Light weight thermoplastic flex foam and hybrid duct system

Patent metadata

Field	Value
Publication number	US-9669593-B2
Application number	US-76342707-A
Country	US
Kind code	B2
Filing date	Jun 14, 2007
Priority date	Jun 14, 2007
Publication date	Jun 6, 2017
Grant date	Jun 6, 2017

Abstract

An aerospace vessel including a fuselage, a means for causing the fuselage to fly coupled to the fuselage, and an environmental control system within the fuselage. The environmental control system includes a duct made of closed cell thermoplastic foam, such as polyvinylidene fluoride foam.

First claim

What is claimed is:

1. A duct comprising:
a thermoplastic foam sheet having flammability properties for use in an environmental control system of a vehicle;
a crenulated first edge of the thermoplastic foam sheet;
a second edge of the thermoplastic foam sheet;
a seam comprising the crenulated first edge compressed with the second edge; and
a wire welded around an outer surface of the duct, the wire comprising a thermoplastic material, and the wire disposed in the shape of a helix.

2. The duct of claim 1 wherein the first edge and the second edge are beveled.

3. The duct of claim 2 wherein the first edge and the second edge are beveled in a same direction.

4. The duct of claim 1 wherein the helix is welded to the duct using one of applied heat, an adhesive, and both applied heat and an adhesive.

5. The duct of claim 1 wherein the duct is pleated.

6. The duct of claim 1 wherein the helix is characterized by a pitch that dampens a noise of a given frequency range.

7. The duct of claim 1 wherein the helix is characterized by an angle that dampens a noise of a given frequency range.

8. The duct of claim 1 wherein the duct is further formed by wrapping the thermoplastic foam sheet around a mandrel to overlap the crenulated first edge and the second edge.

9. The duct of claim 8 wherein wrapping the thermoplastic foam sheet around a mandrel defines an internal shape of the thermoplastic foam sheet, and wherein an outside tool is applied against the overlapped crenulated first edge and the second edge of the thermoplastic foam sheet to compress the overlapped crenulated first edge and the second edge together while heat is applied to the duct.

10. The duct of claim 1 wherein the duct is post-formed to a different shape.

11. The duct of claim 10 wherein the duct is post-formed into a complex shape by heating the duct and pressing the duct into a mold.

12. The duct of claim 11 wherein the duct is post-formed by air blown inside the duct while applying heat.

13. The duct of claim 10 wherein the duct has a shape selected from the group consisting of a tube and a branch-off.

14. The duct of claim 1 wherein the duct is formed by compressing the crenulated first edge and the second edge together while applying heat.

15. The duct of claim 1 wherein the thermoplastic foam sheet has a calculated width substantially corresponding to:
W =π( d+ 2 t (1−0.045 d ))+ O,

wherein W represents width,
d represents an inside diameter of the duct,
t represents a thickness of a duct wall, and
O represents an overlap between the first edge and the second edge.

16. The duct of claim 1 wherein the crenulated first edge is selected from one of a foot form and a tooth form.

17. The duct of claim 1 , wherein the duct comprises a PVDF material.

18. The duct of claim 17 , wherein the wire is a hollow wire.

19. The duct of claim 1 wherein the vehicle is selected from the group consisting of an aircraft, a helicopter, a rocket, and a space vessel.

20. A duct comprising:
a PVDV thermoplastic foam sheet having flammability properties suitable for use in an aircraft;
a crenulated first edge of the thermoplastic foam sheet;
a second edge of the thermoplastic foam sheet, the crenulated first edge and the second edge being beveled, wherein the duct is formed by wrapping the thermoplastic foam sheet around a mandrel to overlap the crenulated first edge and the second edge and to define an internal shape of the thermoplastic foam sheet, wherein a tool is applied against the overlapped crenulated first edge and the second edge to compress the overlapped crenulated first edge and second edge together while heat is applied to the duct; and
a wire welded around an outer surface of the sheet, the wire comprising a thermoplastic material, and the wire disposed in the shape of a helix.

21. A sheet assembly for forming a duct, the assembly comprising:
a thermoplastic foam material sheet having flammability properties for use in an aircraft;
a crenulated first edge of the thermoplastic foam sheet;
a second edge of the thermoplastic foam sheet;
the first edge and second edge joined at a seam so as to form the duct; and
a wire welded around an outer surface of the sheet, the wire comprising a thermoplastic material, and the wire disposed in the shape of a helix.

Assignees

• Frantz Walter Forrest
• Patel Jayant D
• Maben Douglas Dean
• Whitman Bruce
• Freeman Douglas E
• Boeing Co

Inventors

• Frantz Walter Forrest
• Patel Jayant D
• Maben Douglas Dean
• Whitman Bruce
• Freeman Douglas E

Classifications

• Y10T156/1038

  Hollow cylinder article · CPC title

• F24F13/0263

  Insulation for air ducts · CPC title

• F16L11/08

  with reinforcements embedded in the wall (F16L11/11 takes precedence) · CPC title

• F16L9/17

  obtained by bending a sheet longitudinally and connecting the edges · CPC title

• F16L9/12

  of plastics with or without reinforcement (F16L9/16 - F16L9/22 take precedence) · CPC title