Composite rod, manufacturing method and tool

Patent metadata

Field	Value
Publication number	US-9091387-B2
Application number	US-201213722368-A
Country	US
Kind code	B2
Filing date	Dec 20, 2012
Priority date	Dec 22, 2011
Publication date	Jul 28, 2015
Grant date	Jul 28, 2015

Abstract

The present invention describes composite rods keeping two elements apart a determined distance carrying the loads between them, such as railways, industrial premises, etc. Besides, the manufacturing method thereof and the tool involved in this process are also described.

First claim

The invention claimed is:

1. A composite rod device adapted to keep two elements apart a determined distance and carry a load applied between the two elements, the composite rod device comprising:
a structure including an outer hollow body comprising a composite material and an inner hollow body comprising a composite material, wherein each one of the outer hollow body and the inner hollow body is independently able to withstand the applied load, thereby providing a double load path, and wherein a central portion of the inner hollow body comprises an inner diameter that is larger than an inner diameter of peripheral portions of the inner hollow body;
a first rod end arranged at a first end of the structure and a second rod end arranged at a second end of the structure; and
a conductor material arranged between the outer hollow body and the inner hollow body.

2. The composite rod device according to claim 1 , wherein the conductor material comprises at least one layer of copper foil.

3. The composite rod device according to claim 1 , wherein:
an assembly between the outer hollow body, the inner hollow body, the first rod end, and the second rod end is double threaded; and
the outer hollow body comprises outer metallic inserts in contact with the conductor material.

4. The composite rod device according to claim 3 , wherein the outer metallic inserts comprise integrated lugs arranged to connect with conductor bonding jumpers.

5. The composite rod device according to claim 3 , wherein the inner hollow body comprises inner metallic inserts.

6. The composite rod device according to claim 4 , wherein the inner hollow body comprises inner metallic inserts.

7. The composite rod device according to claim 1 , wherein each of the first rod end and the second rod end comprises at least one of metallic material and composite material.

8. The composite rod device according to claim 6 , wherein the outer metallic inserts and the inner metallic inserts are shaped so to avoid a pull out effect or a pull through effect, and at least one of the outer hollow body and the inner hollow body comprises increased wall thickness proximate to the metallic inserts relative to a wall thickness in at least one area distal from the metallic inserts.

9. The composite rod device according to claim 1 , wherein the composite material comprises a quasi-isotropic laminate.

10. The composite rod device according to claim 1 , further comprising a layer of release film between the inner hollow body and the conductor material.

11. The composite rod device according to claim 2 , comprising a densely loaded epoxy resin comprising micro sized highly conductive particles establishing contact between the conductor material and the outer metallic inserts.

12. The composite rod device according to claim 1 , wherein the composite material comprises a fibre-reinforced laminate with about 60% of the fibres of the laminate following a 0° orientation along a longitudinal axis of the composite rod, and wherein the outer hollow body comprises 19 layers.

13. The composite rod device according to claim 9 , wherein the quasi-isotropic laminate for the outer body comprises 19 layers, and the quasi-isotropic laminate for the inner body comprises 27 layers.

14. The composite rod device according to claim 1 , wherein the composite material comprises a high modulus fibre that confer the composite material with a Young's modulus of at least about 157.656 MPa, wherein the outer hollow body comprises 12 layers, and wherein the inner hollow body comprises 16 layers.

Assignees

• Airbus Operations Sl
• Airbus Operations Sl

Inventors

• Quintana Rio Andres

Classifications

• F16C2326/43

  Aeroplanes; Helicopters · CPC title

• B29C33/485

  cores or mandrels (collapsible mandrels for shaping tube ends B29C57/02; collapsible mandrels for winding and joining B29C53/824) · CPC title

• B32B37/02

  characterised by a sequence of laminating steps, e.g. by adding new layers at consecutive laminating stations · CPC title

• B32B37/0053

  Constructional details of laminating machines comprising rollers; Constructional features of the rollers · CPC title

• F16M13/02 Primary

  for supporting on, or attaching to, an object, e.g. tree, gate, window-frame, cycle · CPC title