Manufacturing composite tubular structures using adjustable cylindrical mechanical pressure device and process

Patent metadata

Field	Value
Publication number	US-9527126-B2
Application number	US-201414328702-A
Country	US
Kind code	B2
Filing date	Jul 11, 2014
Priority date	Jul 11, 2014
Publication date	Dec 27, 2016
Grant date	Dec 27, 2016

Abstract

A system for manufacturing a composite tubular structure. The system includes an outer tube configured to remain rigid up to at least a first threshold pressure. The system includes an inner tube internal to the outer tube and substantially coaxial with the outer tube. The inner tube has a first outer surface and a first inner surface. The inner tube is configured to remain rigid up to a second threshold pressure that is less than the threshold first pressure. The system includes a composite tubular layup laid on the first outer surface of the inner tube. The system includes an assembly of a plurality of separate segments disposed inside the inner tube, each segment adjacent to two other segments, to form a segmented inner cylinder having a second outer surface of a cylindrical shape and an inner channel of a first conical shape.

First claim

What is claimed is:

1. A method of manufacturing a composite tubular structure, the method comprising:
slidably advancing a rod having a conical shape within a conically shaped inner channel formed by an assembly of a plurality of adjacent, separate segments, the assembly disposed in an inner tube, the inner tube internal to an outer tube, to apply a substantially uniform pressure to a composite tubular material on an outer surface of the inner tube.

2. The method of claim 1 further comprising varying the substantially uniform pressure by changing an extent to which the rod is advanced within the inner channel.

3. The method of claim 2 , wherein varying the substantially uniform pressure is performed by a mechanical device advancing or retracting the rod.

4. The method of claim 3 further comprising:
monitoring, using a computer in communication with the mechanical device, the extent the rod is advanced or retracted within the inner channel.

5. The method of claim 4 further comprising:
sensing the substantially uniform pressure using a sensor operably connected to the outer tube.

6. The method of claim 5 further comprising:
defining and inputting, using the computer, desired values for composite consolidation or curing pressure and temperature.

7. The method of claim 6 further comprising:
reading temperature from a thermocouple in communication with the composite tubular material.

8. The method of claim 6 further comprising:
determining whether the substantially uniform pressure is equal to a required pressure.

9. The method of claim 8 further comprising:
if the substantially uniform pressure is not equal to the required pressure, and if the substantially uniform pressure is less than the required pressure, then advancing the rod further within the inner tube.

10. The method of claim 8 further comprising:
if the substantially uniform pressure is not equal to the required pressure, and if the substantially uniform pressure is greater than the required pressure, then at least partially retracting the rod from within the inner tube.

11. The method of claim 8 further comprising:
if the substantially uniform pressure is equal to the required pressure, then holding the rod at a location within the inner tube.

12. The method of claim 11 further comprising:
checking the sensor at time increments.

13. The method of claim 12 further comprising:
advancing or retracting the rod within the inner tube as pressure changes so as to maintain the substantially uniform pressure.

14. The method of claim 5 further comprising:
prior to slidably advancing the rod, braiding a thermoplastic material onto a tube to form the composite tubular material.

15. The method of claim 14 further comprising:
infusing the thermoplastic material with an epoxy resin.

16. The method of claim 5 further comprising:
prior to slidably advancing the rod, braiding a pre-impregnated fiber tape over a tube to form the composite tubular material.

17. The method of claim 5 further comprising:
prior to slidably advancing the rod, weaving a thermoplastic material in a pattern onto a tube to form the composite tubular material.

18. The method of claim 17 further comprising:
infusing the thermoplastic material with an epoxy resin.

19. The method of claim 5 further comprising:
prior to slidably advancing the rod, weaving a pre-impreganated fiber tape in a pattern onto a tube to form the composite tubular material.

Assignees

• Boeing Co

Inventors

• Apdalhaliem Sahrudine
• Ashmawi Waeil M
• Shome Moushumi
• Marcoe Jeffery Lee

Classifications

• Y10T29/49771

  Quantitative measuring or gauging · CPC title

• B32B15/14

  next to a fibrous or filamentary layer · CPC title

• B32B2307/302

  Conductive · CPC title

• B21D39/04 Primary

  of tubes with tubes; of tubes with rods {(crimped pipe joints as such F16L13/14)} · CPC title

• Y10T29/49776

  Pressure, force, or weight determining · CPC title