading edge, a trailing edge a pressure side and a suction side and comprising an outer erosion protection layer along one or both of the pressure side or suction side, a structural core having a plurality of resin impregnated plies of unidirectional fibers, and between the outer erosion protection layer and the structural core a woven composite impregnated with a resin having a modulus of elasticity greater than that of the resin impregnating the plies in the structural core.

Abstract: There is disclosed a cutting mechanism 22 for severing elongate fibre reinforcement material 14 in composite material lay-up equipment 10, the cutting mechanism 22 comprising a cutting element 60 and a counteracting element 76 which cooperate to sever fibre reinforcement material 14 extending through the nip between them, the cutting element 60 being mounted on an elongate arm 44 which is pivotable about a pivot axis A spaced from the nip, to displace the cutting element 60 relatively to the counteracting element 76 to perform a cutting stroke, the mechanism 22 further comprising guide means 52 arranged to guide the fibre reinforcement material 14 through the nip in a feed direction transverse to the pivot axis A, and an actuation device 84 for driving the elongate arm 44 in a cutting stroke, the actuation device 84 acting on the elongate arm 44 at a position away from the cutting element 60. There is also provided composite material lay-up equipment 10 comprising the cutting mechanism 22.

Abstract: There is disclosed composite material lay-up equipment 10 for applying a plurality of individual lengths of elongate fibre reinforcement material 14 to an article 12, the equipment 10 comprising: a support head 20; a cutting mechanism 22 carried by the support head 20 for severing a plurality of individual lengths of elongate fibre reinforcement material 14. The cutting mechanism 22 comprises a plurality of cutting elements 60 coupled to and moveable with respect to the support head 20 and a cassette 65 removably attached to the support head 20 and having a plurality of corresponding counteracting elements 76 statically mounted thereto. Each cutting element 60 is displaceable relative to the corresponding counteracting element 76 to perform a cutting stroke in which the respective cutting and counteracting elements 60, 76 cooperate to sever a length of elongate fibre reinforcement 14 material extending through the nip formed between them.