초록 ▼

A method of moulding articles from layers of composite material being fibres impregnated with uncured resin, includes draping at least one layer of the composite material over a moulding tool, applying over the composite material layer or layers a membrane, and establishing an at least partial vacuu

A method of moulding articles from layers of composite material being fibres impregnated with uncured resin, includes draping at least one layer of the composite material over a moulding tool, applying over the composite material layer or layers a membrane, and establishing an at least partial vacuum between the membrane and the moulding tool to consolidate the composite material, and wherein the membrane is made of a resilient material, and the method includes applying a force to the membrane to stretch the membrane over the moulding tool and maintaining the force whilst the at least partial vacuum is established.

대표청구항 ▼

1. A method of moulding articles from layers of composite material comprising fibres impregnated with uncured resin, using a moulding apparatus including a male moulding tool, and a frame affording an opening, and the opening having therein a membrane of resilient material, the method including drap

1. A method of moulding articles from layers of composite material comprising fibres impregnated with uncured resin, using a moulding apparatus including a male moulding tool, and a frame affording an opening, and the opening having therein a membrane of resilient material, the method including draping at least one layer of the composite material over the moulding tool, applying the membrane over the at least one layer of composite material, and establishing an at least partial vacuum between the membrane and the moulding tool to consolidate the composite material, the method further including, prior to applying the at least partial vacuum, positioning the frame in a first position in which portions of the frame are disposed on opposite sides of the moulding tool and the membrane is disposed in an unstretched condition on the moulding tool, moving the frame from the first position, in a direction towards the tool, to a second position wherein said portions of the frame disposed on opposite sides of the moulding tool are spaced along the moulding tool from said first position and the membrane is stretched over the moulding tool during movement of the frame between said first and second positions, and wherein a stretching force is applied to the membrane in the second position of said frame such as to provide stretching of the membrane over the moulding tool sufficient to consolidate the at least one layer of composite material, and maintaining the frame in the second position to maintain the force on the at least one layer whilst the at least partial vacuum is established, the method further including applying heat to the composite material with the membrane in a stretched condition and with the at least partial vacuum established, to cause or promote curing of the uncured resin, the resin being a thermosetting resin, and the method further including placing the moulding tool, uncured composite material, and stretched membrane in an autoclave in which the composite material is subjected to heat. 2. A method according to claim 1 wherein the resilient membrane material is an elastomeric material.3. A method according to claim 2 wherein the method includes re-using the membrane material to consolidate further layers of composite material.4. A method according to claim 1 wherein the method includes consolidating and de-baulking individual composite materials prior to the resin being cured.5. A method according to claim 1 wherein the method includes consolidating and de-baulking a plurality of individual layers of the composite material prior the resin being cured.6. A method according to claim 1 wherein in the autoclave, the moulding tool, uncured composite material, and stretched membrane are subjected to pressure.7. A method according to claim 1 wherein the article is elongate and the membrane is applied over at least a substantial part of the axial extent of the article.8. A method according to claim 7 wherein the article is a leading edge spar of a helicopter rotor blade.