Abstract:
There is disclosed a method of checking headpath data for a layup operation in which fibre reinforcement material is applied over a tool by an applicator roller of an applicator head biased against the tool along a compaction axis by a compaction force. The method comprises receiving baseline headpath data defining a baseline headpath position of the applicator head relative the tool; and determining a head displacement along the compaction axis corresponding to an equilibrium condition between the compaction force and a reaction force through the fibre reinforcement material. The method further comprises checking for at least one of a non-compacted portion of fibre reinforcement material and an intersection of the applicator head and an obstacle.
Abstract:
Methods and apparatus are described for improving fit checking at the bonding interface of a first component, such as a fan blade (1), and a second component, such as an edge guard (2) for the fan blade (1), to be bonded by adhesive. A bondline thickness profile over the area of the bonding interface is determined by interposing a compressible, flexible sensor layer between the components before they are bonded. The sensor layer contains an array of piezoelectric elements which indicate local bondline thickness by signalling pressure due to compression of the layer. The bondline thickness profile can be processed by a programmed control processor to produce an adhesive application schedule prescribing the shapes of pieces of adhesive film which, when applied over the bonding interface, will build up an adhesive layer corresponding in thickness to the bondline thickness. The sensor layer can be prepared as a kit of shaped panels or as a contoured preform (55) matching the form of the bonding interface.
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 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 tool (102) for forming a composite component having a curved body and an integral flange from a pre-form (200), the tool comprising: a curved body portion 104 having a lay-up surface (110); and a forming assembly (105) having a lay-up configuration and a forming configuration. The forming assembly comprises: a plurality of forming elements (106) each having a lay-up surface (120) and a primary flange-forming surface (122), the forming elements (106) being radially outwardly moveable between the lay-up configuration and the forming configuration, in which the forming elements are circumferentially spaced from one another; and a plurality of filler elements (107) each having a secondary flange-forming surface (156), the filler elements (107) being arranged to move into the circumferential gaps between the forming elements in the forming configuration so as to form a substantially continuous flange-forming surface. In use a pre-form (200) is disposed on the layup surfaces of the curved body portion (104) and the forming elements (106), and movement to the forming configuration causes the pre-form (200) to be deformed between the continuous flange-forming surface and a counteracting forming surface to form the integral flange (210).
Abstract:
There is disclosed a self-heating tool (10) for manufacturing a composite component, comprising: a support structure (24); a mandrel (26) onto which composite material can be applied; a heater (58) for heating the mandrel (26) during a curing operation; and a plurality of extendible support members (28) extending between the support structure (24) and the mandrel (26) to support the mandrel (26). Each extendible support member (28) is configured to change in length in response to thermal expansion of the mandrel (28) during a curing operation. A method of manufacturing a composite component using a self-heating tool is also disclosed.
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 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:
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.
Abstract:
There is provided a lay-up head (18) for applying elongate fibre reinforcement material (14) to an application surface (12). The lay-up head (18) comprises a support head (20) having a transverse axis T, a dispensing mechanism (28) carried by the support head for dispensing elongate fibre reinforcement material (14), and a roller (24) for pressing elongate fibre composite material (14) against the application surface (12). The roller (24) is tiltable with respect to the support head (20) such that the roller axis R can be angled with respect to the transverse axis T of support head (20). The lay-up head (18) also comprises a holding mechanism (40) operable to hold the roller (24) in a central position in which the roller axis R is parallel to the transverse axis T of the support head.