Tank comprising inner and outer chambers and at least one link system with flexible radial blades linking said chambers

Patent metadata

Field	Value
Publication number	US-12078293-B2
Application number	US-202318172079-A
Country	US
Kind code	B2
Filing date	Feb 21, 2023
Priority date	Feb 25, 2022
Publication date	Sep 3, 2024
Grant date	Sep 3, 2024

Abstract

A double-walled tank including at least one link system linking the outer and inner chambers of the tank and including a central part linked to the inner chamber and at least three blades distributed around the central part, each blade extending between a first end linked to the central part and a second end which has a head linked to the outer chamber, each blade being sufficiently flexible to be deformed elastically between its first and second ends in a direction of displacement.

First claim

The invention claimed is:

1. A tank comprising:
an outer chamber,
an inner chamber positioned in the outer chamber; and
first and second link systems, diametrically opposite, linking the outer chamber and the inner chamber, the outer chamber and the inner chamber being displaced with respect to one another in a direction of displacement in operation,
wherein at least one of the first and second link systems comprises:
a central part linked to one of the outer chamber and the inner chamber; and
at least three blades distributed around the central part, each blade extending between a first end linked to the central part and a second end which has a head linked to the other of the outer chamber and the inner chamber;
wherein each blade is sufficiently flexible to be deformed elastically between its first and second ends in the direction of displacement, wherein the at least three blades are curved and have a profile such that the heads are:
offset towards the inner chamber with respect to the central part in an absence of strains corresponding to an absence of hydrogen in the inner chamber, and
disposed substantially in a same transverse plane as the central part in a presence of strains corresponding to a presence of hydrogen in a cryogenic state in the inner chamber.

2. The tank according to claim 1 ,
wherein the central part is linked to the inner chamber, and
wherein each of the heads is linked to the outer chamber.

3. The tank according to claim 2 ,
wherein the central part comprises:
a support secured to the inner chamber,
a ring linked to the outer chamber via the blades and configured to be positioned around the support; and
a fixing system configured to immobilize the ring with respect to the support at least in the direction of displacement.

4. The tank according to claim 3 ,
wherein the support comprises:
a base fixed onto the inner chamber by fixing elements; and
a tubular portion secured to the base, having an axis substantially coinciding with the direction of displacement and onto which the ring is fitted.

5. The tank according to claim 4 ,
wherein the fixing system comprises:
a threaded section provided on the tubular portion, and
a nut configured to be screwed onto the threaded section.

6. The tank according to claim 5 , wherein the fixing system comprises:
a system for blocking rotation of the nut;
a compression fitting inserted between the nut and the ring;
two shear rings positioned on either side of the ring; or
any combination of the above.

7. The tank according to claim 3 ,
wherein the outer chamber comprises:
an aperture in line with the support; and
a cover configured to block the aperture.

8. The tank according to claim 2 ,
wherein the outer chamber comprises, for each of the heads, an attachment with a U section, comprising:
a base against which the head is fixed, positioned in a substantially transverse plane; and
legs linking the base to the outer chamber.

9. The tank according to claim 1 , wherein the link system further comprises:
a safety system comprising:
a female sleeve secured to the outer chamber, which has an axis coinciding with the direction of displacement; and
a male extension, secured to the inner chamber, positioned in the female sleeve, the male extension and the female sleeve being dimensioned such that there remains a play all around the male extension between the female sleeve and the male extension when the blades are not damaged.

10. The tank according to claim 3 , wherein the first and second link systems comprise dissociable first and second parts, the first part comprising the ring, the blades and the heads, the second part comprising the support.

Assignees

• Airbus Operations Sas

Inventors

• Gallardo Julien

Classifications

• F17C2260/04

  Reducing risks and environmental impact · CPC title

• F17C2223/0161

  cryogenic, e.g. LNG, GNL, PLNG · CPC title

• F17C2221/012

  Hydrogen · CPC title

• F17C2203/0629

  Two walls · CPC title

• F17C2203/03

  Thermal insulations · CPC title