Method for the manufacturing of a hollow fiber reinforced structural member
The invention provides a method of manufacturing a hollow fiber reinforced structural member, in particular for air vehicles, comprising the steps of providing a first circular braiding layer, positioning a flat strengthening body comprising at least one fabric layer having warp fibers and a woof fiber against a part of the surface of the first braiding layer, providing a second braiding layer around the first braiding layer and the strengthening body, positioning the combination of the first braiding layer, the strengthening body and the second braiding layer in a mold, impregnating the combination with resin, removing the combination as impregnated with a resin from the mold.
1. Method of manufacturing a hollow fiber-reinforced structural member for air vehicles, comprising:
providing a mandrel,
providing a first circumferential braiding layer formed by braiding fibers around the mandrel,
positioning a flat strengthening body comprising at least one fabric layer having warp fibers and woof fibers against only a part of a surface of the first braiding layer,
providing a second braiding layer formed by braiding fibers around the first braiding layer and the strengthening body,
positioning the mandrel and a combination of the first braiding layer, the strengthening body and the second braiding layer in a mold which completely surrounds the mandrel and the combination,
impregnating the combination with resin, by injecting the flat strengthening body and the first braiding layer and the second braiding layer in the mold with the resin and
removing the combination as impregnated with the resin from the mold.
2. Method according to claim 1 , wherein the strengthening body comprises a stack of fabric layers.
3. Method according to claim 1 or claim 2 , wherein the resin is a thermo-setting resin.
4. Method according to claim 1 , wherein the braiding fiber, warp fibers and/or woof fibers are a glass fiber, a carbon fiber, an aramide fiber or a polyamide fiber.
5. The hollow fiber-reinforced structural member manufactured by a method according to claim 1 , the structural member comprising:
the first circular braiding layer;
the strengthening body comprising the at least one fabric layer having the warp fibers and the woof fibers, the strengthening body being positioned against only the part of the surface of the first braiding layer; and
the second braiding layer around the first braiding layer and the strengthening body,
wherein the combination of the first braiding layer, the strengthening body, and the second braiding layer is impregnated with the resin.
6. Method according to claim 2 , wherein the braiding fiber, warp fibers and/or woof fibers are a glass fiber, a carbon fiber, an aramide fiber or a polyamide fiber.
7. Method according to claim 3 , wherein the braiding fiber, warp fibers and/or woof fibers are a glass fiber, a carbon fiber, an aramide fiber or a polyamide fiber.
8. The hollow fiber-reinforced structural member manufactured by a method according to claim 2 , the structural member comprising:
the first circular braiding layer;
the strengthening body comprising the at least one fabric layer having the warp fibers and the woof fibers, the strengthening body being positioned against only the part of the surface of the first braiding layer; and
the second braiding layer around the first braiding layer and the strengthening body,
wherein the combination of the first braiding layer, the strengthening body, and the second braiding layer is impregnated with the resin.
9. The hollow fiber-reinforced structural member manufactured by a method according to claim 3 , the structural member comprising:
the first circular braiding layer;
the strengthening body comprising the at least one fabric layer having the warp fibers and the woof fibers, the strengthening body being positioned against only the part of the surface of the first braiding layer; and
the second braiding layer around the first braiding layer and the strengthening body,
wherein the combination of the first braiding layer, the strengthening body, and the second braiding layer is impregnated with the resin.
10. The hollow fiber-reinforced structural member manufactured by a method according to claim 4 , the structural member comprising:
the first circular braiding layer;
the strengthening body comprising the at least one fabric layer having the warp fibers and the woof fibers, the strengthening body being positioned against only the part of the surface of the first braiding layer; and
the second braiding layer around the first braiding layer and the strengthening body,
wherein the combination of the first braiding layer, the strengthening body, and the second braiding layer is impregnated with the resin.
11. Method according to claim 1 , wherein the part of the surface of the first braiding layer that the flat strengthening body is positioned against is an outer surface of the first braiding layer.
12. Method according to claim 1 , wherein the flat strengthening body is positioned against only a circumferential part of the surface of the first braiding layer.
13. Method according to claim 1 , wherein the combination as impregnated with the resin is removed from the mandrel.
14. Method according to claim 1 , wherein the flat strengthening body is positioned against only a circumferential part of the surface of the first braiding layer, and
wherein the combination as impregnated with the resin is removed from the mandrel.