Sandwich core material
View Patent ↗A sandwich core material for a sandwich laminate is disclosed. The sandwich core material includes a number of flexible core material elements having a longitudinal structure. A flexible core material for a sandwich core material, a sandwich laminate and a wind turbine blade including such a sandwich core material are provided. In addition, the present a method of manufacturing such a sandwich core material is provided.
1. A process for manufacturing a sandwich core material comprising:
deploying a plurality of flexible core material elements from a roll or a bobbin having the flexible core material elements wound thereon, each of the flexible core material elements having a longitudinal structure, wherein each of the core material elements is formed as a tow from a plurality of hollow tubes being connected together, where one of the plurality of hollow tubes is in the middle and the remaining of the plurality of hollow tubes are arranged around the middle hollow tube;
arranging the flexible core material elements from the bobbin or roll in a mould;
after the arranging, cutting the flexible core material elements to a desired dimension to form a layer in the mould; and
repeating the process at least once until the layers in the mould comprise a desired thickness and shape of the sandwich core material; and
bonding the material layers together to one another to form the sandwich core material.
2. The process of claim 1 , wherein the arranging is done by a robot device which arranges the flexible core material elements in the mould.
3. The process of claim 2 , wherein the robot device comprises a placement head for arranging the flexible core material elements in the mould.
4. The process of claim 1 , wherein the flexible core material elements comprise a plastic or a resin on an outer surface thereof, and wherein the process further comprises heating the material layers to form the sandwich core material.
5. The process of claim 1 , wherein the bonding is done by:
placing a first and a second skin layer on a surface of the flexible core material elements and applying heat and/or pressure to form the sandwich core material.
6. The process of claim 1 , wherein the plurality of hollow tubes is connected by helical threads wound around the plurality of hollow tubes.
7. The process of claim 1 , wherein the flexible core material element comprises reinforcement fibres about a perimeter thereof.
8. The process of claim 1 , wherein the flexible core material elements comprise a sandwich skin layer on a first and/or a second surface of the flexible material core elements.
9. The process of claim 1 , wherein the plurality of hollow tubes is connected by a bonding at their respective contact points.
10. The process of claim 9 , wherein the plurality of hollow tubes is further connected by helical threads wound around the plurality of hollow tubes.