Segmented vacuum jacketed tank system and method of using the same

Patent metadata

Field	Value
Publication number	US-12287067-B2
Application number	US-202318336991-A
Country	US
Kind code	B2
Filing date	Jun 17, 2023
Priority date	Jun 17, 2023
Publication date	Apr 29, 2025
Grant date	Apr 29, 2025

Abstract

There is provided a segmented vacuum jacketed tank system. The system includes a segmented structurally integrated vacuum tank having a vacuum tank main portion between vacuum tank end portions. The vacuum tank main portion includes a vacuum tank skin having an outer surface and an inner surface, vacuum tank skin segments, and a longitudinal cross section with a profile geometry configured for buckling prevention for the vacuum tank skin under external pressure loads. The vacuum tank main portion includes multipurpose stiffener member(s) configured to carry one or more of system transport line(s), a liquid fuel, or a nitrogen gas in an interior. The system includes a pressure tank within the segmented structurally integrated vacuum tank. The pressure tank is configured to store a cryogenic fluid and includes a pressure tank main portion between pressure tank end portions. The system further includes a vacuum cavity.

First claim

The invention claimed is:

1. A segmented vacuum jacketed tank system, comprising:
a segmented structurally integrated vacuum tank having a vacuum tank main portion extending between vacuum tank end portions, the vacuum tank main portion comprising:
a vacuum tank skin having an outer surface with outer surface portions and an inner surface with inner surface portions, the vacuum tank skin comprising a plurality of vacuum tank skin segments, and having a longitudinal cross section with a profile geometry configured for buckling prevention for the vacuum tank skin under external pressure loads; and
one or more multipurpose longerons, each coupled between two of the plurality of vacuum tank skin segments, and each coupled to at least two of the outer surface portions and at least two of the inner surface portions, the one or more multipurpose longerons each having an interior volume that is substantially hollow to accommodate and hold one or more of one or more system transport lines, a liquid fuel, or a nitrogen gas;

a pressure tank mounted within the segmented structurally integrated vacuum tank, and attached to an interior of the segmented structurally integrated vacuum tank, via a forward tank attach fitting and an aft tank attach fitting, the pressure tank configured to store a cryogenic fluid and comprising a pressure tank main portion extending between pressure tank end portions, the pressure tank main portion comprising a pressure tank skin having an outer surface and an inner surface; and
a vacuum cavity formed between the segmented structurally integrated vacuum tank and the pressure tank, the vacuum cavity forming a gap between a pressure tank outer surface of the pressure tank, and a vacuum tank inner surface of the segmented structurally integrated vacuum tank, such that the pressure tank is not in direct contact with both the vacuum tank skin and the one or more multipurpose longerons.

2. The segmented vacuum jacketed tank system of claim 1 , wherein the vacuum tank skin comprises the plurality of vacuum tank skin segments in a range of two vacuum tank skin segments to eight vacuum tank skin segments.

3. The segmented vacuum jacketed tank system of claim 1 , wherein the profile geometry of the longitudinal cross section of the vacuum tank skin has a shape comprising one or more of a corrugated shape, a sinusoidal shape, a superimposed curves shape, a symmetrical shape, a non-symmetrical shape, a pointed corner shape, a hat shape, or a fractal shape.

4. The segmented vacuum jacketed tank system of claim 1 , wherein the one or more multipurpose longerons comprise one or more multipurpose mega-stringers.

5. The segmented vacuum jacketed tank system of claim 1 , wherein the one or more multipurpose longerons comprise a range of one multipurpose longeron to eight multipurpose longerons.

6. The segmented vacuum jacketed tank system of claim 1 , wherein one of the one or more multipurpose longerons comprises a bottommost centered multipurpose longeron having a tail skid attachment fitting coupled to an exterior side of the bottommost centered multipurpose longeron, the tail skid attachment fitting coupled to a tail skid.

