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1. A method for connecting a first composite member comprising first fibres composed of a first material and a first resin to a second composite member comprising a second resin and second fibres composed of a second material different than the first material, using a connection comprising a layered structure comprising a transition member, the method comprising: assembling the transition member, which includes: providing at least two first layers composed of the first fibres, the first fibres being fully oriented in each first layer;providing at least t...
1. A method for connecting a first composite member comprising first fibres composed of a first material and a first resin to a second composite member comprising a second resin and second fibres composed of a second material different than the first material, using a connection comprising a layered structure comprising a transition member, the method comprising: assembling the transition member, which includes: providing at least two first layers composed of the first fibres, the first fibres being fully oriented in each first layer;providing at least two second layers composed of the second fibres, the second fibres being fully oriented in each second layer;interlacing the at least two first layers and the at least two second layers into partially overlapping relation such that at least one of the first layers is positioned adjacent to and between two second layers and extends in its plane beyond the two adjacent second layers, and at least one of the second layers is positioned adjacent to and between two first layers and extends in its plane beyond the two adjacent first layers;providing a resin in contact with at least one of the first or second layers to form the transition member;connecting the transition member to the first composite member;connecting the transition member to the second composite member; andcuring the transition member. 2. The method of claim 1, further comprising co-curing the first and/or the second composite member with the curing of the transition member. 3. The method of claim 1, further comprising pre-consolidating the transition member. 4. The method of claim 1, wherein the first composite member and the second composite member are joined together, substantially end-to-end, via the transition member, in a direction of respective longitudinal planes of the first layer and the second layer. 5. The method of claim 1, wherein the first resin, the second resin, and the resin in contact with at least one of the first or second layers are composed of a thermosetting resin, and wherein the first material has at least one physical property such as a coefficient of thermal expansion or Young's modulus that is different than the same physical property of the second material. 6. A method for connecting a first composite member comprising first fibres composed of a first material and a first resin to a second composite member comprising a second resin and second fibres composed of a second material different than the first material, via a connection comprising a layered structure which forms a transition zone, the transition zone comprising respective layers of the first fibres and the second fibres, the method comprising: providing the first composite member;providing the second composite member;assembling the transition zone, which includes: providing at least two first layers for forming part of a layered structure and comprising first layer fibres having substantially the same composition as the first fibres, the first layer fibres being one of: (i) the first fibres of the first composite member,(ii) connected to the first composite member, and(iii) on a previous layer comprising fibres which form part of the layered structure in the transition zone;providing at least two second layers, which, with the at least two first layers, forms the layered structure of the transition zone, the at least two second layers comprising second layer fibres having substantially the same composition as the second fibers, the second layer fibres being one of: (i) part of the first composite member,(ii) connected to the first composite member, and(iii) on a previous layer of the layered structure of the transition zone,interlacing the at least two first layers and the at least two second layers into partially overlapping relation such that at least one of the first layers is positioned adjacent to and between two second layers and extends in its plane beyond the two adjacent second layers, and at least one of the second layers is positioned adjacent to and between two first layers and extends in its plane beyond the two adjacent first layers; andproviding a resin in contact with at least one of the first or second layers comprising fibres in the layered structure;connecting the layered structure to the second composite member; andcuring the transition zone. 7. The method of claim 6, further comprising co-curing the first and/or the second composite members together with the curing of the transition zone. 8. The method of claim 6, wherein the first composite member and the second composite member are joined together, substantially end-to-end, via the transition zone, in a direction of respective longitudinal planes of the first layer and the second layer. 9. The method of claim 6, wherein the first resin, the second resin, and the resin in contact with at least one of the first or second layers are composed of a thermosetting resin, and wherein the first material has at least one physical property such as a coefficient of thermal expansion or Young's modulus that is different than the same physical property of the second material. 