Tubular structure and a method of manufacturing thereof

Patent metadata

Field	Value
Publication number	US-11634206-B2
Application number	US-201916359539-A
Country	US
Kind code	B2
Filing date	Mar 20, 2019
Priority date	Aug 2, 2016
Publication date	Apr 25, 2023
Grant date	Apr 25, 2023

Abstract

Methods and structures are disclosed. An example method includes: rotating a tubular mandrel about a longitudinal axis of the tubular mandrel; depositing a composite material on an inner surface of the tubular mandrel to form a composite tubular member on the inner surface of the tubular mandrel; inserting and expanding an inner expandable mandrel within the composite tubular member to cause the inner expandable mandrel to press the composite tubular member against the inner surface of the tubular mandrel; curing the composite tubular member; removing the inner expandable mandrel; placing a frame within the composite tubular member; and removing the tubular mandrel so as to obtain the composite tubular member with the frame placed therein.

First claim

What is claimed is:

1. A method comprising:
rotating a tubular mandrel about a longitudinal axis of the tubular mandrel, wherein the tubular mandrel is vertically-oriented;
depositing a composite material on an inner surface of the tubular mandrel as the tubular mandrel is rotated so as to form a composite tubular member on the inner surface of the tubular mandrel;
inserting an inner expandable mandrel within the composite tubular member;
expanding the inner expandable mandrel so as to cause the inner expandable mandrel to press the composite tubular member against the inner surface of the tubular mandrel;
curing the composite tubular member while being sandwiched between the inner expandable mandrel and the tubular mandrel;
removing the inner expandable mandrel;
placing a frame within the composite tubular member, wherein the frame is a geodesic frame comprising two oppositely-wound spirals joined at intersection points of the two oppositely-wound spirals, and wherein placing the geodesic frame within the composite tubular member comprises: axially stretching the geodesic frame to reduce a diameter of the geodesic frame, inserting the axially stretched geodesic frame within the composite tubular member, and releasing the geodesic frame to cause the diameter of the geodesic frame to expand, thereby causing the geodesic frame to contact the composite tubular member; and
removing the tubular mandrel so as to obtain the composite tubular member with the frame placed therein.

2. The method of claim 1 , wherein the tubular mandrel is rotated at a particular rotational speed, and wherein the inner expandable mandrel is rotated at the particular rotational speed such that respective rotations of the inner expandable mandrel and the tubular mandrel are synchronized.

3. The method of claim 1 , further comprising:
stopping rotation of the tubular mandrel prior to the curing.

4. The method of claim 3 , wherein the inner expandable mandrel includes an inflatable bladder, and wherein expanding the inner expandable mandrel comprises:
inflating the inflatable bladder until an outer surface of the inflatable bladder applies a predetermined pressure on the composite tubular member to secure the composite tubular member against the inner surface of the tubular mandrel upon stopping the rotation of the tubular mandrel.

5. The method of claim 1 , further comprising:
orientating the tubular mandrel, the composite tubular member, and the inner expandable mandrel in a horizontal position prior to the curing.

6. The method of claim 1 , wherein the tubular mandrel comprises a plurality of interlocked arc segments of a tube.

7. The method of claim 1 , wherein depositing the composite material on the inner surface of the tubular mandrel comprises:
depositing the composite material using a device that is moving vertically within the tubular mandrel as the tubular mandrel is rotated.

8. The method of claim 1 , further comprising:
coupling respective ends of the two oppositely-wound spirals via an end plate.

9. The method of claim 1 , wherein the composite tubular member includes one or more sections having an increased thickness compared to other sections of the composite tubular member, and wherein depositing the composite material to form the composite tubular member on the inner surface of the tubular mandrel comprises:
depositing the composite material via a longitudinally-moving device, wherein a longitudinal speed of the longitudinally-moving device and number of passes of the longitudinally-moving device at the one or more sections are varied to increase thickness of the composite material at the one or more sections of the composite tubular member.

10. The method of claim 1 , wherein at least one of the two oppositely-wound spirals of the geodesic frame has a U-shaped or an L-shaped cross section.

11. A method for preparing a tubular structure, the method comprising:
rotating a tubular mandrel about a longitudinal axis of the tubular mandrel;
depositing a composite material on an inner surface of the tubular mandrel as the tubular mandrel is rotated so as to form a composite tubular member on the inner surface of the tubular mandrel, wherein the composite tubular member includes one or more sections having an increased thickness compared to other sections of the composite tubular member, and wherein depositing the composite material to form the composite tubular member on the inner surface of the tubular mandrel comprises: depositing the composite material via a longitudinally-moving device, wherein a longitudinal speed of the longitudinally-moving device and number of passes of the longitudinally-moving device at the one or more sections are varied to increase thickness of the composite material at the one or more sections of the composite tubular member;
inserting an inner expandable mandrel within the composite tubular member;
expanding the inner expandable mandrel so as to cause the inner expandable mandrel to press the composite tubular member against the inner surface of the tubular mandrel;
removing the inner expandable mandrel;
inserting a geodesic frame within the composite tubular member; and
removing the tubular mandrel so as to obtain the composite tubular member with the geodesic frame placed therein.

12. The method of claim 11 , wherein rotating the tubular mandrel about the longitudinal axis thereof comprises rotating the tubular mandrel while the tubular mandrel is vertically-oriented.

13. The method of claim 11 , further comprising:
prior to removing the inner expandable mandrel, curing the composite tubular member while being sandwiched between the inner expandable mandrel and the tubular mandrel.

14. The method of claim 13 , further comprising:
orientating the tubular mandrel, the composite tubular member, and the inner expandable mandrel in a horizontal position prior to the curing.

15. The method of claim 11 , wherein inserting the geodesic frame comprises inserting the geodesic frame comprising two oppositely-wound spirals joined at intersection points of the two oppositely-wound spirals.

16. The method of claim 11 , further comprising:
coupling respective ends of the two oppositely-wound spirals via an end plate.

17. The method of claim 11 , wherein inserting the geodesic frame within the composite tubular member comprises:
axially stretching the geodesic frame to reduce a diameter of the geodesic frame;
inserting the geodesic frame within the composite tubular member while being axially stretched; and
releasing the geodesic frame to cause the geodesic frame to expand, thereby causing the geodesic frame to contact the composite tubular member.

18. The method of claim 11 , wherein the inner expandable mandrel comprises an inflatable bladder, and wherein expanding the inner expandable mandrel comprises:
inflating the inflatable bladder until an outer surface of the inflatable bladder applies a predetermined pressure on the composite tubular member to secure the composite tubular member against the inner surface of the tubular mandrel.

19. The method of claim 11 , wherein the tubular mandrel comprises a plurality of interlocked arc segments of a tube, and wherein removing the tubular mandrel comprises:
disassembling the plurality of interlocked arc segments from around the composite tubular member.

20. The method of claim 11 , wherein rotating the tubular mandrel comprises rotating the tubular mandrel at a particular rotational speed, and wherein the method further comprises

Assignees

• Boeing Co

Inventors

• Cowart George Stephen

Classifications

• B29C2043/143

  stepwise in a vertical direction, i.e. each time modifying the thickness · CPC title

• B29C67/0022

  using an internal mandrel · CPC title

• B29C43/102

  using rigid mould parts specially adapted for moulding articles having an axis of symmetry · CPC title

• B29C43/08

  with circular movement {, e.g. mounted on rolls, turntables} · CPC title

• B29C2043/043

  rotating on their own axis without linear displacement · CPC title