7. The segmented vacuum jacketed tank system of claim 1 , wherein the vacuum tank main portion further comprises one or more single purpose longerons coupled to one or more of the outer surface portions of the plurality of vacuum tank skin segments.

8. The segmented vacuum jacketed tank system of claim 1 , wherein the one or more system transport lines comprise one or more of one or more fuel lines, one or more electrical lines, one or more electrical signal lines, one or more hydraulic lines, one or more pneumatic lines, one or more compressed air lines, one or more power lines, one or more lighting lines, one or more auxiliary power unit lines, or one or more data bus lines.

9. The segmented vacuum jacketed tank system of claim 1 , wherein the pressure tank further comprises an internal structure in an interior of the pressure tank, the internal structure comprising one or more interior shear walls forming two or more interior sections.

10. The segmented vacuum jacketed tank system of claim 9 , wherein each of the one or more interior shear walls of the internal structure comprises a flat sheet, a tension structure, a wire, or a truss structure.

11. The segmented vacuum jacketed tank system of claim 9 , wherein the one or more interior shear walls of the internal structure support anti-slosh baffles.

12. The segmented vacuum jacketed tank system of claim 1 , wherein:
the outer surface and the inner surface of the vacuum tank skin, and the outer surface and the inner surface of the pressure tank skin have a circular shape;
the outer surface and the inner surface of the vacuum tank skin, and the outer surface and the inner surface of the pressure tank skin have a lobed shape; or
the outer surface of the vacuum tank skin has the circular shape, and the inner surface of the vacuum tank skin and the outer surface and the inner surface of the pressure tank skin have the lobed shape.

13. An aircraft, comprising:
a fuselage with a plurality of fuselage barrel sections, and an outer aero skin at a fuselage mold line; and
a segmented vacuum jacketed tank system, comprising:
a segmented structurally integrated vacuum tank integrated with the fuselage, the segmented structurally integrated vacuum tank having a vacuum tank main portion extending between vacuum tank end portions, the vacuum tank main portion comprising:
a vacuum tank skin having an outer surface with outer surface portions and an inner surface with inner surface portions, the vacuum tank skin comprising a plurality of vacuum tank skin segments, and having a longitudinal cross section with a profile geometry configured for buckling prevention for the vacuum tank skin under external pressure loads; and
one or more multipurpose stringers longerons, each coupled between two of the plurality of vacuum tank skin segments, each coupled to at least two of the outer surface portions and at least two of the inner surface portions, and each coupled to the outer aero skin, the one or more multipurpose longerons each having an interior volume that is substantially hollow to accommodate and hold one or more of one or more system transport lines, a liquid fuel, or a nitrogen gas;

a pressure tank mounted within the segmented structurally integrated vacuum tank, and attached to an interior of the segmented structurally integrated vacuum tank, via a forward tank attach fitting and an aft tank attach fitting, the pressure tank configured to store a cryogenic fluid and comprising a pressure tank main portion extending between pressure tank end portions, the pressure tank main portion comprising a pressure tank skin having an outer surface and an inner surface; and
a vacuum cavity formed between the segmented structurally integrated vacuum tank and the pressure tank, the vacuum cavity forming a gap between a pressure tank outer surface of the pressure tank, and a vacuum tank inner surface of the segmented structurally integrated vacuum tank, such that the pressure tank is not in direct contact with both the vacuum tank skin and the one or more multipurpose longerons.

14. The aircraft of claim 13 , wherein the segmented structurally integrated vacuum tank is configured without the outer aero skin in an omitted outer aero skin configuration, so that the vacuum tank skin and the one or more multipurpose longerons are exposed to an air flow.

15. The aircraft of claim 13 , wherein the pressure tank further comprises an internal structure in an interior of the pres

Assignees

• Boeing Co

Inventors

• Grip Robert E
• Kutzmann Aaron J
• Noel Nathaniel J

Classifications

• F17C2203/066

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