GAS TURBINE ENGINE FIBRE-REINFORCED COMPOSITE MATERIAL COMPONENT WITH PROTECTIVE SHIELD, AND CORRESPONDING MANUFACTURING METHOD

A method of manufacturing a component for a gas turbine engine includes applying a thermoplastic polymer sheet over a composite body for the component; applying a shield over part of the composite body, the shield terminating at an end which overlies the thermoplastic polymer sheet and defines an in...

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Bibliographische Detailangaben
Hauptverfasser: CHURCHER, David, COLLIS, Andrew R
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:A method of manufacturing a component for a gas turbine engine includes applying a thermoplastic polymer sheet over a composite body for the component; applying a shield over part of the composite body, the shield terminating at an end which overlies the thermoplastic polymer sheet and defines an interface between shielded and unshielded regions of the component; and pressing the shield into the thermoplastic polymer sheet so that the thermoplastic polymer sheet deforms around the end of the shield, such that the exterior profile of the component at the interface between the shielded and unshielded regions is flush.