IP Library Granted Patent US 9,458,955
Granted Patent B2
US 9,458,955 · App. 13/945,940 · Granted Oct 4, 2016

Composite waste and water transport elements and methods of manufacture for use on aircraft

Inventors: Jason Hammer (Mukilteo, WA); Mohan Muttur (Bothell, WA)
Assignee: MAG Aerospace Industries, LLC
F16L9/127B29C33/52B29C67/0055B29C70/30B29D23/00F16L9/12F16L9/128F16L9/133F16L43/008B29L2023/004Y10T428/139Y10T428/1393
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Quick Facts
Patent No.
US 9,458,955
App. No.
13/945,940
Granted
Oct 4, 2016
Kind
B2
Abstract

Embodiments of the present invention provide composite waste and water transport elements that can be designed having various unique shapes and methods for their manufacture.

Claims (14)

1. A composite tube for use in a waste or water system on board a passenger transport vehicle, the tube comprising:

a. a tube body comprising a thermoplastic or thermoset material;

b. one or more fiber materials incorporated into the tube body;

c. wherein the tube has at least one bend comprising a thicker section that is reinforced such that impact resistance at the bend in the tube is greater than along other portions of the tube.

2. The tube of claim 1 , wherein the tube is manufactured using 3D printing technology.

3. The tube of claim 1 , wherein the tube has a non-circular cross-section.

4. The tube of claim 3 , wherein the cross section comprises an oval, D-shaped, C-shaped, curved and flat surface, flat-sided, corkscrewed cross section, or any combination thereof.

5. The tube of claim 1 , wherein the thermoplastic or thermoset material of the tube body comprises polyethylenimine, polyphenylene sulfide, polyphenylsulfone, polyether ether ketone, polyetherketone ketone, polyvinylidene fluoride, or any combination thereof.

6. The tube of claim 1 , wherein the thermoplastic or thermoset material of the tube body comprises epoxy, vinyl ester, or any combination thereof.

7. The tube of claim 1 , wherein the fiber materials comprise carbon fiber, fiber glass, Kevlar, nomex, or any combination thereof.

8. The tube of claim 1 , wherein the fiber materials are continuous fibers, short fibers, uni-directional, woven, braided, or any combination thereof.

9. The tube of claim 1 , wherein the thicker section comprises an impact pad at the bend in the tube.

10. The tube of claim 9 , wherein the impact pad comprises polyarylsulphones, polycarbonates, titanium, CRES, or any combination thereof.

11. The tube of claim 1 , wherein the thicker section comprises a thicker section of the same material of the tube positioned at the bend in the tube.

Assignments (2)
CHANGE OF NAME Recorded Jun 19, 2014
From: MAG AEROSPACE INDUSTRIES, INC.
To: MAG AEROSPACE INDUSTRIES, LLC
Reel/Frame 033202/0315 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 30, 2013
From: HAMMER, JASON; MITTUR, MOHAN
To: MAG AEROSPACE INDUSTRIES, INC.
Reel/Frame 031505/0579 →
Continuity (2)
Provisional Application 61673863 · Jul 20, 2012
Related Publication 20140023812A1 · Jan 23, 2014