Thermoplastic composite structures embedded with at least one load fitting and methods of manufacturing same

Patent metadata

Field	Value
Publication number	US-9718248-B2
Application number	US-201414465911-A
Country	US
Kind code	B2
Filing date	Aug 22, 2014
Priority date	Oct 12, 2012
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.

First claim

The invention claimed is:

1. A method of manufacturing a thermoplastic composite tubular structure embedded with a first load fitting, the method comprising:
braiding a first plurality of inner layers of thermoplastic composite material around a mandrel,
the mandrel comprising a soluble, expandable material and comprising a mandrel cross-section defining a first closed geometric shape;
placing a first load fitting on the first plurality of inner layers of thermoplastic composite material,
wherein the first load fitting comprises a main body and a clevis that extends from a central portion of the main body, the first load fitting treated with an adhesion promoter prior to placing the loading fitting on the first plurality of inner layers; and
overbraiding a second plurality of outer layers of thermoplastic composite material around the main body of the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting.

2. The method of claim 1 , further comprising the step of:
installing the overbraided mandrel embedded with the first load fitting into a matched tooling assembly.

3. The method of claim 2 , further comprising the step of:
heating in a heating apparatus the matched tooling assembly with the overbraided mandrel embedded with the first load fitting at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting.

4. The method of claim 3 , wherein upon heating in the heating apparatus, the expandable material of the mandrel expands and exerts pressure on the plurality of inner and outer layers of thermoplastic composite material against the matched tooling assembly causing consolidation of the plurality of inner and outer layers of thermoplastic composite material with the at least one fitting.

5. The method of claim 3 , further comprising the steps of:
cooling the matched tooling assembly containing the thermoplastic composite tubular structure embedded with the first load fitting at a specified cooling profile, and
removing the thermoplastic composite tubular structure embedded with the first load fitting from the matched tooling assembly.

6. The method of claim 5 , further comprising the step of solubilizing the mandrel to remove the mandrel from the thermoplastic composite tubular structure embedded with the first load fitting.

7. The method of claim 6 , wherein, solubilizing the mandrel further comprises solubilizing the mandrel with water or a water-based solution to permanently remove the mandrel from the thermoplastic composite tubular structure embedded with the first load fitting.

8. The method of claim 1 , wherein,
braiding the first plurality of inner layers of thermoplastic composite material around the mandrel so as to define a first inner layer depth, and
braiding the second plurality of outer layers of thermoplastic composite material around the first load fitting and the mandrel so as to define a second outer layer depth so as to form an overbraided mandrel embedded with the first load fitting.

9. The method of claim 8 , wherein, the first inner layer depth of the first plurality of inner layers of thermoplastic composite material is different than the second outer layer depth of the second plurality of outer layers of thermoplastic composite material.

10. The method of claim 1 , further comprising the step of:
placing a second load fitting on the first plurality of inner layers of thermoplastic composite material; and
braiding the second plurality of outer layers of thermoplastic composite material around the first load fitting, the second load fitting, and the mandrel so as to form an overbraided mandrel embedded with the first and second load fitting.

Assignees

• Boeing Co

Inventors

• Marcoe Jeffery Lee
• Matsen Marc Rollo
• Ashmawi Waeil M
• Garcia Jaime C
• Apdalhaliem Sahrudine
• Moser John B
• Lyons Brett I
• Shome Moushumi
• Blohowiak Kay Y

Classifications

• B32B2605/18

  Aircraft · CPC title

• B29C70/462 Primary

  Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames · CPC title

• B29C70/205

  the structure being shaped to form a three-dimensional configuration · CPC title

• B32B5/024

  Woven fabric · CPC title

• B29C2035/0811

  using induction · CPC title