Cryogenic tank for an aircraft and aircraft including such a tank

Patent metadata

Field	Value
Publication number	US-12491996-B2
Application number	US-202217991982-A
Country	US
Kind code	B2
Filing date	Nov 22, 2022
Priority date	Nov 25, 2021
Publication date	Dec 9, 2025
Grant date	Dec 9, 2025

Abstract

A storage tank for a cryogenic fluid including an inner tank that is configured to store the fluid and that is seated in an outer envelope, the inner tank and the outer envelope having a shared longitudinal axis, such that a thermal insulation volume surrounds the inner tank, and wherein the outer envelope surrounds the volume about the inner tank. The tank has at least one damping element made of a deformable material positioned between one end of the inner tank and the outer envelope to wedge the inner tank against the outer envelope. This enables a reliable sliding mechanical link to be formed between at least one end of the inner tank and the outer envelope of the tank, thereby increasing resistance to wear and facilitating assembly of the tank.

First claim

The invention claimed is:

1 . A storage tank for a cryogenic fluid comprising:
an outer envelope, and an inner tank that is configured to store said fluid and that is seated in the outer envelope,
the inner tank and the outer envelope having a shared longitudinal axis defining a direction X, such that a thermal insulation volume surrounds the inner tank, and wherein said outer envelope surrounds said volume about the inner tank,
at least one damping element made of a deformable material positioned between one end of said inner tank and said outer envelope to wedge the inner tank against the outer envelope,
said at least one damping element being fastened firstly to said end of the inner tank and secondly to said outer envelope, and being arranged to create said wedge by positioning said end of the inner tank in relation to said outer envelope when said end of the inner tank moves in translation along the direction X, and
first fastening means being arranged to attach said at least one damping element to the end of said inner tank and second fastening means being arranged to attach said at least one damping element to an inner surface of said outer envelope, wherein said at least one damping element is ring-shaped, wherein said first fastening means comprise a sleeve fastened to the end of the inner tank and have a first shoulder and a thread that are configured to fasten said at least one damping element about a portion of said sleeve, against said first shoulder, and to hold said at least one damping element against said first shoulder by tightening an assembly comprising a washer and a nut onto said sleeve portion, and wherein said second fastening means comprise
a neck formed about an opening at one end of the outer envelope positioned on the same side of the tank as the end of the inner tank, the neck having a second shoulder, and
a locking ring crimped onto said neck and configured to hold said at least one damping element against said second shoulder.

2 . The storage tank for a cryogenic fluid according to claim 1 , wherein the deformable material is an elastomer.

3 . The storage tank for a cryogenic fluid according to claim 1 , wherein the deformable material has a plurality of metal inserts arranged parallel to the direction X.

4 . An aircraft including at least one storage tank for a cryogenic fluid according to claim 1 .

5 . A storage tank for a cryogenic fluid comprising:
an outer envelope, an inner tank that is configured to store said fluid and that is seated in the outer envelope,
the inner tank and the outer envelope having a shared longitudinal axis defining a direction X, such that a thermal insulation volume surrounds the inner tank, and wherein said outer envelope surrounds said volume about the inner tank,
at least one damping element made of a deformable material positioned between one end of said inner tank and said outer envelope to wedge the inner tank against the outer envelope, said at least one damping element being fastened firstly to said end of the inner tank and secondly to said outer envelope, and being arranged to create said wedge by positioning said end of the inner tank in relation to said outer envelope when said end of the inner tank moves in translation along the direction X, and first fastening means being arranged to attach said at least one damping element to the end of said inner tank and second fastening means being arranged to attach said at least one damping element to an inner surface of said outer envelope, wherein said at least one damping element is ring-shaped, wherein said first fastening means comprise a sleeve fastened to the end of the inner tank and have a first shoulder and a thread that are configured to fasten said at least one damping element about a portion of said sleeve, against said first shoulder, and to hold said at least one damping element against said first shoulder by tightening an assembly comprising a washer and a nut onto said sleeve portion, and wherein said second fastening means comprise
a ring-shaped metal insert, and
a neck formed about an opening at one end of the outer envelope positioned on the same side of the tank as the end of the inner tank,
an inner surface of the neck having a slot into which the ring-shaped metal insert is inserted, or a threaded hole into which the ring-shaped metal insert is screwed,
an inner surface of said insert having a second shoulder and a thread that are arranged to hold said at least one damping element against said second shoulder by tightening an assembly comprising a washer and a nut in said ring-shaped metal insert.

6 . The storage tank for a cryogenic fluid according to claim 5 , wherein the deformable material is an elastomer.

7 . The storage tank for a cryogenic fluid according to claim 5 , wherein the deformable material has a plurality of metal inserts arranged parallel to the direction X.

8 . An aircraft including at least one storage tank for a cryogenic fluid according to claim 5 .

Assignees

• Airbus Operations Sas

Inventors

• Vercamer Tanguy
• Penven Benoît
• Goupil Frédéric

Classifications

• F17C2270/0189

  Planes · CPC title

• F17C2223/0161

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

• F17C2221/012

  Hydrogen · CPC title

• F17C2203/0629

  Two walls · CPC title

• F17C2203/0391

  by vacuum · CPC title