Vessel insulation assembly

Patent metadata

Field	Value
Publication number	US-9783324-B2
Application number	US-201414570370-A
Country	US
Kind code	B2
Filing date	Dec 15, 2014
Priority date	Aug 26, 2014
Publication date	Oct 10, 2017
Grant date	Oct 10, 2017

Abstract

A vessel includes a vessel wall and an insulation assembly coupled to the vessel wall. The insulation assembly includes a stochastic foam material and a microtruss structure encased within the foam material. The microtruss structure includes a plurality of truss members interconnected at a plurality of nodes. Each truss member is in contact with the foam material such that the microtruss structure provides a structural core for the foam material.

First claim

What is claimed is:

1. A vessel comprising:
a vessel wall; and
an insulation assembly coupled to said vessel wall, said insulation assembly comprising:
a stochastic foam material;
a microtruss structure comprising a plurality of truss members interconnected at a plurality of nodes, said microtruss structure encased within said foam material such that said foam material is in contact with said plurality of truss members, wherein said plurality of truss members each include a first end and an opposing second end; and
a plurality of adhesion features extending obliquely with respect to an outer surface of said plurality of truss members from said plurality of truss members between said first end and said second end to facilitate adhesion between said microtruss structure and said foam material.

2. The vessel in accordance with claim 1 , wherein each truss member of said plurality of truss members is substantially hollow.

3. The vessel in accordance with claim 2 , wherein said foam material is distributed within said hollow truss members and is distributed between adjacent truss members of said plurality of truss members.

4. The vessel in accordance with claim 1 , wherein each truss member of said plurality of truss members is substantially solid.

5. The vessel in accordance with claim 1 , wherein said vessel comprises a propellant tank configured to contain a supply of a cryogenic propellant.

6. The vessel in accordance with claim 1 , wherein said vessel wall comprises a solid sheet of material.

7. The vessel in accordance with claim 1 , wherein said vessel wall comprises a top wall, a bottom wall, and a plurality of supports extending therebetween such that said top and bottom walls and said plurality of supports define a plurality of cavities, wherein said foam material and said microtruss structure are coupled at least one of within said plurality of cavities and to said top wall adjacent said plurality of cavities.

8. The vessel in accordance with claim 1 further comprising a thermal protection layer configured to protect said foam material, wherein said thermal protection layer comprises an outermost layer of said insulation assembly.

9. The vessel in accordance with claim 1 , wherein said plurality of adhesion features are formed from at least one of glass fibers and carbon fibers.

10. An aerospace vehicle comprising:
a vessel comprising a vessel wall defining an inner volume that is configured to hold a propellant supply; and
a reinforced insulation assembly coupled to said vessel wall, said insulation assembly comprising;
a stochastic foam material;
a microtruss structure encased within said foam material, said microtruss structure comprising a first end and an opposing second end and providing a structural core for said foam material; and
a plurality of adhesion features extending from said microtruss structure between said first end and said second end, wherein said plurality of adhesion features facilitates adhesion between said microtruss structure and said foam material, wherein said plurality of adhesion features comprise elongated members that extend away from said microtruss structure.

11. The aerospace vehicle in accordance with claim 10 , wherein said vessel wall includes an interior and an exterior surface, said insulation assembly coupled to at least one of said interior and said exterior surfaces.

12. The aerospace vehicle in accordance with claim 10 , wherein said insulation assembly is coupled to said vessel wall using an adhesive.

13. The aerospace vehicle in accordance with claim 10 further comprising a sealant layer applied to said insulation assembly, said sealant layer configured to isolate said insulation assembly from said propellant supply.

14. The aerospace vehicle in accordance with claim 10 , further comprising a selectively permeable membrane coupled to said insulation assembly, said membrane is configured to allow a flow of fluids therethrough and to impede the passage of a solid particulate therethrough.

15. A method of manufacturing an insulation assembly, said method comprising:
fabricating a microtruss structure having a plurality of truss members interconnected at a plurality of nodes;
coupling a plurality of adhesion features to the plurality of truss members such that the plurality of adhesion features extend only partially about a circumference of the plurality of truss members;
coupling the microtruss structure to a wall of a vessel; and
applying a foam material to the microtruss structure and the vessel wall such that the microtruss structure is encased within the foam material to provide a structural core for the foam material, wherein the plurality of adhesion features facilitate adhesion between the microtruss structure and the foam material.

16. The method in accordance with claim 15 , wherein fabricating a microtruss structure comprises fabricating a hollow microtruss structure by:
fabricating a scaffold;
coating the scaffold with a material; and
removing the scaffold.

17. The method in accordance with claim 15 , wherein coupling the microtruss structure to a wall of a vessel further comprises applying an adhesive to at least one of the microtruss structure and the vessel wall.

18. The method in accordance with claim 15 , wherein the plurality of truss members comprises a plurality of hollow truss members, and wherein applying a foam material to the microtruss structure further comprises one of spraying or pouring the foam material within the plurality of hollow truss members that combine to form the microtruss structure.

19. The method in accordance with claim 15 further comprising applying a sealant to a top surface of the foam material, wherein the sealant is configured to isolate the microtruss structure and the foam material from a propellant supply contained within the vessel.

20. The method in accordance with claim 19 further comprising coupling a selectively permeable membrane to one of the top surface of the foam material or the sealant.

Assignees

• Boeing Co

Inventors

• Embler Jonathan D
• Gaynor Iii Timothy Leo
• Roper Christopher S
• Schaedler Tobias A
• Fukushima Jeffrey Dale
• Hand Michael Leslie
• Chong Keith Y
• Schubert Randall Colin

Classifications

• B64G1/402 Primary

  Propellant tanks; Feeding propellants · CPC title

• B32B2305/022

  Foam · CPC title

• B29K2075/00

  Use of {PU, i.e.} polyureas or polyurethanes {or derivatives thereof}, as moulding material · CPC title

• B32B2266/0228

  Aromatic vinyl resin, e.g. styrenic (co)polymers · CPC title

• B29C44/18

  Filling preformed cavities {(B29C44/1204 takes precedence)} · CPC title