Tube having a hybrid-type structure, in particular for an aircraft seat
A hybrid tube, in particular for an aircraft seat structure includes ribs intended to receive the hybrid tube. The hybrid tube includes a monolithic carbon tube and at least one sleeve made from a ductile material and connected to the carbon tube by means of gluing, shrink-fitting or over-molding.
1. A seat structure comprising:
a first reinforcement structure having an L-shape;
a second reinforcement structure having an L-shape, wherein the second reinforcement structure is separated by the first reinforcement structure by a gap;
a hybrid tube that spans the gap and is attached to both the first reinforcement structure and the second reinforcement structure, wherein the hybrid tube comprises:
a monolithic carbon tube comprising carbon fibers; and
a cylindrical sleeve piece of ductile material comprising a peripheral end chamfer, wherein the cylindrical sleeve piece has a length smaller than a length of the monolithic carbon tube, and the cylindrical sleeve piece is added on to and fixed to the monolithic carbon tube by gluing or shrink fitting.
2. The seat structure according to claim 1 , wherein the monolithic carbon tube is a tube made by pultrusion.
3. The seat structure according to claim 1 , wherein the cylindrical sleeve piece comprises a second peripheral end chamfer.
4. The seat structure according to claim 1 , wherein the cylindrical sleeve piece is made of a metallic material.
5. The seat structure according to claim 4 , wherein the metallic material is an aluminum alloy.
6. The seat structure according to claim 4 , wherein the cylindrical sleeve piece is made of a thermoplastic material, added on to and fixed to the monolithic carbon tube by gluing, shrink fitting, or over-molding.
7. The seat structure according to claim 4 , wherein the cylindrical sleeve piece is disposed on an outside portion of the monolithic carbon tube.
8. The seat structure according to claim 4 , wherein the cylindrical sleeve piece is disposed on an inside portion of the monolithic carbon tube.
9. A seat structure comprising:
a first reinforcement structure having a first hole and a second hole;
a second reinforcement structure having a third hole and a fourth hole, wherein the second reinforcement structure is separated by the first reinforcement structure by a gap; and
a first hybrid tube passing through the first hole and the third hole, wherein the first hybrid tube comprises:
a first monolithic carbon tube; and
a first sleeve of ductile material disposed at a right angle to the first hole and the third hole, wherein the first hybrid tube is added on to and fixed to the first monolithic carbon tube by gluing or shrink fitting; and
a second hybrid tube passing through the second hole and the fourth hole, wherein the second hybrid tube comprises:
a second monolithic carbon tube; and
a second sleeve of ductile material disposed at a right angle to the second hole and the fourth hole, wherein the second hybrid tube is added on to and fixed to the second monolithic carbon tube by gluing or shrink fitting.
10. The seat structure according to claim 1 , wherein the hybrid tube is straight from a first end of the hybrid tube to a second end of the hybrid tube.
11. The seat structure according to claim 1 , wherein the peripheral end chamfer is positioned closer to the first reinforcement structure than the second reinforcement structure and faces away from the first reinforcement structure.
12. The seat structure according to claim 1 , wherein the peripheral end chamfer comprises an annular surface that extends from a first end of the peripheral end chamfer to a second end of the peripheral end chamfer, and wherein the annular surface faces an annular surface of the monolithic carbon tube.
13. The seat structure according to claim 9 , wherein the first hybrid tube is straight from a first end of the hybrid tube to a second end of the hybrid tube.
14. The seat structure according to claim 9 , wherein a portion of the first sleeve is inserted into the first hole.