10. A method for connecting a first composite member comprising first fibres composed of a first material and a first resin to a second composite member comprising a second resin and second fibres composed of a second material different than the first material, via a connection comprising a layered structure which forms a transition zone, wherein the transition zone is integrated at least partially with the first composite member, the method comprising: providing a first composite member comprising first layers, wherein at least two of the first layers extends into a transition zone and includes first fibres that are fully oriented with each other;providing at least two second layers extending into, the transition zone, and including second fibres that are fully oriented with each other,interlacing the at least two first layers and the at least two second layers into partially overlapping relation in the transition zone to form a layered structure such that at least one of the first layers is positioned adjacent to and between two second layers and extends in its plane beyond the two adjacent second layers, and at least one of the second layers is positioned adjacent to and between two first layers and extends in its plane beyond the two adjacent first layers;providing a resin in contact with at least one of the first and second layers;connecting the first composite member to the second composite member; andcuring the transition zone and the first composite member. 11. The method of claim 10, further comprising co-curing the second composite member together with the curing of the transition zone. 12. The method of claim 11, further comprising pre-consolidating the transition zone. 13. The method of claim 12, further comprising pre-consolidating the first composite member. 14. The method of claim 10, further comprising providing a means for at least partially immobilizing the fibres. 15. The method of claim 10, wherein connecting the first composite member to the second composite member comprises connecting the second composite member to the second layers of the transition zone. 16. The method of claim 10, wherein the first composite member and the second composite member are joined together, substantially end-to-end, via the transition zone, in a direction of respective longitudinal planes of the first layer and the second layer. 17. The method of claim 10, wherein the first resin, the second resin, and the resin in contact with at least one of the first or second layers are composed of a thermosetting resin, and wherein the first material has at least one physical property such as a coefficient of thermal expansion or Young's modulus that is different than the same physical property of the second material. 18. A method for connecting a first composite member comprising first fibres composed of a first material and a first resin to a second composite member comprising a second resin and second fibres composed of a second material different than the first material, via a connection comprising a layered structure which forms a transition zone, the method comprising: providing at least two first layers comprising first fibres and extending outward from the first composite member to form a first composite member extending structure that extends into the second composite member;providing at least two second layers comprising second fibres and extending outward from the second composite member to form a second composite member extending structure, the second composite member extending structure being complementary to the first composite member extending structure;providing a resin in contact with at least one of the first layers or the second layers;mating the first layer extending structure with the second layer extending structure to thereby form a transition zone, the mating including interlacing the at least two first layers and the at least two second layers into partially overlapping relation such that at least one of the first layers is positioned adjacent to and between two second layers and extends in its plane beyond the two adjacent second layers, and at least one of the second layers is positioned adjacent to and between two first layers and extends in its plane beyond the two adjacent first layers; andcuring the transition zone. 19. The method of claim 18, further comprising providing a means for at least partially immobilizing the fibres. 20. The method of claim 18, further comprising pre-consolidating the transition zone. 21. The method of claim 18, wherein the fibres for at least one of the first layers and the second layers are selected from one or more of the group consisting of prepregs, semi-pregs, woven or non-woven fabrics, mats, pre-forms, pre-consolidated pre-forms, individual or groups of fibres, tows, tow-pregs and a combination thereof. 22. The method of claim 18, wherein at least a part of the resin is introduced by at least one of resin infusion, resin transfer moulding, and vacuum assisted resin transfer moulding. 23. The method of claim 18, wherein the curing involves providing of a pressure and/or a vacuum on the transition zone. 24. The method of claim 23, wherein the pressure and/or vacuum on the transition zone commences before the curing of the transition zone. 25. The method of claim 18, wherein the first composite member and the second composite member are joined together, substantially end-to-end, via the transition zone, in a direction of respective longitudinal planes of the first layer and the second layer. 26. The method of claim 18, wherein the first resin, the second resin, and the resin in contact with at least one of the first or second layers are composed of a thermosetting resin, and wherein the first material has at least one physical property such as a coefficient of thermal expansion or Young's modulus that is different than the same physical property of the second material.
